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.
Type:
Grant
Filed:
May 5, 1977
Date of Patent:
November 21, 1978
Assignee:
Societe Nationale et de Construction de Moteurs d'Aviation
Inventors:
Ernest J. Barou, Roland Beyler, Marc F. B. Buisson, Jacques E. J. Caruel, Roger A. J. Vandenbroucke