Invention Grant
US06775985B2 Support assembly for a gas turbine engine combustor 失效
用于燃气涡轮发动机燃烧器的支撑组件

Support assembly for a gas turbine engine combustor
Abstract:
A support assembly for a gas turbine engine combustor including an inner liner and an inner casing spaced therefrom, wherein a longitudinal centerline axis extends through the gas turbine engine. The support assembly includes an annular inner support cone located adjacent an aft end of said inner liner, an annular nozzle support connected to the inner support cone, and a plurality of support members connected at a first end to a forward end of the inner liner and connected at a second end to the inner support cone.
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