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Title: 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:
; ;
Publication Date:
Research Org.:
SIEMENS ENERGY, INC. Orlando, FL (United States)
Sponsoring Org.:
USDOE
OSTI Identifier:
1372665
Patent Number(s):
9,714,611
Application Number:
13/768,038
Assignee:
SIEMENS ENERGY, INC. NETL
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 = {Tue Jul 25 00:00:00 EDT 2017},
month = {Tue Jul 25 00:00:00 EDT 2017}
}

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