| 摘要 |
The invention relates to a fuel pipe coupling ( 101 ), in particular a fuel pipe coupling for an aircraft. The invention provides a pipe end fitting ( 102 ) including a flange ( 103 ), a resiliently deformable interfacing body ( 105 ) including a partially spherical internal surface ( 112 ) and a socket arrangement ( 104 ). The coupling is arranged such that the flange ( 103 ) of the pipe end fitting ( 102 ) is associated with the partially spherical internal surface ( 112 ) of the resiliently deformable interfacing body ( 105 ) and may move both axially and angularly with respect to the socket arrangement ( 104 ).
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