Gas turbine engines

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

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F02C 7/22 (2006.01)

Patent

CA 1160467

- 12 - Abstract A split type fuel manifold for gas turbine engines which includes a simple check valve rather than the heretofore used individual valves or complex central valve for uniformly distributing fuel to an array of liquid fuel injectors supplied by the manifold,

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