Fuel manifold system for gas turbine engines

Power plants – Combustion products used as motive fluid

Patent

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Details

60 3931, 60739, F02C 722

Patent

active

051686988

ABSTRACT:
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.

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patent: 4852348 (1989-08-01), Allard et al.
patent: 4903478 (1990-02-01), Seto et al.
patent: 5031407 (1991-07-01), Zaremba et al.

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