DISPOSITIF D'ALLUMAGE DE CARBURANT INJECTE DANS UN MILIEU GAZEUX EN ECOULEMENT RAPIDE

An auxiliary chamber or ignition "prechamber" for afterburners of aeronautical turbine engines draws in, through a perforated plate, a carbureted mixture produced by fuel projected against an anvil by an injection manifold, and the injection manifold also issues a jet of fuel into a tube w...

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1. Verfasser: ROLAND ROBERT CHARLES BEYLER, ERNEST JEAN BAROU, MARC FRANCOIS BERNARD BUISSON, JACQUES EMILE JULES CARUEL ET ROGER ALFRED JULES VANDENBROUCKE
Format: Patent
Sprache:fre
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Zusammenfassung:An auxiliary chamber or ignition "prechamber" for afterburners of aeronautical turbine engines draws in, through a perforated plate, a carbureted mixture produced by fuel projected against an anvil by an injection manifold, and the injection manifold also issues a jet of fuel into a tube which discharges into the chamber downstream of a spark plug. The produced flame is guided into a flame stabilizer.