发明名称 |
Boundary layer prefilmer airblast nozzle |
摘要 |
A gas turbine fuel injection nozzle is disclosed in which the secondary fuel is spread into a very thin film entirely within a region of low air momentum. The fuel is therefore not affected by turbulence, and this results in an evenly circumferentially distributed fuel film at the discharge orifice of the nozzle resulting in an even and extremely fine spray of fuel to enhance proper engine performance.
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申请公布号 |
US4365753(A) |
申请公布日期 |
1982.12.28 |
申请号 |
US19800180284 |
申请日期 |
1980.08.22 |
申请人 |
PARKER-HANNIFIN CORPORATION |
发明人 |
HARDING, CURTIS F.;SIMMONS, HAROLD C. |
分类号 |
B05B7/04;B05B7/06;B05B7/10;F23D11/12;F23D11/24;(IPC1-7):B05B7/10 |
主分类号 |
B05B7/04 |
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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