F - Mech Eng,Light,Heat,Weapons – 01 – D
Patent
F - Mech Eng,Light,Heat,Weapons
01
D
F01D 25/30 (2006.01) B64D 33/04 (2006.01)
Patent
CA 2581827
An exhaust duct system for a gas turbine engine that mounts within a tail cone of an aircraft, comprises an exhaust exit that exits one side of the tail cone offset from the axial centreline of the tail cone and an exhaust duct that couples the engine to the offset exhaust exit, with a straight section of the exhaust duct extending from the exhaust exit for a length that corresponds to at least one diameter of the exhaust duct.
Francisco Jay M.
Napier James C.
Hamilton Sundstrand Corporation
Ogilvy Renault Llp/s.e.n.c.r.l.,s.r.l.
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