F - Mech Eng,Light,Heat,Weapons – 23 – D
Patent
F - Mech Eng,Light,Heat,Weapons
23
D
F23D 14/12 (2006.01) F23D 14/16 (2006.01) F23R 3/28 (2006.01)
Patent
CA 2409780
A segmented (A, B, C) radiant burner permits modulation of thermal output by independent control of fuel gas flow (66, 67, 68) to each segment. The burner features a porous fiber burner face (54)optionally having dual porosities, and a metal liner (57) providing a compact combustion zone. The burner is ideal for gas turbines because the fuel flow (66, 67, 68) can be controlled independently of the air flow through the plenums (51, 52, 53) into the combustion zone (75).
L'invention concerne un brûleur rayonnant segmenté (A, B, C) permettant de moduler l'émission thermique par commande indépendante du flux de gaz combustible (66, 67, 68) sur chaque segment. Le brûleur selon l'invention comporte un orifice en fibres poreuses (54) présentant éventuellement des porosités doubles, ainsi qu'une gaine métallique (57) créant une zone de combustion compacte. Ledit brûleur se révèle être parfaitement adapté à des turbines à gaz puisque le flux de combustible (66, 67, 68) peut être commandé indépendamment du flux d'air s'écoulant au travers de la chambre de distribution (51, 52, 53) dans la zone de combustion (75).
Kendall Robert M.
Smith Scott H.
Alzeta Corporation
Gowling Lafleur Henderson Llp
LandOfFree
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