Gas turbine engine actuation system

作者: Dudley O. Nash

DOI:

关键词: Gas turbinesCrankshaftMechanical engineeringCasingInjectorSynchronizingRotationAxial symmetryEngineeringStructural engineeringSleeve valve (water)

摘要: An actuation system for a gas turbine engine is provided axially translating an annular member such as cylindrical sleeve valve of variable area bypass injector (VABI). In one embodiment, the comprises crankshaft rotatably attached at outer casing transmitting rotational movement. A crankarm pivotally connected between and rotation to helical motion member. Two linkarms are circumferentially spaced from crankarm, casing. The effective synchronizing when rotated.

参考文章(4)
Eckhard Kraft, Gregor Pennig, Wolfgang Pollert, Device for bleeding-off compressor air in turbine jet engine ,(1973)
Ivan E. Kenworth, Ivan E. Woltmann, Variable area bypass injector system ,(1976)
Ransom S Thompson, Hasbrouck Augustus, Circumferential bleed valve ,(1958)