Invention Grant
US09540939B2 Gas turbine engine with attached nosecone 有权
燃气涡轮发动机附带的nosecone

Gas turbine engine with attached nosecone
Abstract:
A gas turbine engine includes a compressor section and a nosecone assembly. The compressor section includes an inlet guide vane assembly including an inner shroud, an outer shroud, and an inlet guide vane extending from the inner shroud to the outer shroud. The nosecone assembly is attached to the inner shroud.
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