Surge/stall cessation detection system

Power plants – Combustion products used as motive fluid – Combined with regulation of power output feature

Patent

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Details

415 27, F02C 900, F02C 918

Patent

active

046228080

ABSTRACT:
The cessation of stall/surge in the compressor of a twin spool gas turbine engine is detected by comparing by digital electronics the engine's 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.

REFERENCES:
patent: 4060980 (1977-12-01), Elsaesser et al.
patent: 4117668 (1978-10-01), Elsaesser et al.
patent: 4118926 (1978-10-01), Curvino et al.
patent: 4164034 (1979-08-01), Glennon et al.

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