Gas turbine engine case thermal control flange

F - Mech Eng,Light,Heat,Weapons – 01 – N

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F01N 1/00 (2006.01) F01D 11/24 (2006.01) F01D 25/14 (2006.01)

Patent

CA 2089275

DV11000 PATENT 13DV-11000 GAS TURBINE ENGINE CASE THERMAL CONTROL FLANGE ABSTRACT An apparatus i provided to thermally control a section of engine casing by flowing heat transfer fluid within an axially disposed plurality of circular flowpaths within a section of engine casing or flange such as a thermal control ring. Flowpaths are preferably arranged in alternating counterflowing directions in the ring such that there is substantially no circumferential gradient in the mass flowrate weighted average temperature of the heat transfer fluid supplied by any two adjacent counterflowing fluid flowpaths. Each flowpath may have two or more circuits having inlets and outlets for flowing the heat transfer fluid.

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