Invention Grant
US08596965B2 Gas turbine engine compressor case mounting arrangement 有权
燃气涡轮发动机压缩机壳体安装布置

Gas turbine engine compressor case mounting arrangement
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.
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