-
公开(公告)号：US20190112986A1
公开(公告)日：2019-04-18
申请号：US16124559
申请日：2018-09-07
Applicant: ROLLS-ROYCE plc
Inventor： Simon M. RUSTON , Rong YANG , Matthew FOX , Aniket Anand KULARNI
Abstract: A pressure relief arrangement for a gas turbine engine comprises a hinged door and a mount. A plastically deformable member is provided between and coupled to the hinged door and the mount. The deformable member is configured to deform between a non-deformed state when the door is in a closed position and an elongated deformed state when the door is in an open position.
Search Results
1
records
(took 0.01 seconds)
筛选
AND
AND
过滤
NOT
NOT
Scan to Join
