发明名称 |
SURGE/STALL CESSATION DETECTION SYSTEM |
摘要 |
<p>Surge/Stall Cessation Detection System The cessation of stall/surge in the compressor of a twin spool gas turbine engine is detected by comparing by digital electronics the 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.</p> |
申请公布号 |
CA1252770(A) |
申请公布日期 |
1989.04.18 |
申请号 |
CA19850489135 |
申请日期 |
1985.08.21 |
申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
KENISON, DAVID F.;SHEPPARD, DONALD E. |
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 |
|
代理人 |
|
主权项 |
|
地址 |
|