F - Mech Eng,Light,Heat,Weapons – 02 – K
Patent
F - Mech Eng,Light,Heat,Weapons
02
K
F02K 3/02 (2006.01) F02K 1/38 (2006.01)
Patent
CA 2515849
A gas turbine engine exhaust nozzle (38) includes a nacelle (16) having an inlet (32) and main outlet (46) at opposite ends, and a main duct (36) extending therebetween. A secondary bypass duct (48) extends radially through the nacelle (16) upstream of the main outlet (46) and includes an unobstructed secondary inlet (50) joined to the main duct (36), and a secondary outlet (52) surrounding the main outlet (46) for collectively discharging exhaust flow in confluent streams.
L'invention concerne une tuyère de turbine à gaz (38) comprenant une nacelle (16) dotée d'une entrée (32) et d'une sortie principale (46) à des extrémités opposées, et d'une conduite principale (36) s'étendant entre elles. Un canal de dérivation secondaire (48) s'étend radialement à travers la nacelle (16) en amont de la sortie principale (46) et comprend une entrée secondaire libre (50) reliée à la conduite principale (36), et une sortie secondaire (52) encerclant la sortie principale (46) de manière à décharger de façon collective la veine de gaz en flux confluents.
Deeth Williams Wall Llp
The Nordam Group Inc.
LandOfFree
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