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1. 发明公开

EP2772428A1 Aircraft landing gear cooling system 有权
标题翻译： Kühlsystemeines Flugzeugfahrwerks
公开(公告)号：EP2772428A1
公开(公告)日：2014-09-03
申请号：EP14153604.5
申请日：2014-02-03
申请人： The Boeing Company
发明人： Kirkbride, David W. , Jolliffe, Darrell S.
IPC分类号： B64C25/42 , F16D65/847
CPC分类号： B60R99/00 , B60T5/00 , B64C25/42 , F16D65/847 , Y10T137/0318 , Y10T137/6855
摘要： According to one embodiment, an apparatus for cooling at least one landing gear brake (42) of an aircraft in flight is described. The apparatus includes an air handling assembly (120) that is coupled to the aircraft. The air handling assembly (120) includes at least one air inlet port (124). The apparatus also includes an air delivery assembly (150) that is in air receiving communication with the air handling assembly (120). The air delivery assembly (150) includes at least one nozzle (152) that is configured to direct air into a first space adjacent a first side of the landing gear brake (42) to create an air pressure differential across the landing gear brake (42).
摘要翻译：根据一个实施例，描述了用于冷却飞行中的飞行器的至少一个起落架制动器（42）的装置。该装置包括联接到飞行器的空气处理组件（120）。空气处理组件（120）包括至少一个空气入口（124）。该设备还包括空气输送组件（150），其与空气处理组件（120）处于空气接收通信。空气输送组件（150）包括至少一个喷嘴（152），其被构造成将空气引导到与起落架制动器（42）的第一侧相邻的第一空间中，以在起落架制动器（42）上产生气压差）。

2. 发明授权

EP2772428B1 Aircraft landing gear cooling system 有权
标题翻译：飞机起落架冷却系统
公开(公告)号：EP2772428B1
公开(公告)日：2018-05-02
申请号：EP14153604.5
申请日：2014-02-03
申请人： The Boeing Company
发明人： Kirkbride, David W. , Jolliffe, Darrell S.
IPC分类号： B64C25/42 , F16D65/847
CPC分类号： B60R99/00 , B60T5/00 , B64C25/42 , F16D65/847 , Y10T137/0318 , Y10T137/6855
摘要： According to one embodiment, an apparatus for cooling at least one landing gear brake (42) of an aircraft in flight is described. The apparatus includes an air handling assembly (120) that is coupled to the aircraft. The air handling assembly (120) includes at least one air inlet port (124). The apparatus also includes an air delivery assembly (150) that is in air receiving communication with the air handling assembly (120). The air delivery assembly (150) includes at least one nozzle (152) that is configured to direct air into a first space adjacent a first side of the landing gear brake (42) to create an air pressure differential across the landing gear brake (42).

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