Fuel injector for a turbine engine

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

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Details

60746, 239 86, 239551, 239562, F02C 722

Patent

active

048626937

ABSTRACT:
Manifold head effects at low fuel flows in a fuel injected air breathing turbine are minimized by utilizing fuel injectors having fuel injecting tubes 66 with open ends 70 for fuel injection and provided with elongated capillary tubes 99 upstream thereof and connected to receive fuel from a fuel manifold 48.

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