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- Aerodynamic complex
- Computer-aided reliability monitoring system of airline fleet
- Computer-aided reliability monitoring system of the Ukrainian fleet
- Robust flight control systems for light unmanned aerial vehiecles and piloted aircrafts
- Science intensive technologies of high presicion stabilized platforms development
- Science intensive technologies for development and modernization of high presicion navigation and control complexes for aviation, marine and space engineering
- The diagnostic technique of the aviation gas turbine engine’s (GTE) passage part
- Mobile informational, measuring and control complex
- Theory, methods and procedures of aircraft-in-flight external outline aerodynamical state diagnostics
- System of composite materials diagnostics using low-speed shock method
- The system of impedance diagnostics of composite materials
- Acoustic-emission diagnostics and monitoring of transport and tribotechnical systems, research of dynamic constructions characteristics
- Indentometr “Micron-gamma”
- Surface quality control with an interference profilometer
- Active system of internal combustion engines parameters’ monitoring
- Sparingly doped eutectic powedery materials and technologies of tribotechnical function coatings with gradient type structure
- Advanced machine of 2070 СМТ-1 type for material’s friction and wearing testing
- Monitoring of petrol actual losses from evaporation
- Sorbent for light fractures collection on objects of oil products supply system
- Nonpolluting complex for recycling used tires
- Complex for contamination level determination with following liquids and fuels rectification process
- Traffic intellectual monitoring system
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- Advanced digital flight trainer of L-410 aircraft
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- Catalyst-activator of liquid fuel
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1113Ukrainian scientific-practical conference "Actual problems of accounting and auditing in the present"November 13, 2012
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1114Scientific conference "Multimedia Technologies in Education"November 14-15, 2012
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1115International scientific-practical conference "Managing high expressway moving objects and training of operators of complex systems"November 15-16, 2012
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1118Scientific-practical seminar "Ways of Improving the Criminal Procedure Law to Limit the Constitutional Rights and Civil Rights in Criminal Proceedings"November 18, 2012
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1120International Scientific Conference "Finance: Theory and Practice"November 20-21, 2012
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1123International scientific conference "Problems of Air Transportation and Aviation Applications in the Fields of Economy"November 23, 2012
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1128Scientific and Technical Conference "Problems of Global Communication, Navigation, Surveillance and Air Traffic CNS / ATM»November 28-30, 2012
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1128National Scientific Conference of Young Scientists and Students "Problems of Navigation and Traffic Management"November 28-29, 2012
2011
1. Useful Model Patent № 59071, МПК В08В 3/12. METHOD OF CONTACTLESS PULSE MAGNETIC TURBULENT CLEANING FRICTIONLESS BEARINGS / Aksionov Oleksandr Fedotovych (UA); Stelmakh Oleksandr Ustymovych (UA); Kostiunik Ruslan Yevhenovych (UA); Manita Oleksandr Serhiiovych (UA); Kuschev Oleksii Viktorovych (UA); Badir Karim Kashash (UA); Stelmakh Oleksandr Volodymyrovych (UA); Bondar Volodymyr Semenovych (UA); Koba Viktor Petrovych (UA); Horenko Maksym Viktorovych (UA); Shevchenko Roald Oleksandrovych (UA); Kovalchuk Olena Heorhiivna (UA).; applicant and patentholder National Aviation University. - № u201006048; filed 19.05.2010; issued 10.05.2011. Bul. №9.
A method of contactless pulse magnetic turbulent cleaning frictionless bearings by washing by a jet of washing liquid in a bath. Removal from the surface of impurities, which are held by adhesion, gravity, and coercive (at domain boundaries) forces on the surfaces of parts is carried out by an intense magnetization reversal by pulse magnetic field both of impurity particles, and the working surfaces, and simultaneous mutual spatial displacement of bearing components in turbulized flow of washing liquid, which carries the particles of impurities into the area of maximum intensity of pulsed magnetic field beyond the bearings, and under action of centrifugal forces in the cleaning liquid is directed into the circulation system for further mechanical filtration.
2. Useful Model Patent № 59112, МПК G06F 15/16. COMPUTING UNIT / Klymenko Iryna Anatoliivna (UA); Zhabina Valentyna Valeriivna (UA); applicant and patentholder National Aviation University. - № u201009793; filed 06.08.2010; issued 10.05.2011. Bul. №9.
The computing unit increases functional capabilities and productivity at processing unit failure for account of reduction of system reconfiguration time delay. The device comprises a operations flow timer unit in according to each processing unit. In the format of each command there is latency period of this command execution. Simultaneously with command sending for execution to one of processing units and a duplicated command record to an operation register, execution time of this command is loaded to an operations flow timer. Each processing unit is adjusted individually for execution of preset operation. If for the preset time the computing unit doesn’t yield ready flags of the result, it considers to be disabled, herewith the system reconfiguration is carried out and unexecuted command is rewritten in ready command buffer independent of information available command shaping medium at a time. The command will be re-executed in an employable computing unit. The individual operation execution unit setting up for time required for execution of each operation allows decreasing delay time at system reconfiguration with abruption of data units. This provides reduction of data conversion time i.e. in general case device yield increase.
3. Useful Model Patent № 59113, МПК G01Р 3/36. LASER TWO-COMPONENT DOPPLER ANEMOMETER / Dyvnych Mykola Polikarpovych (UA); Dyvnych Vasyl Mykolaiovych (UA).; applicant and patentholder National Aviation University. - № u201009796; filed 06.08.2010; issued 10.05.2011. Bul. №9.
Laser two-component Doppler anemometer comprises optically matched laser, splitter of laser ray into three rays, focusing and diverging objectives, aperture and background diaphragm, photo-receiver and measuring device for Doppler frequency. Additionally there at pass of laser rays three optical gates are installed, two of those are directly, and one through delay line are connected to pulse generator, behind divergent objective opaque mirror is installed.
4. Useful Model Patent № 59144, МПК С02F 3/00. PROCESS FOR THE PURIFICATION OF WASTE WATER FROM ORGANIC IMPURITIES / Mykhalevska Tetiana Viacheslavivna (UA); Fokin Andrii Volodymyrovych (UA); Franchuk Hryhorii Mykhailovych (UA); Bondarets Yuliia Volodymyrivna (UA).; applicant and patentholder National Aviation University. - № u201010903; filed 10.09.2010; issued 10.05.2011. Bul. №9.
A process for the purification of waste water from organic impurities comprises the use of plant material. As plant material living plants of water hyacinth are used by growing in reservoir-storages for 6 months with primary growing density of 10 plants/m of water surface to 0.1 % of total reservoir square, with cutting of layer of died plants to mate of 2x2x0.2-0.3 m size, their gathering and digestion in clamps of 10x4x3 m size.
5. Useful Model Patent № 59215, МПК G01Р 3/64. DEVICE FOR DETERMINATION OF OBJECT VELOCITY / Astanin Viacheslav Valentynovych (UA); Schehel Hanna Oleksiivna (UA).; applicant and patentholder National Aviation University. - № u201011897; filed 07.10.2010; issued 10.05.2011. Bul. №9.
Device for determination of velocity of object includes two photo-relay barriers brought into coincidence in one body, placed along line of motion of object at fixed distance one from another, and block for signal processing with time measuring device between instant of intersection by object of those photo-relay barriers. Each photo-relay barrier is arranged as emitter of light with ray with thickness h. The ray is directed through line of flight of object at angle a to it of system of (2n-1) mirrors parallel to line of flight of object for representation of ray in plane of line of flight of object with intersection of the line n times at angle a.
6. Useful Model Patent № 59216, МПК G01N 3/30, G01N 3/02. DEVICE FOR A HAMMER SPEEDUP OF / Astanin Viacheslav Valentynovych (UA); Schehel Hanna Oleksiivna (UA); applicant and patentholder National Aviation University. - № u201011898; filed 07.10.2010; issued 10.05.2011. Bul. №9.
