Airfoil shape for a turbine nozzle
Patent
·
OSTI ID:874479
- Schenectady, NY
- Cohoes, NY
- Simpsonville, SC
A first-stage nozzle vane includes an airfoil having a profile according to Table I. The annulus profile of the hot gas path is defined in conjunction with the airfoil profile and the profile of the inner and outer walls by the Cartesian coordinate values given in Tables I and II, respectively. The airfoil is a three-dimensional bowed design, both in the airfoil body and in the trailing edge. The airfoil is steam and air-cooled by flowing cooling mediums through cavities extending in the vane between inner and outer walls.
- Research Organization:
- General Electric Company (Schenectady, NY)
- DOE Contract Number:
- FC21-95MC31176
- Assignee:
- General Electric Company (Schenectady, NY)
- Patent Number(s):
- US 6398489
- OSTI ID:
- 874479
- Country of Publication:
- United States
- Language:
- English
Similar Records
Cooling circuit for steam and air-cooled turbine nozzle stage
Film cooling air pocket in a closed loop cooled airfoil
Exit chimney joint and method of forming the joint for closed circuit steam cooled gas turbine nozzles
Patent
·
Mon Dec 31 23:00:00 EST 2001
·
OSTI ID:874517
Film cooling air pocket in a closed loop cooled airfoil
Patent
·
Mon Dec 31 23:00:00 EST 2001
·
OSTI ID:874656
Exit chimney joint and method of forming the joint for closed circuit steam cooled gas turbine nozzles
Patent
·
Mon Dec 31 23:00:00 EST 2001
·
OSTI ID:874605