A splitter is disclosed that can be coupled with a splitter support and used within a diffuser of a gas turbine engine. The splitter includes apertures for receiving a portion of the splitter support. The splitter support includes support arms that are adapted to be slidingly received within the apertures of the splitter.
1. An apparatus comprising: a gas turbine engine having a compressor;a flow splitter disposed within a flow path between a radially inner wall and radially outer wall of the gas turbine engine and having upper and lower surfaces for splitting a flow of working fluid from the compressor, the flow splitter also having fastener portions disposed on opposing circumferential ends operable to be connected to the gas turbine engine;a radially oriented splitter support structured to be coupled to and support the flow splitter;a fastener assembly used to connect ...
이 특허에 인용된 특허 (15)
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