Fuel slinger combustor
OwnerAlbert H. Beaufrereinventor
Life of this patent
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Abstract
Fuel slinger combustor, regenerative air-cooled gas turbine engine embodying the same, characterized by a pre-mix chamber in which fuel is well atomized by being projected against an impingement ring and further atomized and intimately mixed by the shearing action of cool unregenerated opposing swirling air. The remaining primary air also not heated by the regenerator enters through swirl louvres or ports which maintains the fuel-air mixture in a high recirculation state for clean and stable combustion at very lean mixtures. High pressure fuel is fed to the slinger by a high pressure fuel bearing-pump that makes possible starting the combustion at low speeds and at high altitudes.
Claims4
In a combustor with a rotary slinger as the fuel injector, the combination of wall means defining a combustion zone and a premix chamber in flow communication with said combustion zone;
- a rotary fuel slinger attached to shaft means to project atomized fuel in said premix chamber with a predetermined tangential swirl component;
- said premix chamber having an inlet means to supply inlet air to said premix chamber;
- air directing means in said inlet air means for directing said inlet air with a tangential swirl component opposite to said predetermined swirl component whereby the air is directed into and mixed with the projected fuel before the fuel reaches the combustion zone;
- and said wall means for the premix chamber comprising generally planar side walls and at least one conical wall surrounding said slinger so as to redirect the fuel into the path of the inlet air to the premix chamber;
- and said wall means further comprising additional air directional means disposed to direct main primary combustion air into a heavy recirculation swirl of fuel/air mixtures in said combustion zone.
Dependencies are inferred from the claim text.