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Variable volume combustor with nested fuel manifold system

Patent ·
OSTI ID:1324683
The present application provides a combustor for use with a gas turbine engine. The combustor may include a number of micro-mixer fuel nozzles, a fuel manifold system in communication with the micro-mixer fuel nozzles to deliver a flow of fuel thereto, and a linear actuator to maneuver the micro-mixer fuel nozzles and the fuel manifold system.
Research Organization:
GENERAL ELECTRIC COMPANY, Schenectady, NY (United States)
Sponsoring Organization:
USDOE
DOE Contract Number:
FC26-05NT42643
Assignee:
GENERAL ELECTRIC COMPANY (Schenectady, NY)
Patent Number(s):
9,441,544
Application Number:
13/760,092
OSTI ID:
1324683
Country of Publication:
United States
Language:
English

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