发明名称 |
Fuel control for gas turbine engines |
摘要 |
The basic gas turbine engine hydromechanical fuel control is adaptable to different engine configurations such as turbofan, turboprop and turboshaft engines by incorporating in the main housing those elements having a commonality to all engine configurations and providing a removable block for each configuration having the necessary control elements and flow passages required for that particular configuration. That is to say, a block with the elements peculiar to a turbofan engine could be replaced by a mating block that includes those elements peculiar to a turboshaft engine in adapting the control for a turboshaft configuration. Similarly another block with those elements peculiar to a turboprop engine could replace any of the other blocks in adapting the control to a turboprop configuration. Obviously the basic control has the necessary flow passages terminating at the interface with the block and these flow passages mate with corresponding passages in the block.
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申请公布号 |
US4422287(A) |
申请公布日期 |
1983.12.27 |
申请号 |
US19800191548 |
申请日期 |
1980.09.29 |
申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
STEARNS, CHARLES F.;TUTHERLY, HERBERT W. |
分类号 |
F02C9/32;F02C9/26;F02C9/28;(IPC1-7):F02C9/28 |
主分类号 |
F02C9/32 |
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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