Invention Grant
- Patent Title: Pressure relief arrangement for a gas turbine engine
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Application No.: US16124559Application Date: 2018-09-07
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Publication No.: US11028782B2Publication Date: 2021-06-08
- Inventor: Simon M. Ruston , Rong Yang , Matthew Fox , Aniket Anand Kulkarni
- Applicant: ROLLS-ROYCE plc
- Applicant Address: GB London
- Assignee: ROLLS-ROYCE plc
- Current Assignee: ROLLS-ROYCE plc
- Current Assignee Address: GB London
- Agency: Barnes & Thornburg LLP
- Priority: IN201711036298 20171012,GB1720831 20171214
- Main IPC: F01D25/24
- IPC: F01D25/24 ; F02C9/18 ; B64D29/08 ; F02K3/06 ; F02K3/075
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.
Public/Granted literature
- US20190112986A1 PRESSURE RELIEF ARRANGEMENT FOR A GAS TURBINE ENGINE Public/Granted day:2019-04-18
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