Back to results
US 5,857,339 AGranted
Combustor flame stabilizing structure
AssigneeThe United States of America as represented by the Secretary of the Air Force
InventorsWilliam M. Roquemore, Dale T. Shouse, Kuang-Yu M. Hsu
Life of this patent
Estimating the term…
Abstract
A combustor structure is described which comprises a cavity defined in the combustor for trapping a vortex of fuel, air and hot combustion products to stabilize the flame, the cavity being formed in any suitable way such as being defined between two or more bluff bodies in tandem, or in a wall of the combustor, or in the combustor liner, and wherein fuel and air are injected directly into the fuel/air recirculation zone defined by the trapped vortex.
Claims1
A combustor structure comprising:
- (a) a housing defined along a substantially central axis;
- (b) means defining a pair of axially spaced bluff bodies disposed along said central axis, said bluff bodies defining therebetween a substantially annularly shaped cavity for trapping therewithin a vortex including a mixture of fuel and air for combustion within said cavity whereby a flame within said combustor is stabilized within said cavity;
- (c) wherein the spacing between said bluff bodies is about 0.6 times the diameter of said cavity;
- and
- (d) means for injecting fuel and air into said cavity disposed within said cavity for promoting circulation a mixture of fuel and air within said cavity.
2 more elements
Dependencies are inferred from the claim text.