Component part of especially turbo-engine has protective shroud installed around sleeve element to protect section of sleeve element protruding from cooling passage against effects of surrounding flow

The component part of especially a turbo-engine, has a cooling passage (109) with an outlet opening (117) and a sleeve element (116) divided into a first and a second section, whereby the first section is connected to the outlet opening and the second section protruding from the cooling passage. To...

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Bibliographische Detailangaben

1. Verfasser:	TSCHUOR, REMIGI
Format:	Patent
Sprache:	eng ; ger
Schlagworte:	BLASTING ENGINE PLANTS IN GENERAL HEATING INDEXING SCHEME FOR ASPECTS RELATING TONON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES ORJET-PROPULSION PLANTS INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUSSUBCLASSES OF CLASSES F01-F04 LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES STEAM ENGINES WEAPONS
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