DOE Patents title logo U.S. Department of Energy
Office of Scientific and Technical Information

Title: Turbine airfoil fabricated from tapered extrusions

Abstract

An airfoil (30) and fabrication process for turbine blades with cooling channels (26). Tapered tubes (32A-32D) are bonded together in a parallel sequence, forming a leading edge (21), a trailing edge (22), and pressure and suction side walls (23, 24) connected by internal ribs (25). The tapered tubes may be extruded without camber to simplify the extrusion process, then bonded along matching surfaces (34), forming a non-cambered airfoil (28), which may be cambered in a hot forming process and cut (48) to length. The tubes may have tapered walls that are thinner at the blade tip (T1) than at the base (T2), reducing mass. A cap (50) may be attached to the blade tip. A mounting lug (58) may be forged (60) on the airfoil base and then machined, completing the blade for mounting in a turbine rotor disk.

Inventors:
Issue Date:
Research Org.:
Siemens Energy, Inc. (Orlando, FL)
Sponsoring Org.:
USDOE
OSTI Identifier:
1087894
Patent Number(s):
8485787
Application Number:
12/555,096
Assignee:
Siemens Energy, Inc. (Orlando, FL)
Patent Classifications (CPCs):
B - PERFORMING OPERATIONS B21 - MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL B21C - MANUFACTURE OF METAL SHEETS, WIRE, RODS, TUBES OR PROFILES, OTHERWISE THAN BY ROLLING
B - PERFORMING OPERATIONS B21 - MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL B21J - FORGING
DOE Contract Number:  
FC26-05NT42644
Resource Type:
Patent
Country of Publication:
United States
Language:
English
Subject:
33 ADVANCED PROPULSION SYSTEMS

Citation Formats

Marra, John J. Turbine airfoil fabricated from tapered extrusions. United States: N. p., 2013. Web.
Marra, John J. Turbine airfoil fabricated from tapered extrusions. United States.
Marra, John J. Tue . "Turbine airfoil fabricated from tapered extrusions". United States. https://www.osti.gov/servlets/purl/1087894.
@article{osti_1087894,
title = {Turbine airfoil fabricated from tapered extrusions},
author = {Marra, John J},
abstractNote = {An airfoil (30) and fabrication process for turbine blades with cooling channels (26). Tapered tubes (32A-32D) are bonded together in a parallel sequence, forming a leading edge (21), a trailing edge (22), and pressure and suction side walls (23, 24) connected by internal ribs (25). The tapered tubes may be extruded without camber to simplify the extrusion process, then bonded along matching surfaces (34), forming a non-cambered airfoil (28), which may be cambered in a hot forming process and cut (48) to length. The tubes may have tapered walls that are thinner at the blade tip (T1) than at the base (T2), reducing mass. A cap (50) may be attached to the blade tip. A mounting lug (58) may be forged (60) on the airfoil base and then machined, completing the blade for mounting in a turbine rotor disk.},
doi = {},
journal = {},
number = ,
volume = ,
place = {United States},
year = {2013},
month = {7}
}

Works referenced in this record:

Method of Fabricating Airfoils
patent, October 1948


Tapered hollow pole extruder
patent, December 2008


Stitched composite fan blade
patent, August 2002


Ceramic matrix composite structure having integral cooling passages and method of manufacture
patent, June 2004


Method of Fabricating Airfoils
patent, July 1963


Photoetched cooling slots for diffusion bonded airfoils
patent, January 1993


Variable section extrusion die set and variable extrusion molding method
patent, November 1999


SPF/DB hollow core fan blade
patent, August 1993


Vertical axis wind turbine with pultruded blades
patent, March 1996


Thin wall cooling system
patent, November 2002