Methods and apparatus to adjust bleed ports on an aircraft engine
作者： Brian W. Debronsky , Steve G. Mackin , Sean C. Thomas
DOI:
关键词:
摘要: Methods and apparatus to adjust bleed ports on an aircraft engine are disclosed. An example for bleeding air from a multi-stage compressor of includes case having plurality ports. A first port is associated with stage compressor, second the compressor. The plenum connected define cavity. fluidly coupling fluid conduit providing one or more systems aircraft. also selection mechanism located within including portion proximate operable prevent flow through port.
lens.org 参考文章(20)
John B Wheatley, Compressor air bleed-off valve ,(1954)
Steven L. Battaini, David J. Petro, Apparatus method for calibrating and setting compressor air bleed valve schedules ,(1984)
Nicholas Damlis, Kenneth Paul Onderko, Dale Bradley Elliott, Peter Nicholas Szucs, Bifurcated splitter for variable bleed flow ,(2001)
Thomas Ory Moniz, Thomas Viars, Axial compressor with arrangement for bleeding air from variable stator vane stages ,(2012)
Richard Alan Zimbrick, Larry Allen Schaut, Stator bypass system for turbofan engine ,(1976)
Pascal Gérard Gervais, Michel Gilbert Roland Brault, Bruno Beutin, Monique Andrée Thore, Bleed-off device in a bypass turbojet ,(2002)
Kenneth Alan Bachelder, Donald James Welty, Methods and apparatus for supporting variable bypass valve systems ,(2002)
Baptiste Benoit Colotte, Bruno Robert Gaully, System for controlling variable geometry equipment for a turbine engine, especially by bellcranks ,(2009)
George Albert Coffinberry, Air turbine powered accessory ,(2004)
Michel Cadieux, Bleed off valve system ,(2007)