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1.发明授权公开(公告)号：US09771166B2
公开(公告)日：2017-09-26
申请号：US14404243
申请日：2013-05-23
发明人： Fraser Wilson , Stephen Briancourt , Scott Wallis
IPC分类号： B64D45/00 , B64C25/58 , F16F9/32 , G01L7/16 , G01L9/00 , G01M17/04 , G01B11/14 , B64C25/02 , G01L19/08 , B64F5/60
CPC分类号： B64D45/00 , B64C25/02 , B64C25/58 , B64F5/60 , F16F9/3292 , G01B11/14 , G01L7/16 , G01L9/0089 , G01L19/08 , G01M17/04
摘要： A system for indicating the pressure in an aircraft landing gear shock absorber is provided, the system comprising a source of collimated light and a target, the source of collimated light being attached to the aircraft, and being operable to emit light onto the target; the position of the point of incidence of the light emitted from the source of collimated light on the target being indicative of the pressure in the aircraft landing gear shock absorber. A kit for making such a system and a method of indicating the pressure in an aircraft landing gear are also provided.
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2.发明申请SYSTEM, KIT AND METHOD FOR INDICATING THE PRESSURE IN AN AIRCRAFT LANDING GEAR SHOCK ABSORBER 有权用于表示飞机上的减速齿轮减震器的压力的系统，工具包和方法公开(公告)号：US20150166195A1
公开(公告)日：2015-06-18
申请号：US14404243
申请日：2013-05-23
发明人： Fraser Wilson , Stephen Briancourt , Scott Wallis
CPC分类号： B64D45/00 , B64C25/02 , B64C25/58 , B64F5/60 , F16F9/3292 , G01B11/14 , G01L7/16 , G01L9/0089 , G01L19/08 , G01M17/04
摘要： A system for indicating the pressure in an aircraft landing gear shock absorber is provided, the system comprising a source of collimated light and a target, the source of collimated light being attached to the aircraft, and being operable to emit light onto the target; the position of the point of incidence of the light emitted from the source of collimated light on the target being indicative of the pressure in the aircraft landing gear shock absorber. A kit for making such a system and a method of indicating the pressure in an aircraft landing gear are also provided.
摘要翻译： 提供了一种用于指示飞机起落架减震器中的压力的系统，该系统包括准直光源和目标物体，准直光源连接到飞行器，并且可操作以将光发射到目标上; 从目标上的准直光源发射的光的入射点的位置指示飞机起落架减震器中的压力。 还提供了用于制造这种系统的套件以及指示飞机起落架中的压力的方法。
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公开(公告)号：US10780978B2
公开(公告)日：2020-09-22
申请号：US15302886
申请日：2015-04-09
摘要： A drive system for an aircraft landing gear is described. The drive system includes a drive pinion, a drive shaft arranged to rotate the drive pinion about a drive axis, and a casing which rotatably supports the drive shaft. The drive pinion is rotatably supported on the casing by a self-aligning bearing. The drive pinion is coupled to the drive shaft by a flexible coupling adapted to transfer torque between the drive pinion and the drive shaft and to permit tilting of the drive pinion relative to the drive axis.
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公开(公告)号：US10654562B2
公开(公告)日：2020-05-19
申请号：US15661115
申请日：2017-07-27
摘要： An aircraft include a landing gear is disclosed. The landing gear comprises a main strut and an inboard stay assembly connected to the aircraft fuselage such that landing gear loads can be transferred from the inboard stay assembly into the fuselage. The landing gear also comprises a sidestay connected to the wing such that landing gear loads can be transferred from the sidestay into the wing and a link assembly connected to the aircraft such that landing gear loads can be transferred via the link assembly into the aircraft. The landing gear is arranged such that, in use, when the landing gear is extended, substantially all the landing gear loads are transferred from the landing gear to the aircraft via one or more of the inboard stay assembly, the sidestay and the link assembly.
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