Device for igniting fuel injected into a rapidly flowing gaseous

Power plants – Reaction motor – Liquid oxidizer

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Details

60 3971, 60 3972R, 60 3982P, 431349, F02C 722, F02K 310

Patent

active

041259980

ABSTRACT:
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.

REFERENCES:
patent: 3085401 (1963-04-01), LeFebvre et al.
patent: 3540216 (1970-11-01), Quillevere et al.
patent: 3765178 (1973-10-01), Hufnagel et al.
patent: 3800527 (1974-04-01), Marshall et al.
patent: 3931707 (1976-01-01), Vdoviak

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