发明名称 |
Device for igniting fuel injected into a rapidly flowing gaseous medium |
摘要 |
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.
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申请公布号 |
US4125998(A) |
申请公布日期 |
1978.11.21 |
申请号 |
US19770794242 |
申请日期 |
1977.05.05 |
申请人 |
SOCIETE NATIONALE ET DE CONSTRUCTION DE MOTEURS D"AVIATION |
发明人 |
BAROU, ERNEST J.;BEYLER, ROLAND;BUISSON, MARC F. B.;CARUEL, JACQUES E. J.;VANDENBROUCKE, ROGER A. J. |
分类号 |
F02C7/266;F23R3/20;(IPC1-7):F02C7/22;F02K3/10 |
主分类号 |
F02C7/266 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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