Surge/stall cessation detection system

Details Surge/stall cessation detection system Surge/stall cessation detection system

F - Mech Eng,Light,Heat,Weapons

02

C

60/184, 244/47

F02C 9/00 (2006.01) F04D 27/02 (2006.01) G01P 5/00 (2006.01)

Patent

CA 1252770

- 11 - Abstract 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.

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