Invention Grant
- Patent Title: Mounting system and mounting method for gas turbine aero engine
-
Application No.: US16396923Application Date: 2019-04-29
-
Publication No.: US11292605B2Publication Date: 2022-04-05
- Inventor: Joseph B. Cooper
- Applicant: ROLLS-ROYCE plc
- Applicant Address: GB London
- Assignee: ROLLS-ROYCE plc
- Current Assignee: ROLLS-ROYCE plc
- Current Assignee Address: GB London
- Agency: Shumaker & Sieffert, P.A.
- Priority: GB1808514 20180524
- Main IPC: B64D27/26
- IPC: B64D27/26 ; F01D25/28 ; F02C7/20 ; F02C7/268

Abstract:
A system for mounting a gas turbine engine to a pylon on a wing of an aircraft. A temporary forward link, being length-adjustable, and at least one temporary rearward link, being length-adjustable, are provided. These are for temporarily attaching the gas turbine engine to the pylon. The temporary forward link and the temporary rearward link are each adapted to resist tension and compression, to maintain a positional relationship between the gas turbine engine and the pylon in the absence of adjustment of the lengths of the temporary forward link and the temporary rearward link. Adjustment of the length of the temporary links brings engine mounts into alignment with pylon mounts for service attachment of the gas turbine engine to the pylon.
Information query