Methods and apparatus for supporting variable bypass valve systems

作者: Kenneth Alan Bachelder , Donald James Welty

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摘要: A method enables a gas turbine engine variable bypass valve system to be assembled. The comprises positioning unison ring circumferentially within the such that is radially outward from structural frame, coupling at least one bellcrank ring, supported only by said bellcrank, and support coupled frame.

参考文章(10)
Paul C. Daiber, Scott C. Morton, Michelle L. Taylor, Alexander E. Vermejan, Gas turbine engine fan cooled heat exchanger ,(1993)
Eckhard Kraft, Gregor Pennig, Wolfgang Pollert, Device for bleeding-off compressor air in turbine jet engine ,(1973)
Shipley Gerald E, Girard Robert R, Bypass valve mechanism ,(1970)
Wilson Frost, Peter J. Wood, Melvin Bobo, Daniel R. Little, Method and apparatus for ejecting foreign matter from the primary flow path of a gas turbine engine ,(1990)
Rollin G. Giffin, Donald P. McHugh, Ivan E. Woltmann, Gas turbine engine with augmentor and variable area bypass injector ,(1988)
Thomas S. Clayton, Dudley O. Nash, Actuation system for use on a gas turbine engine ,(1981)
George L. Converse, Donald K. Dunbar, Marlen L. Miller, Methods for designing variable cycle gas turbine engines ,(1998)