Air bleed system for an axial turbomachine
作者： David Depaepe
DOI:
关键词:
摘要: The present application relates to a bladed stator of turbomachine compressor, configured straighten an annular stream the turbomachine. includes at least one wall define stream, row blades extending radially from and means pressurizing in communication with stream. are pressurize chamber which is separated lubrication housing by labyrinth seal. comprise passage through thickness connecting further scoop open upstream so as capture dynamic pressure
lens.org 参考文章(10)
Monchois Florence, Stangalini Gerard, Kervistin Robert, Procedure for pressurising lubrication chambers of turbines, - is effected by tapping off and controlling, by automatic valve, the pressurised gas. ,(1992)
John C. DiTomasso, Steven H. Zysman, Steven D. Sandahl, John P. Nikkanen, Inlet and outlet module for a heat exchanger for a flowpath for working medium gases ,(1997)
Lawrence B Venable, John A Gill, Roger T Earle, Gas turbine engine lubricant sump vent and circulating system ,(1969)
Richard Martin Muny, Compressor bleed case ,(2003)
William Charles Groll, Rolf Robert Hetico, James Edward Stoker, William Andrew Bailey, Robert Eugene Kraft, Nelson Dirk Gibbens, Shrouded turbofan bleed duct ,(2006)
Jack Rogers Taylor, David Louis Burrus, Combustor inlet diffuser with boundary layer blowing ,(2003)
Alan G. Tiltman, Kin Poon, Mark C. Morris, Bradley Volkmann, Gas turbine engine including a low pressure sump seal buffer source and thermally isolated sump ,(2005)
Thomas Ory Moniz, Compact booster bleed turbofan ,(2005)
John A Drake, Aircraft booster jet power unit ,(1947)
Franklin Elliott Miller, Precooling heat exchange arrangement integral with mounting structure fairing of gas turbine engine ,(1990)