Invention Grant
- Patent Title: Gas turbine engine device
- Patent Title (中): 燃气轮机发动机装置
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Application No.: US12634606Application Date: 2009-12-09
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Publication No.: US08875520B2Publication Date: 2014-11-04
- Inventor: Gregory W. P. Zeaton , David L. Sutterfield , Sean F. Sullivan
- Applicant: Gregory W. P. Zeaton , David L. Sutterfield , Sean F. Sullivan
- Applicant Address: US IN Indianapolis
- Assignee: Rolls-Royce North American Technologies, Inc.
- Current Assignee: Rolls-Royce North American Technologies, Inc.
- Current Assignee Address: US IN Indianapolis
- Agency: Krieg DeVault LLP
- Main IPC: F02C7/20
- IPC: F02C7/20 ; F02K1/80 ; F02K1/04 ; F02K1/08
Abstract:
A gas turbine engine adapter is provided. In one form the adapter is segmented and may be attached to a gas turbine engine support ring. The adapter can provide a channel that may receive part of a gas turbine engine component such as, but not limited to, a plug nozzle. The adapter can include a load bearing support to counteract axial forces experienced by the plug nozzle during operation of the gas turbine engine. A compressible seal can be provided between the plug nozzle and the adapter. A leaf seal can also be provided to seal between segments of the adapter. The plug nozzle can be discouraged from rotating relative to the adapter.
Public/Granted literature
- US20100162725A1 GAS TURBINE ENGINE DEVICE Public/Granted day:2010-07-01
Information query
IPC分类:
