skip to main content
OSTI.GOV title logo U.S. Department of Energy
Office of Scientific and Technical Information

Title: Closed-loop air cooling system for a turbine engine

Abstract

Method and apparatus are disclosed for providing a closed-loop air cooling system for a turbine engine. The method and apparatus provide for bleeding pressurized air from a gas turbine engine compressor for use in cooling the turbine components. The compressed air is cascaded through the various stages of the turbine. At each stage a portion of the compressed air is returned to the compressor where useful work is recovered.

Inventors:
 [1]
  1. Winter Springs, FL
Publication Date:
Research Org.:
Westinghouse Electric Corp., Pittsburgh, PA (United States)
OSTI Identifier:
873132
Patent Number(s):
US 6098395
Assignee:
Siemens Westinghouse Power Corporation (Orlando, FL)
DOE Contract Number:  
AC21-93MC30247
Resource Type:
Patent
Country of Publication:
United States
Language:
English
Subject:
closed-loop; air; cooling; turbine; engine; method; apparatus; disclosed; providing; provide; bleeding; pressurized; gas; compressor; components; compressed; cascaded; various; stages; stage; portion; returned; useful; recovered; pressurized air; compressed air; turbine engine; gas turbine; turbine components; air cooling; turbine component; closed-loop air; /60/

Citation Formats

North, William Edward. Closed-loop air cooling system for a turbine engine. United States: N. p., 2000. Web.
North, William Edward. Closed-loop air cooling system for a turbine engine. United States.
North, William Edward. 2000. "Closed-loop air cooling system for a turbine engine". United States. https://www.osti.gov/servlets/purl/873132.
@article{osti_873132,
title = {Closed-loop air cooling system for a turbine engine},
author = {North, William Edward},
abstractNote = {Method and apparatus are disclosed for providing a closed-loop air cooling system for a turbine engine. The method and apparatus provide for bleeding pressurized air from a gas turbine engine compressor for use in cooling the turbine components. The compressed air is cascaded through the various stages of the turbine. At each stage a portion of the compressed air is returned to the compressor where useful work is recovered.},
doi = {},
url = {https://www.osti.gov/biblio/873132}, journal = {},
number = ,
volume = ,
place = {United States},
year = {2000},
month = {1}
}