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21. 发明专利

JP6841592B2 航空機の水平安定板を制御する方法及び装置有权
公开(公告)号：JP6841592B2
公开(公告)日：2021-03-10
申请号：JP2015219176
申请日：2015-11-09
申请人：ザ・ボーイング・カンパニー , The Boeing Company
发明人：ムーア, ジョナサンカイル , ボック, ブライアンチャールズ , コールマン, エドワードイー.
IPC分类号： B64C5/02 , B64C9/12 , B64C13/16

22. 发明专利

JP2006527124A 审中-公开
公开(公告)号：JP2006527124A
公开(公告)日：2006-11-30
申请号：JP2006514974
申请日：2004-05-26
IPC分类号： B64C39/10 , B64C1/00 , B64C5/08 , B64C9/12 , B64C9/32 , B64C9/34 , B64C39/02

23. 发明专利

JPH06321189A LIFT VARIABLE DEVICE 失效
公开(公告)号：JPH06321189A
公开(公告)日：1994-11-22
申请号：JP10812093
申请日：1993-05-10
申请人： MITSUBISHI HEAVY IND LTD
发明人： YOSHIDA SHINICHI
IPC分类号： B64C9/12
摘要： PURPOSE:To provide a lift variable device which solves a trouble such that airframe strength must be designed in a speed area where respective lift bearing ratios of the main wing, tail plane and body bearing the lift of an aircraft are maximum because they are fluctuated according to the change of speed, resulting in an excessive strength design, which causes an increase in airframe weight. CONSTITUTION:A lift variable device is formed of a speed sensor 11 for detecting the flying speed of an aircraft; a memory 12 for storing the operating quantity data for operating a lift surface capable of controlling a generated lift so that the lift surface can generate a lift of a substantially fixed ratio of the total airframe lift in all flying speed areas; and a control device 13 for reading the operating quantity data from the memory in conformation to the signal from the speed sensor, and operating the lift surface according to the speed. Since the lift surface is operated to have a substantially fixed lift bearing ratio from subsonic area to supersonic area to fly the aircraft, troubles such as increase in airframe weight, reduction in loading cargo, and increase in resistance which accompany an excessive strength design can be solved.

24. 发明专利

JPH0356239B2 失效
公开(公告)号：JPH0356239B2
公开(公告)日：1991-08-27
申请号：JP8449585
申请日：1985-04-22
IPC分类号： B64C9/00 , B64C9/04 , B64C9/12 , B64C13/24

25. 发明专利

JPH01137198A GUIDED MISSILE 失效
公开(公告)号：JPH01137198A
公开(公告)日：1989-05-30
申请号：JP29554687
申请日：1987-11-24
申请人： MITSUBISHI ELECTRIC CORP
发明人： WATANABE YOSHIKO
IPC分类号： F42B10/14 , B64C9/12 , B64C9/36 , F42B10/64
摘要： PURPOSE: To achieve a speedy response and a high trim angle by developing a front wing after rocket motor combustion, sending the control signal of one control device to the actuator of two kinds of steering wings, namely front and rear wings, and simultaneously steering both the wings. CONSTITUTION: When the combustion completion signal of a rocket motor is received, a development mechanism 9 of a front wing 2 operates and the front wing 2 being folded inside is developed. As a result, the force-landing point of an airframe moves to a forward Xcp2 , and a distance to a gravity position xm2 is reduced from Δx2 to Δx3 , thus improving the response of the airframe. On rotation, an actuator 6a of a front wing 2 operates in a direction for raising the front edge of the front wing 2 due to a control signal from a control device 5 and an actuator 6 of a rear wing 4 operates in a direction for lowering the front edge of a rear wing 4. At this time, a clockwise moment required for balancing the airframe can be obtained from both of the front wing 2 and the rear wing 4, thus reducing the amount of steering of each wing as compared with a case where only one kind of steering wing is steered and hence relaxing a restriction to an elevation being generated from the stalling characteristics of wings and achieving a high trim angle.

26. 发明专利

JPS6047156B2 失效
公开(公告)号：JPS6047156B2
公开(公告)日：1985-10-19
申请号：JP7916881
申请日：1981-05-27
申请人： FUJI HEAVY IND LTD
发明人： NOZAWA MASAJI
IPC分类号： B64C9/12 , B64C9/02 , B64C9/06 , B64C13/28 , B64C13/30

27. 发明专利

JPS57194192A AILERON DROOP OPERATING MECHANISM FOR AIRCRAFT 失效
公开(公告)号：JPS57194192A
公开(公告)日：1982-11-29
申请号：JP7916881
申请日：1981-05-27
申请人： FUJI HEAVY IND LTD
发明人： NOZAWA MASAJI
IPC分类号： B64C9/12 , B64C9/02 , B64C9/06 , B64C13/28 , B64C13/30

28. 发明专利

JPS5579799A HINGE ASSEMBLY 失效
公开(公告)号：JPS5579799A
公开(公告)日：1980-06-16
申请号：JP14115379
申请日：1979-10-31
申请人： BOEING CO
发明人： RICHIYAADO BAA ODERU , UIRIAMU JIIN ROESERAA , GEIRII JIYOSEFU WAANAA
IPC分类号： B63B1/28 , B63B39/06 , B64C9/02 , B64C9/12 , B64C9/16 , B64D45/00
摘要： A hinge arrangement between a lifting foil and a flap. The flap comprises a plurality of sections. Each section is mounted by one coupling restraining hinge device to the foil, the hinge device has a hinge pin that extends into a socket located in an adjacent section so that both sections are supported by the hinge. In addition, each two sections are interconnected by a shear key protruding from one section into the same socket of the adjacent section.

29. 发明专利

JPS55280B2 失效
公开(公告)号：JPS55280B2
公开(公告)日：1980-01-07
申请号：JP3725173
申请日：1973-03-31
IPC分类号： B64C9/12 , B64C13/40

30. 发明专利

JP6845746B2 航空機のヨー制御有权
公开(公告)号：JP6845746B2
公开(公告)日：2021-03-24
申请号：JP2017105216
申请日：2017-05-29
申请人：ロッキードマーティンコーポレイション , LOCKHEED MARTIN CORPORATION
发明人：ケネスマールドーセット , ロバートカールストーリー
IPC分类号： B64C9/12

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