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1. 发明授权

US06679452B1 Aircraft landing gear support assemblies and associated methods of installation 有权
标题翻译：飞机起落架支撑组件及相关安装方法
公开(公告)号：US06679452B1
公开(公告)日：2004-01-20
申请号：US10278633
申请日：2002-10-22
申请人： Justin D. Cottet , Michael J. Meneghetti , Brett D. Whitmer
发明人： Justin D. Cottet , Michael J. Meneghetti , Brett D. Whitmer
IPC分类号： B64C2510
CPC分类号： B64C1/0009 , B64C1/26 , B64C25/04 , B64C25/10 , B64C30/00 , B64C2001/0027 , B64C2001/0045 , B64D9/003 , B64D11/00 , B64D27/18 , B64D37/04 , Y02T50/12 , Y02T50/44 , Y02T50/46
摘要： Landing gear support assemblies and associated methods of installation. In one embodiment, a landing gear support assembly usable with an aircraft wing includes an aft trunnion support beam having a base portion, an aft trunnion support spaced apart from the base portion, and a shear center axis extending from the base portion toward the aft trunnion support. The aft trunnion support can be at least approximately vertically aligned with the shear center axis. The base portion can be configured to be attached at least proximate to the rear wing spar with a plurality of fuse pins configured to fail and release the aft trunnion support beam from the rear wing spar when the landing gear exerts a preselected force against the aft trunnion support.
摘要翻译：起落架支撑组件和相关的安装方法。在一个实施例中，可与飞行器机翼一起使用的起落架支撑组件包括：后耳轴支撑梁，其具有基部部分，与基部部分间隔开的后耳轴支撑件以及从基部部分向后耳轴延伸的剪切中心轴线支持。后耳轴支撑件可以至少大致垂直于剪切中心轴线对准。基座部分可以构造成至少靠近后翼梁连接，多个保险丝销构造成当起落架对后耳轴施加预选力时，使后翼翼梁失效并释放后耳轴支撑梁支持。

2. 发明授权

US07118067B2 Wheel mounted water spray deflector 失效
标题翻译：轮式喷水导流板
公开(公告)号：US07118067B2
公开(公告)日：2006-10-10
申请号：US10434747
申请日：2003-05-09
申请人： Justin D. Cottet , Mark N. Simpson
发明人： Justin D. Cottet , Mark N. Simpson
IPC分类号： B64C25/00
CPC分类号： B64C25/32
摘要： A water spray deflector to deflect water spray produced from aircraft landing gear from components of the aircraft. The water spray deflector has an inner diameter and an outer diameter. Coupled to the spray deflector are attachment arms that are adapted to couple with an outer portion of a rim of the landing gear. The attachment arms are also configured to support the water spray deflector position the water spray deflector a distance from a side wall of the tire to prevent the side wall of the tire from coming in contact with the water spray deflector under various loading conditions placed on the tire. In some versions, the water spray deflector is weakened in areas to encourage a failure mode of the water spray deflector.
摘要翻译：一个喷水导流板，用于使从飞机起落架产生的喷水器偏离飞机的部件。喷水偏转器具有内径和外径。耦合到喷射偏转器的是附接臂，其适于与起落架的边缘的外部部分联接。连接臂还构造成支撑喷水偏转器将喷水偏转器定位在距离轮胎侧壁一定距离的位置，以防止轮胎的侧壁在放置在所述轮胎上的各种负载条件下与所述喷水导流板接触胎。在一些版本中，喷水导流板在区域上被削弱，以鼓励喷水导流板的故障模式。

3. 发明授权

US06845943B2 Apparatuses and methods for preventing foreign object damage to aircraft engines 失效
标题翻译：防止飞机发动机异物损坏的装置和方法
公开(公告)号：US06845943B2
公开(公告)日：2005-01-25
申请号：US10690739
申请日：2003-10-20
申请人： David S. Chambers , Justin D. Cottet , David W. Foutch , Mark N. Simpson
发明人： David S. Chambers , Justin D. Cottet , David W. Foutch , Mark N. Simpson
IPC分类号： B64C7/00 , B64C25/16 , B64C25/32
CPC分类号： B64C25/16 , B64C7/00 , B64C25/32 , B64C2025/345
摘要： Apparatuses and methods for preventing foreign object damage (FOD) to aircraft engines are disclosed. In one embodiment, a deployable blocker is coupled to a wing portion and/or a fuselage portion of the aircraft and is configured to prevent debris from travelling on a direct trajectory from a landing gear wheel to an engine air inlet. In other embodiments, the blocker can prevent debris from bouncing off the wing lower surface into the engine inlet, or sticking to the wing lower surface and falling into the engine inlet. The deployable blocker can cover at least a portion of the landing gear when the landing gear is retracted and the blocker assembly stowed. In another embodiment, the blocker can be mounted to the landing gear.
摘要翻译：公开了用于防止飞机发动机的异物损坏（FOD）的装置和方法。在一个实施例中，可展开的阻挡器联接到飞行器的翼部和/或机身部分，并且被构造成防止碎片在从起落架齿轮到发动机空气入口的直接轨迹上行进。在其他实施例中，阻挡器可以防止碎片从机翼下表面弹出到发动机入口中，或者粘附到机翼下表面并落入发动机入口。当起落架缩回并且阻塞组件收起时，可展开的阻挡器可以覆盖起落架的至少一部分。在另一个实施例中，阻挡器可以安装到起落架上。

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