Device for speedup of hammer has combustion chamber, block for supply of working gases to combustion chamber, block for initiation of working gas mix, tube of hammer speedup, block of controller of pressure on hammer. Combustion chamber is arranged as cylindrical with back and front ends as hemi-spheres and placed as axis of cylinder at side of the back end channel of block for supply of working gases and at side of the front end channel for discharge of high pressure combustion products to block of pressure on hammer controller and then to tube of hammer speedup. Element of initiation of block for initiation of working gas mix is brought into coincidence with channel for supply of working gas burning mix and is arranged in such way that ignition spark is formed in geometric center of hemi-spherical back end of combustion chamber.
7. Useful Model Patent № 59217, МПК G01N 3/30, G01N 3/02. DEVICE FOR ACCELERATION OF HAMMER WITH EVAPORATOR / Astanin Viacheslav Valentynovych (UA); Schehel Hanna Oleksiivna (UA).; applicant and patentholder National Aviation University. - № u201011899; filed 07.10.2010; issued 10.05.2011. Bul. №9.
Device for speedup of hammer with evaporator has combustion chamber, block for supply of working gases to combustion chamber, block for ignition of working gas mix, hammer speedup tube, block of pressure on hammer controller. Block for supply of working gases to combustion chamber is arranged with channel for supply of vapor of liquid fuel from evaporator realized as high pressure flask with three channels.
8. Useful Model Patent № 59218, МПК G01N 3/30, G01N 3/02. DEVICE FOR HAMMER SPEEDUP WITH FORECHAMBER / Astanin Viacheslav Valentynovych (UA); Schehel Hanna Oleksiivna (UA); applicant and patentholder National Aviation University. - № u201011900; filed 07.10.2010; issued 10.05.2011. Bul. №9.
Device for speedup of hammer with forechamber has combustion chamber, block for supply of working gases to combustion chamber, block for ignition of working gas mix, tube of hammer speedup, block of pressure controller on hammer. Combustion chamber is connected to additional forechamber equipped with separate channel for supply of working gases and separate element for ignition of working gas mix, with possibility of reagent inflow in process of reaction of burning from forechamber to combustion chamber.
9. Useful Model Patent № 59219, МПК G01N 3/30. METHOD FOR NON-DESTRUCTIVE CONTROL OF STRENGTH OF MATERIAL / Astanin Viacheslav Valentynovych (UA); Schehel Hanna Oleksiivna (UA).; applicant and patentholder National Aviation University. - № u201011901; filed 07.10.2010; issued 10.05.2011. Bul. №9.
Method for non-destructive control of strength of material through analysis of parameters of electromagnetic signals brought to existence in material through mechanical impact loading and amplitude-frequency characteristics of those, at which analysis of parameters is carried out for series of registered electromagnetic signals and amplitude-frequency characteristics of those obtained in separate studies, in each of those mechanical impact load is realized by hammer of same mass and form at values of kinetic energy of hammer differing from previous values through setting respective values of its initial velocity.
10. Useful Model Patent № 59220., МПК G01N 27/72, G01N 3/30. DEVICE FOR DETERMINATION OF PARAMETERS OF ELECTROMAGNETIC EMISSION OF MATERIALS / Astanin Viacheslav Valentynovych (UA); Schehel Hanna Oleksiivna (UA); applicant and patentholder National Aviation University. - № u201011902; filed 07.10.2010; issued 10.05.2011. Bul. №9.
Device for determination of parameters of electromagnetic emission of materials includes block for registration of change of parameters of electromagnetic field and block for amplification of registered signal. Device is arranged with block for processing and storage of data obtained, block for control of device, power supply block. Block for registration of change of parameters of electromagnetic field is arranged as completed with block for setting initial magnetic field formed with source of direct magnetic field for provision of dominant orientation of electromagnetic radiation of material.
11. Useful Model Patent № 59221, МПК G01N 3/30, G01N 3/02. MOVABLE DEVICE FOR HAMMER SPEEDUP WITH CONTROL OF VELOCITY / Astanin Viacheslav Valentynovych (UA); Schehel Hanna Oleksiivna (UA); applicant and patentholder National Aviation University. - № u201011903; filed 07.10.2010; issued 10.05.2011. Bul. №9.
Movable device for speedup of hammer with control of velocity has combustion chamber, block for supply of working gases to combustion chamber, block for ignition of working gas mix, tube for speedup pf hammer, block of controller of pressure on hammer, block for determination of velocity of hammer. Combustion chamber, block of pressure on hammer controller, tube for speedup of hammer and block for determination of velocity of hammer are rigidly connected to each other and together with block for supply of working gases to combustion chamber and block for ignition of working gas mix are arranged with additional block of remote control of processes of speedup of hammer and control of parameters of operation of the device, information processing and provision of communication with computer, and block for power supply with built-in accumulator with possibility of provision of completely functional autonomous operation of the device, placement on movable platform arranged as semi-trailer of a car-tractor with wheel supports and block for linkage with car-tractor.
12. Useful Model Patent № 59387, МПК В64С 23/00. PILOTLESS AIRCRAFT / Kharchenko Volodymyr Petrovych (UA); Pereverziev Oleksandr Mykhailovych (UA); Sviaschenko Yurii Ivanovych (UA); Pasichnyk Viktor Oleksandrovych (UA); applicant and patentholder National Aviation University. - № u201013626; filed 16.11.2010; issued 10.05.2011. Bul. №9.
A pilotless aircraft comprises a fuselage, a wing in the middle part of the fuselage, an empennage behind the fuselage, an engine mounted above the fuselage and wing. The part of fuselage located in front of the wing is made in the form of a front part of wing of ultra-low elongation.
13. Useful Model Patent № 59443, МПК G01M 15/00. METHOD FOR DETERMINATION OF JET THRUST OF GTE IN FLIGHT / Volianska Larysa Heorhiivna (UA); Kulyk Mykola Serhiiovych (UA); Panin Vladyslav Vadymovych (UA); Tereschenko Yurii Matviiovych (UA); applicant and patentholder National Aviation University. - № u201014722; filed 08.12.2010; issued 10.05.2011. Bul. №9.
Method for determination of jet thrust of GTE in flight through measurement of pressure of outer air, area of outlet cross section of jet nozzle and total pressure behind compressor of the engine. One measures instantaneous flow rate of fuel, total temperature of outflow gases and velocity of flight, and jet thrust is determined by formula.
14. Useful Model Patent № 59534, МПК Н03М 13/31. SYSTEMS FOR STATIC FUNCTIONS OF MAKING DECISION IN IDENTIFICATION TASKS OF FULL CODE CONSTRUCTION WITH WEAKLY DISTINCTIVE PARAMETERS / Yudin Oleksandr Kostiantynovych (UA); Lutskyi Maksym Heorhiiovych (UA); Chunariova Anna Vadymivna (UA); Kurin’ Kseniia Oleksandrivna (UA); applicant and patentholder National Aviation University. - № u201010898; filed 10.09.2010; issued 25.05.2011. Bul. №10.
A system for statistic functions of making decision in tasks of code construction with distinctive parameters comprises calculating unit for information sufficient minimum and form thresholds with Kotelnikov, Baies, Fisher, Kulbaka classic criteria. A direct Fourier transformation unit is incorporated; determination of the most informative components of signals and formation of decision threshold is made depending on input set of code constructions and the selected function taking into account the applied requirements and criteria.
15. Useful Model Patent № 59726, МПК A01D 25/04. WORKING ELEMENT FOR DIGGING TUBEROUS ROOTS / Yurchuk Volodymyr Petrovych (UA); Volokha Mykola Petrovych (UA); Bashta Olena Tryfonivna (UA); Volokha Vladyslav Mykolaiovych (UA); Boldyrieva Larysa Vladyslavivna (UA); applicant and patentholder National Aviation University. - № u201013625; filed 16.11.2010; issued 25.05.2011. Bul. №10.
