Control mechanism for injector diaphragms

Details Control mechanism for injector diaphragms Control mechanism for injector diaphragms

1987-07-02

1989-05-02

Stout, Donald E.

Power plants

Combustion products used as motive fluid

With variable oxidizer control

60748, F02C 900, F02C 100

Patent

active

048256412

ABSTRACT:
A control mechanism for injector diaphragms in a turbojet engine is disclosed wherein an annular fairing is utilized to synchronize the movement of the individual air-fuel injector diaphragms. The fairing member is interconnected to each of the diaphragms and a single control element controls the rotational movement of the annular fairing. This minimizes the turbulence of the air flow passing around the control system.

REFERENCES:
patent: 3490230 (1970-01-01), Pillsbury et al.
patent: 3723049 (1973-03-01), Juricek
patent: 3932110 (1976-01-01), Waddell
patent: 4534166 (1985-08-01), Kelm et al.
patent: 4696157 (1987-09-01), Barbier et al.
patent: 4726182 (1988-02-01), Barbier et al.
patent: 4754600 (1988-07-01), Barbier et al.
patent: 4766722 (1988-08-01), Bayle-Laboure et al.

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