Apparatus for use in a fuel delivery system for a gas turbine en

Power plants – Combustion products used as motive fluid – Combustion products generator

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60740, F02C 722

Patent

active

050314076

ABSTRACT:
A fuel manifold (70) for a gas turbine engine is formed from a plurality of spaced bodies (10) and interconnecting conduits (72). The bodies (10) are adapted to provide fluid communication between the conduits (72) and a corresponding plurality of nozzle assemblies (62) which are removably secured to the bodies. The nozzle assemblies (62) can thereby be detached from a structure (58) to which the manifold (70) is secured, while all components (10, 72) of the manifold (70) remain secured to the structure (58) and to each other. A fail-safe sealing member (32) adapted for use with the fuel manifold
ozzle assembly combination (70, 62) is also disclosed.

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patent: 3472025 (1969-10-01), Simmons et al.
patent: 3516252 (1970-06-01), Udell et al.
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patent: 3973395 (1976-08-01), Markowski et al.
patent: 4201046 (1980-05-01), De Negris et al.
patent: 4466240 (1984-08-01), Miller
patent: 4467610 (1984-08-01), Pearson et al.
patent: 4903478 (1990-02-01), Seto et al.

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