发明名称 Flow divider & purge air system for a gas turbine engine
摘要 A purge air and fuel flow divider module (15) independently directs fuel flow to a plurality of manifolds (25, 27 and 29) and independently purges fuel from these manifolds with air when they are not flowing fuel. A secondary manifold (29) is filled with fuel before flowing metered burn flow to it and fuel flow is apportioned between a primary manifold (27) and the secondary manifold (29) during secondary manifold metered burn flow. Three manifolds are disclosed, a primary manifold (27), a secondary manifold (29) and a start or pilot manifold (25), each containing fuel nozzles (31, 33). A manifold main housing (61) contains a purge valve (41) and two three-way solenoids (37, 39) controlling respectively a secondary transfer valve (43) and a pilot nozzle transfer valve (45). Depending on the requirements, the solenoids position the valves to either provide manifold fill fuel, burn flow fuel or purge air to their respective manifolds. When fuel is shut off to the manifold, the purge valve (41) is remotely commanded to purge the primary manifold (27) with air.
申请公布号 US2003200754(A1) 申请公布日期 2003.10.30
申请号 US20020135233 申请日期 2002.04.29
申请人 FUTA PAUL W.;RICE DAVID W.;NIETER THOMAS A. 发明人 FUTA PAUL W.;RICE DAVID W.;NIETER THOMAS A.
分类号 F02C7/228;F02C7/232;(IPC1-7):F02C7/22 主分类号 F02C7/228
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