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Title: Mid-section of a can-annular gas turbine engine with a radial air flow discharged from the compressor section

Abstract

A midframe portion (213) of a gas turbine engine (210) is presented, and includes a compressor section (212) configured to discharge an air flow (211) directed in a radial direction from an outlet of the compressor section (212). Additionally, the midframe portion (213) includes a manifold (214) to directly couple the air flow (211) from the compressor section (212) outlet to an inlet of a respective combustor head (218) of the midframe portion (213).

Inventors:
; ;
Publication Date:
Research Org.:
SIEMENS ENERGY, INC., Orlando, FL (United States)
Sponsoring Org.:
USDOE
OSTI Identifier:
1330364
Patent Number(s):
9,476,355
Application Number:
13/408,147
Assignee:
SIEMENS ENERGY, INC. (Orlando, FL) NETL
DOE Contract Number:  
FC26-05NT42644
Resource Type:
Patent
Resource Relation:
Patent File Date: 2012 Feb 29
Country of Publication:
United States
Language:
English
Subject:
42 ENGINEERING; 33 ADVANCED PROPULSION SYSTEMS

Citation Formats

Little, David A., McQuiggan, Gerard, and Wasdell, David L. Mid-section of a can-annular gas turbine engine with a radial air flow discharged from the compressor section. United States: N. p., 2016. Web.
Little, David A., McQuiggan, Gerard, & Wasdell, David L. Mid-section of a can-annular gas turbine engine with a radial air flow discharged from the compressor section. United States.
Little, David A., McQuiggan, Gerard, and Wasdell, David L. Tue . "Mid-section of a can-annular gas turbine engine with a radial air flow discharged from the compressor section". United States. https://www.osti.gov/servlets/purl/1330364.
@article{osti_1330364,
title = {Mid-section of a can-annular gas turbine engine with a radial air flow discharged from the compressor section},
author = {Little, David A. and McQuiggan, Gerard and Wasdell, David L.},
abstractNote = {A midframe portion (213) of a gas turbine engine (210) is presented, and includes a compressor section (212) configured to discharge an air flow (211) directed in a radial direction from an outlet of the compressor section (212). Additionally, the midframe portion (213) includes a manifold (214) to directly couple the air flow (211) from the compressor section (212) outlet to an inlet of a respective combustor head (218) of the midframe portion (213).},
doi = {},
journal = {},
number = ,
volume = ,
place = {United States},
year = {2016},
month = {10}
}

Patent:

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