Method and apparatus for enhancing gas turbo machinery flow

Details Method and apparatus for enhancing gas turbo machinery flow Method and apparatus for enhancing gas turbo machinery flow

F - Mech Eng,Light,Heat,Weapons

01

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F01D 25/24 (2006.01) F01D 25/30 (2006.01) F04D 29/54 (2006.01)

Patent

CA 2096722

An improved efficiency flow enhancement method and system is provided for a duct system downstream of blading (24) in a turbomachine, the system comprising the blading, a duct (12) leading from the blading, two or more passages de- fined at least in part by partitions (26) which take flow from within the duct, or from across its outlet (35), or from within four duct widths downstream of its outlet, the partitions (26) defining at least partially separated flow passages intended for flows leaving the expanding duct of generally different me- chanical energy, one or more zones of significant pressure drop for the flows of higher energy, one or more passages of comparatively less pressure drop for the passages with flows of lower mechanical energy, one or more zones where the flows are rejoined, and an outlet.

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