Turbo-jet engine afterburner system

Details Turbo-jet engine afterburner system Turbo-jet engine afterburner system

1984-09-05

1986-06-03

Croyle, Carlton R.

Power plants

Reaction motor

Liquid oxidizer

60749, F02K 310, F02C 100

Patent

active

045922004

ABSTRACT:
An annular burner has an annular flame stabilizer of substantially V shaped cross-section containing a circular fuel injection manifold discharging in counterflow. The annular flame stabilizer is formed by two independent parts, each of these parts constituting one blade of the V cross-section. Pivotal support means are provided at the end of the separation wall of the flows in order to mount each of the parts of the annular stabilizer. The injection manifold is secured to the outer blade of the ring.

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patent: 4125998 (1978-11-01), Barou et al.
patent: 4280324 (1981-07-01), Arliguie et al.

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