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公开(公告)号：US20170096215A1
公开(公告)日：2017-04-06
申请号：US15284751
申请日：2016-10-04
发明人： Nicholas Foster , Nikhil Sehgal , Daniel Mulley , Peter Scott
摘要： An aircraft assembly having a first body connected to a second body via a flexible coupling arranged to limit separation of the bearing faces while permitting relative rotational movement between the bodies in a movement plane so as to define a joint between the bodies.
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公开(公告)号：US10683085B2
公开(公告)日：2020-06-16
申请号：US15284751
申请日：2016-10-04
发明人： Nicholas Foster , Nikhil Sehgal , Daniel Mulley , Peter Scott
摘要： An aircraft assembly having a first body connected to a second body via a flexible coupling arranged to limit separation of the bearing faces while permitting relative rotational movement between the bodies in a movement plane so as to define a joint between the bodies.
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公开(公告)号：US20170291695A1
公开(公告)日：2017-10-12
申请号：US15477770
申请日：2017-04-03
发明人： Nicholas Foster , Sam Evans
CPC分类号： B64C25/10 , B64C25/34 , B64C25/36 , B65G23/04 , B65G39/06 , E21B19/22 , F16C13/006 , F16C33/203 , F16C33/205 , F16C33/208 , F16C2208/02 , F16C2326/43
摘要： An aircraft landing gear assembly including structural members coupled via a coupling including a bearing. The bearing has a body defining a first bearing surface arranged to contact a first counter-face of the coupling. The first bearing surface is defined by a first tubular layer of fibre reinforced polymer of a first type having an axis and containing synthetic fibres of a first type wound around and along the axis of the bearing. The bearing body further has a second tubular layer of fibre reinforced polymer of a second type containing synthetic fibres of a second type wound around and along the axis of the bearing.
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