Invention Grant
- Patent Title: Gas turbine engine compressor case mounting arrangement
- Patent Title (中): 燃气涡轮发动机压缩机壳体安装布置
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Application No.: US13294492Application Date: 2011-11-11
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Publication No.: US08596965B2Publication Date: 2013-12-03
- Inventor: Brian D. Merry , Gabriel L. Suciu , Christopher M. Dye
- Applicant: Brian D. Merry , Gabriel L. Suciu , Christopher M. Dye
- Applicant Address: US CT Hartford
- Assignee: United Technologies Corporation
- Current Assignee: United Technologies Corporation
- Current Assignee Address: US CT Hartford
- Agency: Carlson, Gaskey & Olds P.C.
- Main IPC: F01D1/00
- IPC: F01D1/00

Abstract:
A compressor case support arrangement for a gas turbine engine includes a fan section having a central axis and a compressor case for housing a compressor. An inlet case guides air to the compressor. The compressor case is positioned axially further from the fan section than the inlet case. A support member extends between the fan section and the compressor case. The support member restricts movement of the compressor case relative to the inlet case. The support member is positioned axially further from the fan section than the plumbing access area.
Public/Granted literature
- US20120288366A1 GAS TURBINE ENGINE COMPRESSOR CASE MOUNTING ARRANGEMENT Public/Granted day:2012-11-15
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