发明名称 System for attaching a turbojet engine spinner
摘要 <p>Disclosed is an upstream rotor of a turbomachine comprising a spinner 2 which is removably attached to the upstream end of the rotor 1 by attachment means comprising a dog clutch 3, 9, 10 and rotation-preventing means which lock the spinner 2 in place to prevent rotation of the spinner 2 relative to the rotor 1. The rotation-preventing means comprise pegs 13 which are resiliently urged to the locked position by elastically deformable means such as spring 17.</p>
申请公布号 GB2503075(A) 申请公布日期 2013.12.18
申请号 GB20130006113 申请日期 2013.04.04
申请人 SNECMA 发明人 EMMANUEL PATSOURIS;JACQUES RENE BART
分类号 F01D5/02;F02C7/04 主分类号 F01D5/02
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