Radial turbine rotor with complex cooling channels and method of making same
Abstract
A turbine rotor includes a base and a plurality of blades. The base and the blades curve such that radially outward portions of the base and the blades extend in a direction with a greater component in a radial direction than in an axial direction. Radially central portions of the base and the blade extend in a direction with the two components being closer. Radially inner sections of the base and the blades extend in a direction with a greater component in the axial direction than in a radial direction. There is a cooling channel arrangement in the turbine rotor. The cooling channel arrangement includes impingement cooling for a nose and serpentine passages for cooling sections of the platform circumferentially intermediate the blades, and distinct serpentine passages for cooling the plurality of blades. A turbomachine and method are also disclosed.
- Inventors:
- Issue Date:
- Research Org.:
- Hamilton Sundstrand Corporation, Charlotte, NC (United States)
- Sponsoring Org.:
- USDOE
- OSTI Identifier:
- 1987174
- Patent Number(s):
- 11591916
- Application Number:
- 17/366,493
- Assignee:
- Hamilton Sundstrand Corporation (Charlotte, NC)
- Patent Classifications (CPCs):
-
B - PERFORMING OPERATIONS B33 - ADDITIVE MANUFACTURING TECHNOLOGY B33Y - ADDITIVE MANUFACTURING, i.e. MANUFACTURING OF THREE-DIMENSIONAL [3-D] OBJECTS BY ADDITIVE DEPOSITION, ADDITIVE AGGLOMERATION OR ADDITIVE LAYERING, e.g. BY 3-D PRINTING, STEREOLITHOGRAPHY OR SELECTIVE LASER SINTERING
F - MECHANICAL ENGINEERING F01 - MACHINES OR ENGINES IN GENERAL F01D - NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- DOE Contract Number:
- EE0009138
- Resource Type:
- Patent
- Resource Relation:
- Patent File Date: 07/02/2021
- Country of Publication:
- United States
- Language:
- English
Citation Formats
Dai, Zhongtao, Ranjan, Ram, and Dold, Robert H. Radial turbine rotor with complex cooling channels and method of making same. United States: N. p., 2023.
Web.
Dai, Zhongtao, Ranjan, Ram, & Dold, Robert H. Radial turbine rotor with complex cooling channels and method of making same. United States.
Dai, Zhongtao, Ranjan, Ram, and Dold, Robert H. Tue .
"Radial turbine rotor with complex cooling channels and method of making same". United States. https://www.osti.gov/servlets/purl/1987174.
@article{osti_1987174,
title = {Radial turbine rotor with complex cooling channels and method of making same},
author = {Dai, Zhongtao and Ranjan, Ram and Dold, Robert H.},
abstractNote = {A turbine rotor includes a base and a plurality of blades. The base and the blades curve such that radially outward portions of the base and the blades extend in a direction with a greater component in a radial direction than in an axial direction. Radially central portions of the base and the blade extend in a direction with the two components being closer. Radially inner sections of the base and the blades extend in a direction with a greater component in the axial direction than in a radial direction. There is a cooling channel arrangement in the turbine rotor. The cooling channel arrangement includes impingement cooling for a nose and serpentine passages for cooling sections of the platform circumferentially intermediate the blades, and distinct serpentine passages for cooling the plurality of blades. A turbomachine and method are also disclosed.},
doi = {},
journal = {},
number = ,
volume = ,
place = {United States},
year = {Tue Feb 28 00:00:00 EST 2023},
month = {Tue Feb 28 00:00:00 EST 2023}
}
Save to My Library
You must Sign In or Create an Account in order to save documents to your library.
Works referenced in this record:
Diverging-converging cooling passage for a turbine blade
patent, April 2019
- Smoke, Jason; Jan, David K.; Miner, Amandine
- US Patent Document 10,260,355
Advanced Automated Fabrication System and Methods for Thermal and Mechanical Components Utilizing Quadratic or Squared Hybrid Direct Laser Sintering, Direct Metal Laser Sintering, CNC, Thermal Spraying, Direct Metal Deposition and Frictional Stir Welding. Cross-Reference to Related Applications
patent-application, October 2020
- Friesth, Kevin
- US Patent Application 16/764910; 20200338639
Impingement-Cooled Turbine Rotor
patent-application, November 2014
- Jan, David K.; Miner, Amandine
- US Patent Application 13/892828; 20140348664
Overhung Turbine and Generator System with Turbine Cartridge
patent-application, February 2015
- Fairman, Kevin; Di Bella, Francis A.; Japikse, David
- US Patent Application 13/937,978; 2015/0037136 Al
Turbine Wheel for a Radial Turbine
patent-application, April 2017
- Schwarz, Lukas
- US Patent Application 15/290236; 20170107821
Turbine disc cooling arrangement
patent, August 2014
- Tibbott, Ian; Jackson, Dougal Richard; Clarkson, Rory J.
- US Patent Document 8,807,942
Gas turbine with secondary cooling means
patent, January 1979
- Corsmeier, Robert J.
- US Patent Document 4,136,516
Turbine for Use with at Least Two Working Fluids
patent-application, August 2020
- Copeland, Colin Douglas; Ceen, Robert; Jones, Simon Lloyd
- US Patent Application 16/607231; 20200263568