WIRE SEAL

The invention concerns a wire seal (10) for sealing a gap (36) between two components of a gas turbine, the wire seal (10) comprising a first core (12, 25) and a second core (14, 26) spaced apart from one another, a wire pack (22) extending around the first core and the second core, and a fastener f...

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Bibliographische Detailangaben
Hauptverfasser:	Tibos, Stacie, Heaven, Sarah, Justl, Sascha
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	BLASTING COMBUSTION APPARATUS COMBUSTION ENGINES COMBUSTION PROCESSES ENGINE PLANTS IN GENERAL GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS 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 JET-PROPULSION PLANTS LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES STEAM ENGINES WEAPONS
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Beschreibung
Zusammenfassung:	The invention concerns a wire seal (10) for sealing a gap (36) between two components of a gas turbine, the wire seal (10) comprising a first core (12, 25) and a second core (14, 26) spaced apart from one another, a wire pack (22) extending around the first core and the second core, and a fastener for securing the wire pack to the first core and the second core, wherein the wire seal (10) is curved. Various embodiments are disclosed, including various types of fastener. A method of manufacturing a wire seal is also disclosed.