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

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

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