A working element for digging tuberous roots comprises two paired disks, arranged at angle to each other, and a transporting unit made as a screw with winding. Said transporter is disposed along the longitudinal symmetry axis of the working element. A winding space of the transporting screw is reduced in the direction from the centre of the disks to periphery thereof.
16. Useful Model Patent № 59787, МПК G01N 3/30, G01N 3/02. INSTALLATION "aSTanin-3d" FOR STUDY OF IMPACT STRENGTH WITH THREE-DIMENSIONAL CONTROL OF PROCESS OF COLLISION / Astanin Viacheslav Valentynovych (UA); Schehel Hanna Oleksiivna (UA); applicant and patentholder National Aviation University. - № u201014721; filed 08.12.2010; issued 25.05.2011. Bul. №10.
Installation "aSTanin-3d" for study of impact strength with three-dimensional control of process of collision includes device for acceleration of striker and pendulum for fixation and registration of pulse of object under investigation. Pendulum is arranged with possibility of rotation of object under investigation studied with respect to three axles of rectangular Cartesian coordinate system accepted and with indicators for registration with provision of transfer from those to block for control, power supply and analysis of information data on value of deflection of fixed object under investigation from initial position at motion separately with respect to each of those axles in time, besides that it is equipped with chip track, and device for acceleration of hammer is fit by device for determination of velocity of hammer placed with respect to it at the side of placement of object under investigation at axis of the flight hammer.
17. Useful Model Patent № 60376, МПК G01S 13/52. METHOD FOR DETECTION OF MOVABLE TARGETS WITH PULSE LOCATOR / Omelchuk Ihor Pavlovych (UA); Prokopenko Ihor Hryhorovych (UA); applicant and patentholder National Aviation University. - № u200907995; filed 29.07.2009; issued 25.06.2011. Bul. №12.
Method for detection of movable targets with pulse locator is in fact that one separates complex envelope for received reflected from targets radar signals, with its transformation to digital complex readings of which range strobes are formed, with determination of modules of differences between readings, with adding those, the result is compared to threshold value that is set on basis of needed probability of error detection of target, with making decision on detection of target at exceeding the threshold value. Additionally in each range strobe that is restricted with sequence N of complex readings reflected from one radio-location volume one measures frequency F of harmonic component of the sequence of complex readings, and modules of differences are determined for pairs of complex readings that are separated one from another with same time interval, value of this one is determined by measured frequency.
18. Useful Model Patent № 60390, МПК G06G 7/30, G05B 13/02, G05B 15/02. COMPUTER NETWORK NONSTATIONARY TRAFFIC DIGITAL OPTIMAL EXTRAPOLATOR / Huzii Mykola Mykolaiovych (UA); Andreiev Oleksandr Volodymyrovych (UA); Ihnatov Volodymyr Oleksiiovych (UA); Andreiev Volodymyr Illich (UA); applicant and patentholder National Aviation University. - № u201006549; filed 28.05.2010; issued 25.06.2011. Bul. №12.
The optimal computer network nonstationary traffic extrapolator comprises traffic monitoring system and a traffic measurement block. Herewith several previous measurements of a nonstationary traffic noisy signal envelope with apriori known probabilistic characteristics (mathematical expectations, dispersions, signal correlation functions and interfering signals) are used, at the bottom of optimal extrapolator building is put determination of optimal predicted (extrapolated) values of random nonstationary traffic against the background of interfering by minimum error dispersion criterion. The optimal extrapolator has a database, a timer, a control unit and a synchronizer, an evaluator, an indication unit.
9. Useful Model Patent № 60391, МПК G06F 7/38. ARITHMETICAL UNIT / Zhukov Ihor Anatoliiovych (UA); Krasovska Yevheniia Viktorivna (UA); Synelnikov Oleksii Oleksiiovych (UA); applicant and patentholder National Aviation University. - № u201006810; filed 02.06.2010; issued 25.06.2011. Bul. №12.
The arithmetical unit comprises an OR element for two inputs, decipher carry units, beginning number shaping units, switching units, digit-by-digit arithmetic units, a jiggling unit, a carry shaping unit, an OR element unit, a result shaping unit, beginning number recognition units.
20. Useful Model Patent № 60392, МПК A61B 5/02. device for high-speed measurement of blood pressure / Zudov Oleh Mykolaiovych (UA); applicant and patentholder National Aviation University. - № u201006811; filed 02.06.2010; issued 25.06.2011. Bul. №12.
Device for high-speed measurement of blood pressure comprises a compression cuff with a compressor and pressure sensor, which covers a hand during measurement and below the cuff at the arm the first pulse sensor is installed and on another hand the second probe pulse is installed, and a signal processing unit. The signal processing unit further comprises a bandpass filter that simulates the frequency response of the vascular bed.
21. Useful Model Patent № 60393, МПК F04F 5/00. METHOD FOR RENEWAL OF WORKING CAPACITY OF REPAIR GEAR-TYPE LUBRICATION HYDRO-PUMPS / Klimin Volodymyr Volodymyrovych (UA); Kindrachuk Miroslav Vasyliovych (UA); Herasimova Olha Viacheslavivna (UA); Kostin Valerii Anatoliiovych (UA); Klimina Yulia Volodymyrivna (UA); Podlesnyi Vadym Vitaliiovych (UA); Perro Daryna Mykolaivna (UA); applicant and patentholder National Aviation University. - № u201006816; filed 02.06.2010; issued 25.06.2011. Bul. №12.
A method for renewal of working capacity of worked-out repair gear-type lubrication hydro-pumps includes production of body parts, removal with finishing grinding of wear defects of working cylindrical surfaces and ends of toothed crowns of pinion shafts at restoration of module of engagement. At that with grinding one renews involute shape of worn profiles as well.
22. Useful Model Patent № 60394, МПК Н03М 13/00. METHOD FOR SPECTRAL DETERMINATION OF SIGNAL INFORMATION COMPONENTS IN PROCEDURES INFORMATION AMBIGUITY REMOVAL / Yudin Oleksandr Kostiantynovych (UA); Lutskyi Maksym Heorhiiovych (UA); Chunariova Anna Vadymivna (UA); Kurin’ Kseniia Oleksandrivna (UA); applicant and patentholder National Aviation University. - № u201006817; filed 02.06.2010; issued 25.06.2011. Bul. №12.
A method for spectral determination of signal informative components in order to create decision rule comprises uncertainty function of spectral representation of code words that further uses to create mathematical procedure of decision making in order to enhance generalized measure of information quantity.
23. Useful Model Patent № 60395, МПК F04D 19/00, F04D 29/66. METHOD FOR REDUCING OF FAN NOISE / Tereschenko Yurii Matviiovych (UA); Kinaschuk Ihor Fedorovych (UA); Doroshenko Kateryna Viktorivna (UA); Markovska Liubov Heorhiivna (UA); applicant and patentholder National Aviation University. - № u201006818; filed 02.06.2010; issued 25.06.2011. Bul. №12.
A method for reducing of level of fan noise includes affecting flow by means of change of fan design. Blades of fan are placed in sectors in 2-4 blades with constant separation between sectors. Separation of blades in sector is smaller compared to that between sectors.
24. Useful Model Patent № 60394, МПК Н03М 13/00. METHOD FOR SPECTRAL DETERMINATION OF SIGNAL INFORMATION COMPONENTS IN PROCEDURES INFORMATION AMBIGUITY REMOVAL / Yudin Oleksandr Kostiantynovych (UA); Lutskyi Maksym Heorhiiovych (UA); Chunariova Anna Vadymivna (UA); Kurin’ Kseniia Oleksandrivna (UA); applicant and patentholder National Aviation University. - № u201006817; filed 02.06.2010; issued 25.06.2011. Bul. №12.
