Compressor diffuser non-return valve and method for starting...

Details Compressor diffuser non-return valve and method for starting... Compressor diffuser non-return valve and method for starting...

F - Mech Eng,Light,Heat,Weapons

01

D

60/57

F01D 19/00 (2006.01) F02C 7/27 (2006.01)

Patent

CA 1209352

ABSTRACT OF THE DISCLOSURE Gas turbine engine starting method and apparatus includes the engine turbine and rotary compressor components coupled for dependent rotation; a compressor plate diffuser with an integral, floating plate one-way valve; a housing receiving diffused com- pressed air for channeling to the combustor; and a source of pressurized air connected for admission to the housing during startup at a point upstream of combustor and downstream of one-way valve for initiating rotation of the turbine and coupled compressor.

431250

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