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US08220271B2 Fuel lance for a gas turbine engine including outer helical grooves 有权
用于包括外螺旋槽的燃气涡轮发动机的燃料喷枪

Fuel lance for a gas turbine engine including outer helical grooves
Abstract:
A fuel lance (7) for introducing fuel into a gas flow in a combustor (1) of a gas turbine engine includes a region of the lance (7) through which the fuel is introduced into the gas flow having a generally helical formation (12).
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