Improved start flow measurement

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

Patent

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Details

F02C 9/26 (2006.01) F01D 19/00 (2006.01) F02C 7/22 (2006.01) F23R 3/28 (2006.01)

Patent

CA 2683942

A method and apparatus for measuring a start fuel flow to a pilot nozzle (34) of a fuel system (28) of a gas turbine engine using pressure differential between fuel passages leading to fuel nozzles (34, 37).

L'invention concerne un procédé et un appareil qui utilisent une différence de pression entre des passages conduisant aux buses de carburant (34, 37) pour mesurer un débit de carburant de départ s'écoulant vers une buse pilote (34) d'un système d'alimentation en carburant (28) d'une turbine à gaz.

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