Turbine einer Turbomaschine
Anmelder: General Electric Company 🇺🇸
Details
- Veröffentlichungs-Nr.
- EP2586978
- Aktenzeichen
- EP12189837
- Anmeldetag
- 24. Oktober 2012
- Veröffentlichung
- 2. September 2020
- Erteilung
- 2. September 2020
- Rechtsraum
- EP
- IPC
- F01D5/14F01D9/04
Abstract
A turbine (14) of a turbomachine (10) is provided and includes opposing endwalls (20,30) defining a pathway (40) into which a fluid flow is receivable to flow through the pathway (40); and a nozzle stage (140) at which adjacent nozzles (50) extend across the pathway (40) between the opposing endwalls (20,30) to aerodynamically interact with the fluid flow. The adjacent nozzles are configured to define a throat distribution (60) exhibiting endwall throat decambering and pitchline throat overcambering.
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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