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Выборка патентов США из подгруппы МПК15 B64C9/38
(1976 – 2016 гг.)
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| N п/п | Номер патента | htm | tif | Название | |
2015 | |||||
| 1 | 9193437 |
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| Unmanned air system (UAS) |
2009 | |||||
| 2 | 7628356 |
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| Yaw control device for a nozzle having a rectangular outlet section |
2000 | |||||
| 3 | 6142425 |
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| Apparatus and method for aerodynamic blowing control using smart materials |
1999 | |||||
| 4 | 5992792 |
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| Aircraft with jet flap propulsion |
1998 | |||||
| 5 | 5791601 |
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| Apparatus and method for aerodynamic blowing control using smart materials |
1997 | |||||
| 6 | 5601256 |
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| Aircraft stabilizing system |
1993 | |||||
| 7 | 5244167 |
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| Lift augmentation system for aircraft |
1992 | |||||
| 8 | 5158251 |
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| Aerodynamic surface tip vortex attenuation system |
1990 | |||||
| 9 | 4976349 |
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| Aerofoil/hydrofoil |
1987 | |||||
| 10 | 4674716 |
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| Blown crescent airfoil |
| 11 | 4648571 |
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| Transverse thrust lift augmentation system |
1986 | |||||
| 12 | 4610410 |
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| Compound helicopter and powerplant therefor |
1984 | |||||
| 13 | 4478378 |
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| Aircraft with jet propulsion |
| 14 | 4463920 |
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| Thrust deflector and force augmentor |
| 15 | 4457480 |
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| Mono-element combined supercritical high lift airfoil |
1983 | |||||
| 16 | 4398687 |
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| Thrust deflector and force augmentor |
| 17 | 4392621 |
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| Directional control of engine exhaust thrust vector in a STOL-type aircraft |
| 18 | 4387869 |
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| Mono-element combined supercritical high lift airfoil |
1981 | |||||
| 19 | 4254620 |
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| Jet engine multiduct noise suppressor |
1979 | |||||
| 20 | 4171112 |
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| V.S.T.O.L. aircraft with control means for maintaining substantially equal thrust on both sides of the aircraft |
1977 | |||||
| 21 | 4005823 |
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| Flap-type two-dimensional nozzle having a plug |
| © 2016. ПАТ-Инфо, В.И. Карнышев | |||||