A method for spectral determination of signal informative components in order to create decision rule comprises uncertainty function of spectral representation of code words that further uses to create mathematical procedure of decision making in order to enhance generalized measure of information quantity.
25. Useful Model Patent № 60395, МПК F04D 19/00, F04D 29/66. METHOD FOR REDUCING OF FAN NOISE / Tereschenko Yurii Matviiovych (UA); Kinaschuk Ihor Fedorovych (UA); Doroshenko Kateryna Viktorivna (UA); Markovska Liubov Heorhiivna (UA); applicant and patentholder National Aviation University. - № u201006818; filed 02.06.2010; issued 25.06.2011. Bul. №12.
A method for reducing of level of fan noise includes affecting flow by means of change of fan design. Blades of fan are placed in sectors in 2-4 blades with constant separation between sectors. Separation of blades in sector is smaller compared to that between sectors.
26. Useful Model Patent № 60398, МПК G06F 15/16. MULTIPROCESSOR / Zhukov Ihor Anatoliiovych (UA); Klymenko Iryna Anatoliivna (UA); Biliaiev Serhii Mykolaiovych (UA); applicant and patentholder National Aviation University. - № u201007467; filed 15.06.2010; issued 25.06.2011. Bul. №12.
The multiprocessor comprises peripheral devices and processor modules connected between them with a common bus consisting of each of which includes a processor and peripheral devices integrated by a local bus. As a part of each priority interruption controller unit a group header, group footer flip-flop, a group header controller, a group footer controller, a priority interruption controlled, a group footer controller, a program interface is introduced.
27. Useful Model Patent № 60399, МПК С21D 1/10, С21D 1/18, С21D 7/13, С21D 8/10, С21D 9/08, В21D 7/028. METHOD for INCREASING DURABILITY OF STEEL thick-walled CYLINDRICAL PARTS / Klimin Volodymyr Volodymyrovych (UA); Kindrachuk Miroslav Vasyliovych (UA); Didenko Oleksandr Leonidovych (UA); applicant and patentholder National Aviation University. - № u201007468; filed 15.06.2010; issued 25.06.2011. Bul. №12.
A method for increasing the durability of steel thick-walled cylindrical parts includes plastic deformation, machining,carbonisation, hardening and low temperature backing. The wear resistance is increased by improving the entire set ofcharacteristics of the mechanical properties of the metal, changing the original coarse-grained heterogeneous structure of the material piece into microstructure of fine-grained structure, for which the workpiece is heated by microwave to a temperature of 900 ÷ 1050 °C and it is expanded with the conical mandrel to the breaking-down of the material by a surface of matrix operational volume. The conicity of the come in part of the mandrel is equal to the 3°. The speed of the mandrel movement is of 0.3 ÷ 0.5 m/s, the relative deformation of the workpiece is of 2.5 ÷ 3.0%. To create the conditions of the breaking-down of the material piece the sizing part of the mandrel is increased by 2.0 ÷ 2.5% of its estimated value for providing of a givenvalue of relative deformation.
28. Useful Model Patent № 60400, МПК Н04В 7/005. DEVICE FOR QUALITY ENHANCEMENT OF DATA TRANSMISSION IN WIRELESS NETWORKS OVER INTERMITTENT RECEPTION ZONES OR WITH INSUFFISIENT NOISE IMMUNITY / Dudnik Andrii Serhiiovych (UA); Shevtzova Yevheniia Valeriivna (UA); Yatzenko Mykola Mykolaiovych (UA); Zubareva Olena Oleksandrivna (UA); applicant and patentholder National Aviation University. - № u201007469; filed 15.06.2010; issued 25.06.2011. Bul. №12.
A device for quality enhancement of data transmission in wireless networks in intermittent reception zones or with insufficient noise immunity comprises a controller. The controller generates a messages comprising signal quality information comprises the main unit – a signal analyzer which using data of physical level interface OSI allows a control device located at the network level OSI to make decision as to changing transmission condition, if necessary.
29. Useful Model Patent № 60401, МПК B64D 1/00. METHOD OF AERODYNAMIC ADJUSTING FLIGHT OF FREE-FALLING CONTAINER USING SATELLITE NAVIGATION SIGNALS / Kovryzhkin Oleh Heorhiiovych (UA); Kovryzhkin Ihor Olehovych (UA); Horin Ivan Yaroslavovych (UA); Lahuta Andrii Hennadiiovych (UA); Melnykovych Volodymyr Borysovych (UA); applicant and patentholder National Aviation University. - № u201007471; filed 15.06.2010; issued 25.06.2011. Bul. №12.
A method for adjusting a trajectory of a free-falling container using satellite navigation signals includes coordinate assignment of the point of container delivery, the container release from an aircraft, determination of the current coordinates of container using a satellite navigation system. Assignment of the coordinates of container delivery, such as geographic latitude lat, geographic longitude λlong and altitude Ha of location of a container above earth geoid is carried out by a unit for entry of the coordinates of delivery point of container with subsequent, after release of the container from the aircraft, sending it to a onboard digital computer, into which current coordinates of falling container are also sent from the satellite navigation system, in particular the current coordinates of latitude , longitude λ and altitude H of location of container above earth geoid, and from an angular velocity sensor - signal of change of angular velocity of rotation x of container, while using the onboard digital computer based on the values of assigned coordinates of the delivery point of container lat, λlong and Ha and current coordinates of the container , λ and H taking into account the signal of change of angular velocity of the container x the signal is formed of control of rudders of falling, which is sent to a control unit of aerodynamic rudders, and when the value of current height H of the container above the earth geoid is reached that is equal to the assigned value Ha, a signal of parachute opening is sent, in the case a receiver antenna of satellite navigation system is located in the rear (tail) part of the container to avoid shielding of signals from satellites by the container casing.
30. Useful Model Patent № 60405, МПК G01M 13/04. DEVICE FOR VIBRO-DIAGNOSTICS OF BEARING UNITS / Ornatskyi Dmytro Petrovych (UA); Dovhan Vasyl Volodymyrovych (UA); applicant and patentholder National Aviation University. - № u201008439; filed 06.07.2010; issued 25.06.2011. Bul. №12.
Device for vibro-diagnostics of bearing units includes connected in series vibro-measuring transformer and amplifier, and filter output of which is connected to block for determination of average square value of amplitudes and first amplitude detector output of which through divider is connected to indicator, device is equipped with block of auto-normalization, second amplitude detector, four controlled narrow-band filters, indicator of frequency of rotation and switch, at that the block of auto-normalization is connected between the amplifier and filter, information inputs of controlled narrow-band filters are connected to output of amplitude detector, control inputs – to indicator of frequency of rotation, and outputs through switch and connected to it in series second amplitude detector – to second input of divider. Device is as well equipped with frequency divider included between the output of tachometer and control input of high-speed barrier synchronous filter input of which is connected to output of multiplexer, and output through connected in series low frequency filter, first quadrator, first block of weight function, first integrator – to the first output of divider second output of which is connected to input of second integrator, input of integrator is connected to input of second block of weight function and its input is connected to output of second quadrator input of which is connected to output of multiplexer.
31. Useful Model Patent № 60419, МПК G06M 19/00. HARDWARE AND SOFTWARE COMPLEX FOR VERIFICATION OF USERS ACCURACY COORDINATES / Konin Valerii Viktorovych (UA); Maliutenko Tetiana Leonidivna (UA); Melkumian Valter Gaikovych (UA); Pohurelskyi Oleksii Serhiiovych (UA); Prykhodko Iryna Anatoliivna (UA); Sushko Oleksii Petrovych (UA); applicant and patentholder National Aviation University. - № u201010902; filed 10.09.2010; issued 25.06.2011. Bul. №12.
