PRE-SWIRLER ADJUSTABILITY IN GAS TURBINE ENGINE
A gas turbine engine having a pre-swirler (400) adjustability is presented. The pre-swirler includes a pre-swirler insert (420) installed in a component enclosed by a cover (12, 16). The component includes an inner compressor exit diffusor (222) enclosed by an outer casing (12) or a shaft cover (16)...
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Format: | Patent |
Sprache: | eng ; fre |
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