Static pressure system for gas turbine engines

Rotary kinetic fluid motors or pumps – With inspection – signaling – indicating or measuring means

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137 152, F01D 1708

Patent

active

048728071

ABSTRACT:
A pressure sensing system strategically located measures static pressure of the inlet air of a gas turbine engine that is utilized as a signal indicative of engine inlet total pressure. The system consists of a number of ports circumferentially spaced around the engine case near the face of the engine which communicate with a manifold for feeding the average static pressure to a transducer.

REFERENCES:
patent: 2989846 (1961-06-01), Hausammann
patent: 4123196 (1978-10-01), Prince, Jr. et al.
patent: 4291533 (1981-09-01), Dugger et al.
patent: 4414807 (1983-11-01), Kerr
patent: 4711084 (1987-12-01), Brockett
patent: 4733975 (1988-03-01), Komanetsky et al.

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