Exhaust nozzle for suppressing infrared radiation

作者: Walter M. Presz , Mark H. Hammond

DOI:

关键词:

摘要: An exhaust nozzle (24 or 28) operative to suppress the InfraRed (IR) signature radiated from high-temperature of an engine (12) which includes inlet conduit adapted for receiving and a plurality adjoined lobes (30) integrally formed in combination with conduit. The are characterized by first second penetrating (60, 62 70, 72) admixing low-temperature gaseous fluid axially staggered respect each other. In preferred embodiment, at least one said (60 62, 70 extends into core region (CR) effect thorough mixing low temperature fluid. Various embodiments such described context multi-stage mixer/ejector (20).

参考文章(27)
Leonard John Rodgers, Exhaust mixer for turbofan aeroengine ,(1982)
Mercier Pierre Ernest, Airplane power plant ,(1941)
William Steyer, Samuel Rothrock Barr, Thomas Chew, James Leroy Nye, Infrared suppression system for a gas turbine engine ,(1974)
Christos Demogenes, Robert A. Stone, Cooled infrared suppressor ,(1970)
H True, R Fitzsimmons, Aircraft engine noise suppression ,(1971)
Michael J. Werle, Walter M. Presz, Robert W. Paterson, Airfoil-shaped body ,(1987)
Delbert W. Torkelson, Fixed geometry mixer/ejector noise suppression system for turbofan aircraft engines Journal of the Acoustical Society of America. ,vol. 99, pp. 644- ,(1994) , 10.1121/1.414587
Jr. Walter M. Presz, Two-stage mixer ejector suppressor ,(1996)