Passives Kühlsystem für eine Turbomaschine
Anmelder: General Electric Company 🇺🇸
Details
- Veröffentlichungs-Nr.
- EP2484872
- Aktenzeichen
- EP12154127
- Anmeldetag
- 6. Februar 2012
- Veröffentlichung
- 20. April 2016
- Erteilung
- 20. April 2016
- Rechtsraum
- EP
- IPC
- F01D11/10F01D25/12
Abstract
A turbomachine (2) includes a housing (60) having an outer surface (12) and an inner surface (14) that defines an interior portion (15). The housing (60) includes a fluid plenum (62). A rotating member (20, 21, 22)is arranged within the housing (60). The rotating member (20, 21, 22)includes at least one bucket (28, 29, 30) having a base portion and a tip portion (45). A stationary member is mounted to the inner surface (14) of the housing (60) adjacent the tip portion (45) of the at least one bucket (28, 29, 30). At least one fluid passage passes through at least a portion of the stationary member. The at least one fluid passage includes a fluid inlet fluidly coupled to the fluid plenum (62) and a fluid outlet exposed to the interior portion (15). The fluid outlet being configured and disposed to direct a flow of fluid toward the tip portion (45) of the at least one bucket (28, 29, 30).
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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