发明名称 |
GAS TURBINE ENGINE COMBUSTOR |
摘要 |
A gas turbine engine combustor (16) is provided with an airspray fuel injector (24), the downstream end of which is coplanar with a heat shield (38) provided at the upstream end of the combustor (16). The fuel injector (24) injects a fuel and air mixture into the combustion chamber (16a) defined within the combustor (16) which is in the form of a cone having an angle of greater than 130 DEG . The combustor (16) has enhanced weak extinction characteristics. |
申请公布号 |
WO9221919(A1) |
申请公布日期 |
1992.12.10 |
申请号 |
WO1992GB00667 |
申请日期 |
1992.04.13 |
申请人 |
ROLLS-ROYCE PLC |
发明人 |
HARRISON, ANDREW;PARK, KEITH |
分类号 |
F23R3/10;F23R3/28;F23R3/42 |
主分类号 |
F23R3/10 |
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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