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公开(公告)号：US10801363B2
公开(公告)日：2020-10-13
申请号：US15935795
申请日：2018-03-26
Applicant: ROLLS-ROYCE plc
Inventor： Zahid M. Hussain , Oliver Taylor-Tibbott
Abstract: A pressure relief arrangement for a gas turbine engine comprises a hinged door and a mount spaced from the door. An expandable structure is connected to the door and to the mount such that when the door hinges open the expandable structure expands.
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