Multi-tube, can-annular pulse detonation combustor based engine

F - Mech Eng,Light,Heat,Weapons – 23 – R

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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.

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