The hardware and software complex for verification of user’s accuracy coordinates comprises a receiver for obtaining information from navigation satellites to be input in an information-processing device and appears in a display. The complex has a unique program for verification of navigation data in the problem-solving environment MatLab and has the opportunity to operate not only with navigation system GPS but also operates with navigation system GLONASS.
32. Useful Model Patent № 60974, МПК G01S 5/14. METHOD FOR CONTROL OF INTEGRITY OF SATELLITE NAVIGATION SYSTEM IN CONTROL-CORRECTION STATION / Konin Valerii Viktorovych (UA); Kovalenko Eduard Oleksandrovych (UA); Kutsenko Oleksandr Viktorovych (UA); applicant and patentholder National Aviation University. - № u201010907; filed 10.09.2010; issued 25.06.2011. Bul. №12.
Method for control of integrity of satellite navigation system in control-correction station includes measurement of radio-navigation parameters (quasi-distances) by signals from N navigation satellites (main channel), formation of combinations of massifs of quasi-distances with exclusion of massif of quasi-distance to i-th navigation satellite (additional channels), solution of navigation problem with determination of coordinates of user by main and additional channels, formation of test statistics as difference of coordinates determined and making decision on presence or absence of failure of navigation satellite through comparison to threshold. In each combination of massifs of quasi-distances in additional channels instead of quasi-distance to i-th navigation satellite included distance calculated by known coordinates of i-th navigation satellite and used is added, and test statistics is formed through averaging differences determined in main and additional channels of coordinates of user by several different measurements.
33. Useful Model Patent № 62862, МПК В64С 25/00. UNMANNED AIRCRAFT / Kharchenko Volodymyr Petrovych (UA); Sviaschenko Yurii Ivanovych (UA); applicant and patentholder National Aviation University. - № u201006812; filed 02.06.2010; issued 25.06.2011. Bul. №12.
An unmanned aircraft comprises a wing profile of given curvature with ribs, a flap, a release truck of chassis with a spring-damper, wheels. The flap is rigidly connected to longitudinal elements fastened on the spring-damper, and on the top of flap under the ribs of wing fins are installed that reproduce the curvature of wing rib by its upper part.
34. Useful Model Patent № 62874, МПК Н03М 13/00. DEVICE FOR DECODING SINGLE NONBINARY ERRORS USING SERIAL CODE ALGORITHM / Zhukov Ihor Anatoliiovych (UA); Kubytskyi Valerii Ivanovych (UA); Synelnikov Oleksii Oleksiiovych (UA); applicant and patentholder National Aviation University. - № u201014713; filed 08.12.2010; issued 26.09.2011. Bul. №18.
A device for decoding single nonbinary errors relates to computing engineering and can be used in coders and decoders of cyclic codes used for transmission of messages with high adequacy, in discrete information delivery and processing systems.
35. Useful Model Patent № 62875, МПК Н03М 13/00. DEVICE FOR DECODING SINGLE NONBINARY ERRORS / Zhukov Ihor Anatoliiovych (UA); Kubytskyi Valerii Ivanovych (UA); Synelnikov Oleksii Oleksiiovych (UA); applicant and patentholder National Aviation University. - № u201014714; filed 08.12.2010; issued 26.09.2011. Bul. №18.
A device for decoding single nonbinary errors relates to computing engineering and can be used in coders and decoders of cyclic codes used for transmission of messages with high adequacy, in discrete information delivery and processing systems.
36. Useful Model Patent № 62876, МПК G09B 9/00. LEVEL DETECTION METHOD FOR INDICATION CONFORMITY OF FLIGHT INDICATOR TO PSYCHOPHISILOGICAL POSSIBILITIES OF AIR CRAFT AVIATOR FOR ITS PERCEIVING/ Skrypets Andrii Vasyliovych (UA); Hryschenko Yurii Vitaliiovych (UA); Hulenko Viktoria Dmytrivna (UA); Volkov Oleksandr Yevheniiovych (UA); Volosheniuk Dmytro Oleksnadrovych (UA); applicant and patentholder National Aviation University. - № u201014715; filed 08.12.2010; issued 26.09.2011. Bul. №18.
A level detection method for indication conformity of a flight indicator to psychophysiological possibilities of aircraft aviators for its perceiving relates to the branch of aviation, aircraft employment in terms of methods to determine performance ability and competence of aviators to walk up to the trough under action of factor blunders and allows prevent aircraft accidents through the fault of human factors namely type mismatch of flight indicator indication to concrete operator (aviator).
37. Useful Model Patent № 62877, МПК G01N 3/56. METHOD FOR RENEWAL OF FRICTION SURFACE IN PULSE MAGNETIC FIELD BY MEANS OF MODULATED SIGNAL / Svyryd Mykhailo Mykolaiovych (UA); Kravets Ivan Andriiovych (UA); Zadniprovska Svitlana Mykolaivna (UA); Volosovych Heorhii Andriiovych (UA); Borodii Viktor Mykolaiovych (UA); applicant and patentholder National Aviation University. - № u201014717; filed 08.12.2010; issued 26.09.2011. Bul. №18.
Method for renewal of friction surface in pulse magnetic field by means of modulated signal is in fact that one affects the particles of material with which friction surface is renewed with magnetic force lines of a pulse magnetic field. Current with frequency 50 Hz that forms magnetic field is switched with frequency 5-15 Hz, and besides that is it rectified.
38. Useful Model Patent № 62878, МПК G06C 3/00, G01S 17/00. METHOD FOR TWO-PARAMETER OPTIMUM EXTRAPOLATION OF NONSTATIONARY RANDOM SIGNAL AGAINST THE BACGROUND OF HINDRANCES / Ihnatov Volodymyr Oleksiiovych (UA); Zhukov Ihor Anatoliiovych (UA); Andreiev Oleksandr Volodymyrovych (UA); Andreev Volodymyr Illich (UA); applicant and patentholder National Aviation University. - № u201014719; filed 08.12.2010; issued 26.09.2011. Bul. №18.
A method for two-parameter optimum extrapolation of nonstationary random signals against the background of hindrances, where for an optimum extrapolation of nonstationary random signal against the background of hindrance is used a maximum likelihood method as well as several preceding measurement results of a noisy signal with a priori known probabilistic characteristics (mathematical expectations, dispersions, signal correlation functions and hindrances). At the heart of the method is put the task of determination of optimum predicted (extrapolated) value of a nonstationary random signal against the background of hindrance by minimum dispersion of extrapolation error.
39. Useful Model Patent № 62926, МПК А61В 5/00. METHOD FOR RAPID MEASUREMENT OF BLOOD PRESSURE / Zudov Oleh Mykolaiovych (UA); applicant and patentholder National Aviation University. - № u201100935; filed 28.01.2011; issued 26.09.2011. Bul. №18.
A method for rapid measurement of blood pressure relates to medical diagnostic equipment. The technical result of the utility model is to improve the accuracy of simulation by limiting the pulse wave with compression cuff.
40. Useful Model Patent № 62927, МПК В01F 5/00. CAVITATION METER-MIXER / Hlazkov Mykhailo Mykhailovych (UA); Boichenko Serhii Valeriiovych (UA); Badakh Valerii Mykolaiovych (UA); Lanetskyi Vasyl Hryhorovych (UA); Netreba Volodymyr Petrovych (UA); applicant and patentholder National Aviation University. - № u201100936; filed 28.01.2011; issued 26.09.2011. Bul. №18.
A cavitation meter-mixer comprises a housing, a nozzle of convergent-divergent type with a needle orifice in the convergent part and a diaphragm with throttle. The nozzle has a stepped convergent pipe, a cylindrical part and a stepped divergent part and the diaphragm is designed as a bellows with a hole in the top.
