Surge detection in a gas turbine engine

F - Mech Eng,Light,Heat,Weapons – 02 – C

Patent

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F02C 9/28 (2006.01) F01D 21/14 (2006.01) F02C 7/22 (2006.01)

Patent

CA 2683945

A method for detecting a surge condition during operation of a gas turbine engine includes detecting a change of pressure differential between fuel flows in a fuel system (28) of the engine during engine operation.

L'invention concerne un procédé de détection d'un état de surpression pendant le fonctionnement d'une turbine à gaz. Le procédé consiste à détecter un écart de la différence de pression entre des débits carburant d'un système d'alimentation en carburant (28) de la turbine pendant son fonctionnement.

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