Unitized fuel manifold and injector for a turbine engine

Power plants – Combustion products used as motive fluid – Combined with regulation of power output feature

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Details

60738, 60739, F02C 722, F23R 332

Patent

active

051505703

ABSTRACT:
The high cost of a fuel injection system in a turbine engine may be substantially reduced by utilizing a combination manifold/fuel injector (80) that is formed of a flattened tube (82) of annular shape and disposed within the case (58) of the engine in substantially surrounding relation to an annular combustor (44). The flattened tube includes fuel injecting apertures (88, 100) which need not be precision formed but which are aligned with the flared ends (74) of inlet tubes (70) extending into the combustor (44) from the plenum defined by the space between the combustor (44) and the case (58).

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