41. Useful Model Patent № 62928, МПК G01В 21/06. DEVICE FOR MEASUREMENT OF VALUE OF LINEAR WEAR WITHOUT MACHINE STOPPING / Zaporozets Volodymyr Vasyliovych (UA); Stadnychenko Viacheslav Mykolaiovych (UA); Stadnychenko Mykola Hryhorovych (UA); Tokaruk Vitalii Volodymyrovych (UA); applicant and patentholder National Aviation University. - № u201100937; filed 28.01.2011; issued 26.09.2011. Bul. №18.
Device for measurement of value of linear wear without stopping machine has profile, standpipe, body with precision hydro-bearings of lever the end of which rests at gear mechanism rod type that at change of position of the lever transforms rotation of the lever to translational motion of the rod that is rigidly connected through connection clutch to axis of rotation of measuring head. Device is fixed to the trolley of the friction machine this makes it possible to prevent distortion of the results of measurements from beats of the body of friction machine. Use as measuring head of indicator of angle-encoder makes it possible to implement transformation of linear displacement of the lever to angular displacement of encoder at measurement of linear wear through transformation of angle of turn of the shaft that rotates to electric signals that by respective interface come to personal computer in which by means of respective software one obtains values of linear wear.
42. Useful Model Patent № 62929, МПК В64С 39/02. MULTIPURPOSE TWIN-ENGINE UNMANNED AIRCRAFT / Kulyk Mykola Serhiiovych (UA); Kharchenko Volodymyr Petrovych (UA); Matiichyk Mykhailo Petrovych (UA); Makarchuk Maksym Vytaliiovych (UA).; applicant and patentholder National Aviation University. - № u201100938; filed 28.01.2011; issued 26.09.2011. Bul. №18.
A multipurpose twin-engine unmanned aircraft has two engines, a wing, a fixed container for on-board special equipment. The wing is made trapezoidal in plan with mechanization in the form of a slot flaperon, two sections of Fowler's flap and two sections of slats and is installed on one split central pylon. Power systems are installed on the center wing section. An empennage is twin-fin H-shaped and is mounted on a demountable tail boom. For takeoff/landing as an aircraft a three-support landing gear with a nose self-oriented support is installed and a payload container is combined with the fuselage nacelle.
43. Useful Model Patent № 63122, МПК Н04К 1/00. METHOD FOR INCREASE OF RATE AND PRIVACY OF INFORMATION TRANSMISSION / Kuts Yurii Vasyliovych (UA); Hopienko Andrii Volodymyrovych (UA); Monchenko Olena Volodymyrivna (UA); Yeremenko Volodymyr Stanislavovych (UA); applicant and patentholder National Aviation University. - № u201103436; filed 23.03.2011; issued 26.09.2011. Bul. №18.
A method for increase of rate and privacy of information transmission consists in shaping information carrier using an information signal, the information carrier is modulated with a time-limited signal, and Gilbert transformation is performed for a received signal. Received messages are shaped according parameters of differential signal phase characteristics of received signal and unmodulated signal. The signal is modulated by multiplication it and amplitude characteristics thereof, modulated signal phase characteristic is obtained. The received signal is shaped as difference between modulated an unmodulated carriers.
44. Useful Model Patent № 63123, МПК G01M 15/00. THREE-FLOW UPRATED TURBOJET ENGINE / Tereschenko Yurii Matviiovych (UA); Volianska Larysa Heorhiivna (UA); Kulyk Mykola Serhiiovych (UA); Panin Vladyslav Vadymovych (UA); Tereschenko Yurii Yuriiovych (UA); applicant and patentholder National Aviation University. - № u201103438; filed 23.03.2011; issued 26.09.2011. Bul. №18.
Three-circuits uprated turbojet engine includes input device, gas generator, ventilator of back arrangement with blade stages and turbine of drive of the ventilator that together form a turboventilator attachment, outer circuit, reactive nozzle, mixing chamber. Between the mi9xing chamber of gas generator and the turbine of turbo ventilator attachment afterburner is placed.
45. Useful Model Patent № 63124, МПК B64C 3/38. UNMANNED AIRCRAFT / Kharchenko Volodymyr Petrovych (UA); Sviaschenko Yurii Ivanovych (UA); Korcheniuk Viacheslav Pavlovych (UA); applicant and patentholder National Aviation University. - № u201103441; filed 23.03.2011; issued 26.09.2011. Bul. №18.
An unmanned aircraft comprises a wing with a center wing section and detachable parts, inner and outer sections of ailerons with an anti-flutter load weight on toes of their ribs. The anti-flutter load is made in the form of a drive-connector unit of aileron sections. The drive-connector unit is designed in the form of two elements set out on the ribs of aileron sections located side by side. In the case one element has a groove with parallel walls, and the second element has a tooth that is slid fit into the slot, and the groove is directed along the aileron chord and on the axis of its rotation.
46. Useful Model Patent № 63125, МПК B64C 3/00, B64C 21/00. UNMANNED AIRCRAFT / Kharchenko Volodymyr Petrovych (UA); Pereverziev Oleksandr Mykhailovych (UA); Sviaschenko Yurii Ivanovych (UA); Korcheniuk Viacheslav Pavlovych (UA).; applicant and patentholder National Aviation University. - № u201103446; filed 23.03.2011; issued 26.09.2011. Bul. №18.
An unmanned aircraft has a wing, an empennage, a fuselage in the form of a wing of ultra-low extension with a tip with a drive, with a ventral ridge, an engine mounted on a pylon above the fuselage with a rotary driven nozzle which shape is close to a circular shape. The nozzle section has a guide portion from below and the nozzle is made rotary up to connection along the straight guiding portion of nozzle section with the fuselage. The nozzle drive is made in the form of a cowling of the tail portion of pylon. The drive of tip is located in the ventral ridge.
47. Useful Model Patent № 63174, МПК G01R 29/08. DETECTOR OF HARMFUL ELECTROMAGNETIC RADIATION / Konakhovych Heorhii Fylymonovych (UA); Konakhovych Anna Serhiivna (UA); Odarchenko Roman Serhiiovych (UA); applicant and patentholder National Aviation University. - № u201105000; filed 20.04.2011; issued 26.09..011. Bul. №18.
Detector of harmful electromagnetic radiation includes antenna device to output of which preliminary power amplifier is connected, those are followed by band filters F1-Fn to outputs of which power amplifiers K1-Kn are connected, then there go integrators I1-In, those are combined to an adder, after that one output of the level of equivalent harmful electromagnetic radiation to display takes place. There are included power amplifiers K1-Kn with variable coefficients of amplification for different frequency ranges that make it possible to divide electromagnetic radiation by level of its harmful effect on human organism and thus to determined level of harmful of organism of human person electromagnetic radiation.
48. Useful Model Patent № 64834, МПК F16H 21/00. METHOD FOR KINEMATICAL ANALYSIS OF A LINK MECHANISM / Zubaschenko Heorhii Pavlovych (UA); Korchenko Oleksandr Hryhorovych (UA); Aleinikova Natalia Vasylivna (UA); applicant and patentholder National Aviation University. - № u201103433; filed 23.03.2011; issued 25.11.2011. Bul. №22.
A method for kinematical analysis of a link mechanism is in plotting diagrams of velocities and accelerations and is connected with need in determination of Coriolis acceleration by value and direction. The link mechanism is transformed to equivalent removable four-bar linkage.
49. Useful Model Patent № 64835, МПК H03М 13/31. METHOD FOR COMPRESSION OF BIT IMAGES BASED ON METHOD OF WIGHT CODING / Yudin Oleksandr Kostiantynovych (UA); Chunariova Anna Vadymivna (UA); Hulak Nataliia Kostiantynivna (UA); Barannik Volodymyr Viktorovych (UA); Skrynnyk Oleksandr Pavlovych (UA); applicant and patentholder National Aviation University. - № u201103434; filed 23.03.2011; issued 25.11.2011. Bul. №22.
