发明名称 |
FUEL INJECTOR |
摘要 |
A fuel injector (2) including a combustion air flow conduit, a fuel inlet (2.4) and means to mix the air and fuel flowing therethrough (2.2, 2.3, 2.6), additionally comprising fluidic control means (2.7) including at least one control port (3.4, 3.5, 3.6, 3.7), such that flow of control air through said control port allows variation in the degree of flow resistance to which combustion air is subjected. For example, control air flowing through the control port may impart swirl to the combustion air flow from the inlet, thereby subjecting the combustion air flow to increased resistance. Alternatively a fluidic diverter (2.7) may selectively divert the main flow to either the first or second sub-conduits (2.2, 2.3), each sub-conduit subjecting combustion air to different degrees of flow resistance.
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申请公布号 |
WO9932828(A1) |
申请公布日期 |
1999.07.01 |
申请号 |
WO1998GB03733 |
申请日期 |
1998.12.18 |
申请人 |
THE SECRETARY OF STATE FOR DEFENCE;BRUNDISH, KEVIN, DAVID;WILSON, CHRISTOPHER, WILLIAM;TIPPETTS, JOHN, RUSSELL |
发明人 |
BRUNDISH, KEVIN, DAVID;WILSON, CHRISTOPHER, WILLIAM;TIPPETTS, JOHN, RUSSELL |
分类号 |
F15C1/08;F23C7/00;F23C99/00;F23R3/26;(IPC1-7):F23C7/00;F15C1/16 |
主分类号 |
F15C1/08 |
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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