Igniter with porous sleeve

F - Mech Eng,Light,Heat,Weapons – 23 – D

Patent

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Details

F23D 11/42 (2006.01) F02C 7/264 (2006.01) F23R 3/32 (2006.01)

Patent

CA 2335355

The igniter for the combustor in a gas turbine engine includes a tubular member extending beyond the igniter tip, wherein the tubular member is a porous ceramic or high temperature nickel alloy. Fuel is fed to the bore of the tubular member by capillary action through the porous material of the tubular member and air passes through the porous tubular member to the bore.

Cet allumeur, destiné à la chambre de combustion d'un moteur à turbine à gaz, comprend un élément tubulaire s'étendant au-delà du bout de l'allumeur, et il est caractérisé en ce que cet élément tubulaire est un alliage poreux de céramique ou de nickel haute température. Le carburant est alimenté vers l'alésage de l'élément tubulaire par action capillaire à travers le matériau poreux de cet élément, l'air passant également à travers cet élément tubulaire poreux en direction de l'alésage.

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