F - Mech Eng,Light,Heat,Weapons – 23 – R
Patent
F - Mech Eng,Light,Heat,Weapons
23
R
F23R 7/00 (2006.01) F02C 5/02 (2006.01) F02C 5/12 (2006.01) F23C 15/00 (2006.01)
Patent
CA 2742062
An engine (100) contains a compressor stage (101), a pulse detonation combustion stage (105) and a turbine stage (103). The pulse detonation combustion stage contains at least one pulse detonation combustor (109) which has an inlet portion (111). The pulse detonation combustor is oriented longitudinally and/or tangentially with respect to a centerline of the engine. A plenum (115), a casing (107), a diffuser (119) and a shroud (113) can be added in this combustion stage to achieve better performances.
L'invention porte sur un moteur (100) qui contient un étage compresseur (101), un étage de combustion à détonations pulsées (105) et un étage de turbine (103). L'étage de combustion à détonations pulsées contient au moins une chambre de combustion à détonations pulsées (109) qui est pourvue dune partie d'entrée (111). La chambre de combustion à détonations pulsées est orientée longitudinalement et/ou de façon tangentielle par rapport à un axe longitudinal du moteur. Un plénum (115), un carter (107), un diffuseur (119) et un carénage (113) peuvent être ajoutés dans cet étage de combustion pour obtenir de meilleures performances.
Dean Anthony John
Glaser Aaron Jerome
Joshi Narendra Digamber
Kenyon Ross Hartley
Rasheed Adam
Company General Electric
Craig Wilson And Company
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