Brennkammeranordnung zur Verwendung in einem Gasturbinenmotor und Herstellungsverfahren dafür
Anmelder: General Electric Company 🇺🇸
Details
- Veröffentlichungs-Nr.
- EP2489937
- Aktenzeichen
- EP12155362
- Anmeldetag
- 14. Februar 2012
- Veröffentlichung
- 12. April 2017
- Erteilung
- 12. April 2017
- Rechtsraum
- EP
- IPC
- F23R3/00F01D9/02F23R3/60
Abstract
A combustor assembly (26) includes a combustor liner (38) defining a combustion chamber (36) there within, and a transition piece (64) including a forward portion (76) coupled to the combustion liner and an aft portion (68) extending from the forward portion, the aft portion including a transition piece frame (66). The transition piece frame includes an upstream surface (98), a downstream surface (100), and a radially inner surface (102) extending between the upstream and downstream surfaces, the radially inner surface comprises a leading edge (110) extending between the radially inner surface and the upstream surface, and a plurality of first cooling passages (132) extending from the upstream surface to the downstream surface, each of the first cooling passages oriented obliquely with respect to the leading edge from the upstream surface towards the downstream surface.
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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