Fuel injector for a turbine engine

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

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Details

60743, 60746, F02C 722

Patent

active

051016346

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 (88) upstream thereof and connected to receive fuel from a fuel manifold (48) while uniform, relatively low velocity fuel exit flow from the ends (70) the injecting tubes (66) is achieved through the use of internal impingement surfaces (96, 102, 106, 110, 124).

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patent: 3302399 (1967-02-01), Tini et al.
patent: 3904119 (1975-09-01), Watkins
patent: 4478045 (1984-10-01), Shekleton
patent: 4854127 (1989-08-01), Vinson et al.
patent: 4862693 (1989-09-01), Batakis et al.
patent: 4967563 (1990-11-01), Shekleton

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