General Electric Company

Bruce A Hamblin

Ivan H Peterson

Marie A Kastrup

A rigid fuel manifold system for use in a gas turbine engine which is resistant to vibrations from operation of the engine. The system comprises two fuel feed manifolds, a fuel drain manifold and support brackets which attach these manifolds to one another and provide a structure with a high natural frequency above the 1/rev of the engine operating range. Structural support brackets that permit easy assembly and low installation stress are also provided.

Fuel manifold system for gas turbine engines

Conduit couplings for high temperature, high pressure applications with up to 10.degree. misalignment capability are provided. The couplings provide a tight seal without special machining or assembly methods. The coupling comprises a spherical ball that fits within an end cap having a frustoconically shaped receptacle. A metal sealing ring positioned therebetween helps provide a tight seal that withstands pressures above 100 psi and temperatures in the range of 700.degree.-1200.degree. F.

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Cincinnati, OH, United States of America

Bruce A Hamblin