A method for compensation of bit images based on methods of weight coding comprises stages for transition to color difference representation of images, discrete-cosine transformation. A non-equilibrium positional coding of bit planes with previous computation of binary series length and computation of code values for non-equilibrium positional figure.
50. Useful Model Patent № 64836, МПК С02F 1/28. METHOD FOR PURIFICATION OF WASTE WATER FROM CHROME (III) COMPOUNDS / Franchuk Hryhorii Mykhailovych (UA); Bovsunovskyi Yevhen Oleksiiovych (UA); Riabchevskyi Oleh Volodymyrovych (UA); Radomska Marharyta Myroslavivna (UA); Madzhd Svitlana Mykhailivna (UA); applicant and patentholder National Aviation University. - № u201103435; filed 23.03.2011; issued 25.11.2011. Bul. №22.
A method for purification of waste water from chrome (III) compounds comprises contacting polluted water with clay material, further mixing and extraction of liquid phase. As sorbent waste of aerosol gas-dynamic suspended treatment of metal surfaces of parts with a chemical composition: (Al2O3); (SiO2); (Fe2O3); (TiO2); (CaO) is used.
51. Useful Model Patent № 64837, МПК С08L 9/10, C08K 13/02. COMPOSITION FOR THE MANUFACTURING CARCASS ELASTOMERIC FOAM / Fabuliak Fedir Hryhorovych (UA); Ostrohrud Andrii Yuriiovych (UA); Maslennikova Liudmyla Dmytrivna (UA); applicant and patentholder National Aviation University. - № u201103437; filed 23.03.2011; issued 25.11.2011. Bul. №22.
A composition for the manufacturing carcass elastomeric foam comprises Revultex® natural rubber latex, mixture of ammonium bicarbonate with aerosil modified with dimethyl chlorosilane.
52. Useful Model Patent № 64838, МПК F03D 3/02, F03D 5/00. COMBINED WIND-DRIVEN POWER UNIT WITH IMPROVED ABILITY / Synehlazov Viktor Mykhailovych (UA); Zelenkov Oleksandr Avramovych (UA); Sochenko Petro Stepanovych (UA); Sydorenko Kostiantyn Mykolaiovych (UA); Holik Artur Petrovych (UA); Molchanov Oleksii Volodymyrovych (UA); Vlasiuk Iryna Ivanivna (UA); applicant and patentholder National Aviation University. - № u201103439; filed 23.03.2011; issued 25.11.2011. Bul. №22.
A combined wind-driven power unit with improved ability includes a vertical axis of rotation installed in rotary bearings in round frame and divided into two parts. To the upper part of the axis of the rotation on spokes of rotary wheels Darrieustype blades are attached. In the Darrieus blades two levels of the Savonius type blades are placed.
53. Useful Model Patent № 64839, МПК В04В 3/00, В01D 17/02. SETTLER FOR REMOVAL OF OIL FROM WASTEWATER / Zubchenko Oleksandr Mykolaiovych (UA); Kovalevska Yuliana Viktorivna (UA); Melnyk Oleksii Mykolaiovych (UA); Zhuk Anna Pavlivna (UA); applicant and patentholder National Aviation University. - № u201103440; filed 23.03.2011; issued 25.11.2011. Bul. №22.
A settler for oil removal from wastewater comprises a cylindrical body with a conical bottom part, a suction hose with an impermeable corrugated wall, an intake pipe, a pipe for removal of sludge, a tap, a pipe for introduction of polluted fluid, "Voyutski fiber". Due to the pressure of labyrinth movement which direction changes by 180 ° and the absence of a pump a higher degree of separation of oil from water is achieved.
54. Useful Model Patent № 64840, МПК В27К 3/34, В27К 5/00. EPOXY DIBUTYL PHTHALATE ADHESIVE / Maslennikova Liudmyla Dmytrivna (UA); Chernykh Svitlana Anatoliivna (UA); Shandruk Maria Ivanivna (UA); Fabuliak Fedir Hryhorovych (UA); applicant and patentholder National Aviation University. - № u201103443; filed 23.03.2011; issued 25.11.2011. Bul. №22.
Epoxy dibutyl phthalate adhesive comprises an epoxy resin, a hardener. As plastifying component it additionally containsdibutyl phtalate.
55. Useful Model Patent № 65003 України, МПК В27К 3/34, В27К 5/00. COMPOUND FOR SOIL STABILIZATION / Maslennikova Liudmyla Dmytrivna (UA); Koshel Oksana Leonidivna (UA); applicant and patentholder National Aviation University. - № u201104983; filed 20.04.2011; issued 25.11.2011. Bul. №22.
A compound for soil stabilization, which is based on a liquid silicate glass, characterized in that in order to reduce thegelatinization time, while improving environmental performance, the compound contains 8 % solution of polyacrylamide.
56. Useful Model Patent № 65004, МПК F04D 19/00, F04D 29/66. DAPTIVE IMPELLER OF AN AXIAL FAN OF A GAS-TURBINE ENGINE / Doroshenko Kateryna Viktorivna (UA); Makarchuk Maksym Vytaliiovych (UA); Tereschenko Yurii Matviiovych (UA); applicant and patentholder National Aviation University. - № u201104985; filed 20.04.2011; issued 25.11.2011. Bul. №22.
An adaptive impeller of an axial fan of a gas-turbine engine with sectional arrangement of blades with constant pitch between the sectors, and at cruising mode of aircraft flight the pitch between the blades in changed to same one.
57. Useful Model Patent № 65006, МПК В60L 11/00, B60K 6/00. DEVICE OF INCREASE OF EFFICIENCY OF REGENERATIVE BRAKING IN ELECTRIC CARS / Synehlazov Viktor Mykhailovych (UA); Zelenkov Oleksandr Avramovych (UA); Sochenko Petro Stepanovych (UA); Sydorenko Kostiantyn Mykolaiovych (UA); Molchanov Oleksii Volodymyrovych (UA); Holik Artur Petrovych (UA); Vlasiuk Iryna Ivanivna (UA); applicant and patentholder National Aviation University. - № u201104989; filed 20.04.2011; issued 25.11.2011. Bul. №22.
A device of increase of efficiency of regenerative braking in electric cars comprises electric motors that are secured on the wheel axles and are able to switch to the mode of electric generators during braking, a battery, an automatic switch of operation modes, and it additionally comprises a high electric capacitance, three automatic switches, switching diodes, and a limiting resistance.
58. Useful Model Patent № 65007, МПК H02N 15/00, H02N 2/00. DEVICE FOR ELECTRIC ENERGY GENERATION USING MECHANICAL OSCILLATIONS / Synehlazov Viktor Mykhailovych (UA); Zelenkov Oleksandr Avramovych (UA); Zubchenko Oleksandr Mykolaiovych (UA); Sochenko Petro Stepanovych (UA); Sydorenko Kostiantyn Mykolaiovych (UA); Molchanov Oleksii Volodymyrovych (UA); Vlasiuk Iryna Ivanivna (UA); applicant and patentholder National Aviation University. - № u201104990; filed 20.04.2011; issued 25.11.2011. Bul. №22.
The invention proposes an apparatus for electric energy generation using mechanical oscillations which is performed via connection a magnet rod to A bow spring of a transport vehicle, as a result oscillations of a magnet relative to inductance coil are obtained, the said coil is fixed to the frame of the vehicle; at the output of the inductance coil electric energy may be taken, electric energy of inductance coil in a damping device increases via formation of resonance contour.
59. Useful Model Patent № 65015, МПК G05B 17/00. CONTROL DEVICE OF LOW-POWERED WIND ENERGY DEVICE GROUP AND SOLAR BATTERIES / Synehlazov Viktor Mykhailovych (UA); Zelenkov Oleksandr Avramovych (UA); Sochenko Petro Stepanovych (UA); Sydorenko Kostiantyn Mykolaiovych (UA); Holik Artur Petrovych (UA); Udovenko Oleksandr Opanasovych (UA); Vlasiuk Iryna Ivanivna (UA); applicant and patentholder National Aviation University. - № u201105002; filed 20.04.2011; issued 25.11.2011. Bul. №22.
