INFLOW SEGMENT FOR A TURBOMACHINE

The invention relates to a turbomachine comprising an inflow segment (21) which carries an inflow segment vane (27) and bores (29) a partial mass flow (M) arriving through these bores (29) at a relief space (30) and leading to a cooling system.

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Bibliographic Details
Main Authors MUSCH CHRISTIAN, FÖRSTER INGO, ZANDER UWE
Format Patent
LanguageEnglish
Published 21.08.2015
Subjects
BLASTING
ENGINE PLANTS IN GENERAL
HEATING
LIGHTING
MACHINES OR ENGINES IN GENERAL
MECHANICAL ENGINEERING
NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES
STEAM ENGINES
WEAPONS
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Summary:The invention relates to a turbomachine comprising an inflow segment (21) which carries an inflow segment vane (27) and bores (29) a partial mass flow (M) arriving through these bores (29) at a relief space (30) and leading to a cooling system.
Bibliography:Application Number: IN2014DELNP10499