| 发明名称 |
Surge/stall cessation detection system. |
| 摘要 |
<p>The cessation of stall/surge in the compressor of a twin spool gas turbine engine is detected by comparing by digital electronics and engines sensed burner pressure with a burner pressure calculated from corrected low pressure compressor speed and sensed airplane Mach number which has been compensated to approximate engine dynamics. (Fig. 3)</p> |
| 申请公布号 |
EP0185601(A2) |
申请公布日期 |
1986.06.25 |
| 申请号 |
EP19850630178 |
申请日期 |
1985.10.31 |
| 申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
KENISON, DAVID FRANCIS;SHEPPARD, DONALD EDWARD |
| 分类号 |
F02C9/28;F02C9/00;F02C9/18;F02C9/44;F02C9/52;F04D27/02;G01P5/00;(IPC1-7):F02C9/00 |
主分类号 |
F02C9/28 |
| 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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