Gas turbine engine air valve assembly

Details Gas turbine engine air valve assembly Gas turbine engine air valve assembly

F - Mech Eng,Light,Heat,Weapons

02

C

F02C 7/12 (2006.01) F01D 25/12 (2006.01) F02C 9/18 (2006.01)

Patent

CA 2537621

A gas turbine engine air valve assembly has first and second valuing elements. The second element is rotatable about a first axis relative to the first element. The rotation controls a flow of air through the first and second elements. An actuator is coupled by a linkage to the second element. A plurality of follower member assemblies each have an insertion portion extending through a corresponding first aperture in the first valuing element and a corresponding second aperture in the second element. The insertion portion is circumferentially fixed relative to one of the first and second valving elements and circumferentially moveable relative to the other of the first and second valving elements.

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