Heat shield manifold system for a midframe case of a gas turbine engine
Abstract
A heat shield manifold system for an inner casing between a compressor and turbine assembly is disclosed. The heat shield manifold system protects the outer case from high temperature compressor discharge air, thereby enabling the outer case extending between a compressor and a turbine assembly to be formed from less expensive materials than otherwise would be required. In addition, the heat shield manifold system may be configured such that compressor bleed air is passed from the compressor into the heat shield manifold system without passing through a conventional flange to flange joint that is susceptible to leakage.
- Inventors:
- Issue Date:
- Research Org.:
- SIEMENS ENERGY, INC. Orlando, FL (United States)
- Sponsoring Org.:
- USDOE
- OSTI Identifier:
- 1372665
- Patent Number(s):
- 9714611
- Application Number:
- 13/768,038
- Assignee:
- SIEMENS ENERGY, INC.
- Patent Classifications (CPCs):
-
F - MECHANICAL ENGINEERING F02 - COMBUSTION ENGINES F02C - GAS-TURBINE PLANTS
F - MECHANICAL ENGINEERING F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04 F05D - INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- DOE Contract Number:
- FC26-05NT42644
- Resource Type:
- Patent
- Resource Relation:
- Patent File Date: 2013 Feb 15
- Country of Publication:
- United States
- Language:
- English
- Subject:
- 42 ENGINEERING; 33 ADVANCED PROPULSION SYSTEMS
Citation Formats
Mayer, Clinton A., Eng, Jesse, and Schopf, Cheryl A. Heat shield manifold system for a midframe case of a gas turbine engine. United States: N. p., 2017.
Web.
Mayer, Clinton A., Eng, Jesse, & Schopf, Cheryl A. Heat shield manifold system for a midframe case of a gas turbine engine. United States.
Mayer, Clinton A., Eng, Jesse, and Schopf, Cheryl A. Tue .
"Heat shield manifold system for a midframe case of a gas turbine engine". United States. https://www.osti.gov/servlets/purl/1372665.
@article{osti_1372665,
title = {Heat shield manifold system for a midframe case of a gas turbine engine},
author = {Mayer, Clinton A. and Eng, Jesse and Schopf, Cheryl A.},
abstractNote = {A heat shield manifold system for an inner casing between a compressor and turbine assembly is disclosed. The heat shield manifold system protects the outer case from high temperature compressor discharge air, thereby enabling the outer case extending between a compressor and a turbine assembly to be formed from less expensive materials than otherwise would be required. In addition, the heat shield manifold system may be configured such that compressor bleed air is passed from the compressor into the heat shield manifold system without passing through a conventional flange to flange joint that is susceptible to leakage.},
doi = {},
journal = {},
number = ,
volume = ,
place = {United States},
year = {2017},
month = {7}
}
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