The control device of the low-powered wind energy device group and solar batteries comprising a programming electrical generator control unit and a using storage battery system aimed to connect them to a customer. There are n wind energy devices and solar batteries and information of the produced electric energy value for each wind energy device, a solar battery, state of storage battery bridge charge, solar irradiation degree of clarity, availability and wind speed, of electric energy to receive a customer introduced sequentially and regularly through a multiplexer system to a microcontroller where these data are processed according to the program, the data processing results are output according to indicating system and necessary control signals are output through a demultiplexer system for separate wind energy devices, solar batteries and solar batteries, the electric energy produced from specified sources are transferred through controlled from a switch microcontroller system to a consumer.
60. Useful Model Patent № 65018, МПК С25D 15/00. COMPOSITION FOR PRODUCING wear-resistant COMPOSITE electrolytic coatings based on Nickel for operation at the increased temperatures / Kindrachuk Miroslav Vasyliovych (UA); Korniienko Anatolii Oleksandrovych (UA); Fedorchuk Svitlana Volodymyrivna (UA); Luchka Myron Vasyliovych (UA); Perro Daryna Mykolaivna (UA); Podliesnyi Vadym Vitaliiovych (UA); applicant and patentholder National Aviation University. - № u201105006; filed 20.04.2011; issued 25.11.2011. Bul. №22.
A composition for obtaining wear-resistant composite electrolytic coatings based on nickel for work at the increased temperatures also contains nickel chloride, boric acid,granules of heat resistant eutectic alloy, at that it additionally contains nanoparticles of silicon carbide in the amount of 10-30 g/L.
61. Useful Model Patent № 65019, МПК G01N 29/04, G01N 3/56. METHOD FOR DETERMINATION OF TIME OF TEAR TAKING PLACEIN FRICTION UNITS / Filonenko Serhii Fedorovych (UA); Kosmach Oleksandr Pavlovych (UA); Kosytska Tetiana Mykolaivna (UA); applicant and patentholder National Aviation University. - № u201105007; filed 20.04.2011; issued 25.11.2011. Bul. №22.
Method for determination of time of tear taking place in friction units that includes loading of friction unit with simultaneous registration of acoustic emission by characteristics of which one makes conclusions on tear torque in friction unit, at that as the characteristics named above one measures dispersion of total energy of signals of acoustic emission, and instant of tear coming to existence one determines by sudden increase of dispersion of total energy of signals of acoustic emission or sudden increase of rate of its change.
62. Useful Model Patent № 65203, МПК F16Н 21/00. METHOD FOR KINEMATIC ANALYSIS OF A MECHANISM OF III CLASS / Zubaschenko Heorhii Pavlovych (UA); Korchenko Oleksandr Hryhorovych (UA); Aleinikova Natalia Vasylivna (UA); applicant and patentholder National Aviation University. - № u201106503; filed 24.05.2011; issued 25.11.2011. Bul. №22.
A method for kinematic analysis of mechanism of III class is in determination of specific point that belongs to the basic link and is determined as a point of intersection of the axes of two arbitrary leads. To the con-rod point of the basic link of the mechanism of III class one connects an imaginary link that does not affect the degree of freedom of the mechanism. The kinematic analysis of the mechanism of III class is reduced to sequential kinematic analysis of two four-bar linkages – mechanisms of II class.
63. Useful Model Patent № 65205, МПКG01N 29/04, G01N 3/56. METHOD FOR DETERMINATION AND CONTROL OF DEPTH OF CUTTING AT TURNING / Filonenko Serhii Fedorovych (UA); Nimchenko Tetiana Vasylivna (UA); applicant and patentholder National Aviation University. - № u201106505; filed 24.05.2011; issued 25.11.2011. Bul. №22.
Method for determination and control of depth of cutting at turning includes realization of operation of turning with simultaneous determination of characteristics by which one makes conclusions on depth of cutting. As characteristics by which one makes conclusions on depth of cutting one registers acoustic emission. Depth of cutting is determined by rate of change of collected energy of signal of acoustic emission in time.
64. Useful Model Patent № 65206, МПК Н03М 13/31. METHOD FOR DETERMINATION OF CODE REDUNDANCY WEIGHTED GROUP' / Vasylenko Mykola Yuriiovych (UA); Vasylenko Viacheslav Serhiiovych (UA); Chunariov Andrii Vadymovych (UA); applicant and patentholder National Aviation University. - № u201106506; filed 24.05.2011; issued 25.11.2011. Bul. №22.
A method for determination of “weighted group” code redundancy consists in calculation of control value. Low and upper limits of required bit of “weighted group” control value are determined to find optimal size of control value and reduction of probability of errors occurrence in modern information and communication systems and networks.
65. Useful Model Patent № 65207, МПК G01N 3/56, F16C 33/14. METHOD FOR RENEWAL OF FRICTION SURFACE IN MOTOR OILS / Svyryd Mykhailo Mykolaiovych (UA); Kudrin Anatolii Pavlovych (UA); Volosovych Heorhii Andriiovych (UA); Zadniprovska Svitlana Mykolaivna (UA); Borodii Viktor Mykolaiovych (UA); applicant and patentholder National Aviation University. - № u201106507; filed 24.05.2011; issued 25.11.2011. Bul. №22.
Method for renewal of friction surface in motor lubricants is in connection of friction unit to source of power supply of pulse alternating current. Pulse alternating current is applied with modulated frequency from 1 to 2 kHz. From generator of signals one applies alternating carrying frequency from 100 to 200 kHz, this promotes effective transfer of material by means of electrode to friction zone in lubricants.
66. Useful Model Patent № 65208, МПК G01R 23/00. METHOD FOR DETERMINATIO OF CURRENT FREQUENCY OF MODULATED HARMONIC SIGNALS / Derhunov Oleksii Volodymyrovych (UA); Yeremenko Volodymyr Stanislavovych (UA); Kuts Yurii Vasyliovych (UA); Scherbak Leonid Mykolaiovych (UA); applicant and patentholder National Aviation University. - № u201106508; filed 24.05.2011; issued 25.11.2011. Bul. №22.
Method for determination of current frequency of modulated harmonic signals is in fact that for the signal being analyzed one carriers out the Hilbert transformation with determination of its phase characteristic. One performs continuous window processing of values of phase characteristic of signal with interval wit value 2π. One represents selected by the window sections of phase characteristic of the signal to time axis. One determines respective time intervals with determination of current frequency as reverse value to time intervals obtained.
67. Useful Model Patent № 65209, МПК С23С 4/18. METHOD FOR FORMATION OF WEAR RESISTANT AND GAS-THERMAL COATINGS BY TEMPERATURE CYCLING WITH LASER / Kindrachuk Miroslav Vasyliovych (UA); Dukhota Oleksandr Ivanovych (UA); Holovko Leonid Fedorovych (UA); Tisov Oleksandr Viktorovych (UA); Shevchenko Oleksii Leonidovych (UA); HAGHERIZADEN ROODAN MEISAM HABIB (UA); applicant and patentholder National Aviation University. - № u201106509; filed 24.05.2011; issued 25.11.2011. Bul. №22.
A method for formation of wear resistant and gas-thermal coatings by temperature cycling with laser includes a laserprocessing. At that, the processing is carried out without melting thermal-cyclically in the temperature range of 1273873 K, covering the polymorphic transformations, discretely by the points with the processing area of 15-35 % of the total area ofcoverage of the plasma-sprayed coating with the power density of laser radiation of 103-104 W/cm2, with the focused beamdiameter of 5 mm at the optimum value of thermal cycles and depth equal to and greater than the thickness of the coating.
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