Flexible Dichtung zur Verwendung zwischen Turbinentriebwerkssegmenten
Anmelder: General Electric Company 🇺🇸
Details
- Veröffentlichungs-Nr.
- EP2481888
- Aktenzeichen
- EP12152940
- Anmeldetag
- 27. Januar 2012
- Veröffentlichung
- 3. September 2014
- Rechtsraum
- EP
- IPC
- F01D11/00F16J15/08
Abstract
The invention relates to a flexible seal for use in a turbine engine and to a respective system and method. The system includes a first turbine segment (32) comprising a first blade (40) coupled to a first shank (36). The system also includes a second turbine segment (32) including a second blade (40) coupled to a second shank (36), as well as an elongated flexible seal (46,60,64,68,80,96) disposed in a gap (42) between the first and second shanks. The elongated flexible seal includes an opening (49) configured to channel a fluid flow into a hollow region of the elongated flexible seal to induce expansion of the elongated flexible seal in the gap.
Anmelder
- Firma
- General Electric Company
- Land
- 🇺🇸 USA
US-amerikanischer Technologiekonzern mit Sitz in Massachusetts. Historisch aktiv in Energieerzeugung, Luftfahrttriebwerken, Medizintechnik und Industrietechnik über verschiedene Geschäftsbereiche.
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