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NTIS 바로가기국가/구분 | United States(US) Patent 등록 |
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국제특허분류(IPC7판) |
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출원번호 | US-0425238 (1989-10-23) |
우선권정보 | GB-0026514 (1988-11-12) |
발명자 / 주소 |
|
출원인 / 주소 |
|
인용정보 | 피인용 횟수 : 11 인용 특허 : 5 |
When a breakage occurs to the connecting links which connect a gas turbine engine to aircraft structure, the engine drops onto a fail/safe mounting. The drop is minimal in magnitude and the invention provides a visual means for appreciating that the drop and therefore the breakage, has occurred. Rel
An engine mount failure indicator for indicating abnormal relative movement between a gas turbine engine and an associated aircraft structure, comprising: a member slidably mounted in a housing which is adapted for fixing to said aircraft structure; a movable means for engaging said member so as to
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