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

Title: Radial midframe baffle for can-annular combustor arrangement having tangentially oriented combustor cans

Abstract

A can-annular gas turbine engine combustion arrangement (10), including: a combustor can (12) comprising a combustor inlet (38) and a combustor outlet circumferentially and axially offset from the combustor inlet; an outer casing (24) defining a plenum (22) in which the combustor can is disposed; and baffles (70) configured to divide the plenum into radial sectors (72) and configured to inhibit circumferential motion of compressed air (16) within the plenum.

Inventors:
Publication Date:
Research Org.:
Siemens Energy, Inc., Orlando, FL (United States)
Sponsoring Org.:
USDOE
OSTI Identifier:
1214598
Patent Number(s):
9,134,029
Application Number:
14/024,892
Assignee:
Siemens Energy, Inc. (Orlando, FL) NETL
DOE Contract Number:  
FC26-05NT42644
Resource Type:
Patent
Resource Relation:
Patent File Date: 2013 Sep 12
Country of Publication:
United States
Language:
English
Subject:
33 ADVANCED PROPULSION SYSTEMS

Citation Formats

Rodriguez, Jose L. Radial midframe baffle for can-annular combustor arrangement having tangentially oriented combustor cans. United States: N. p., 2015. Web.
Rodriguez, Jose L. Radial midframe baffle for can-annular combustor arrangement having tangentially oriented combustor cans. United States.
Rodriguez, Jose L. Tue . "Radial midframe baffle for can-annular combustor arrangement having tangentially oriented combustor cans". United States. https://www.osti.gov/servlets/purl/1214598.
@article{osti_1214598,
title = {Radial midframe baffle for can-annular combustor arrangement having tangentially oriented combustor cans},
author = {Rodriguez, Jose L.},
abstractNote = {A can-annular gas turbine engine combustion arrangement (10), including: a combustor can (12) comprising a combustor inlet (38) and a combustor outlet circumferentially and axially offset from the combustor inlet; an outer casing (24) defining a plenum (22) in which the combustor can is disposed; and baffles (70) configured to divide the plenum into radial sectors (72) and configured to inhibit circumferential motion of compressed air (16) within the plenum.},
doi = {},
journal = {},
number = ,
volume = ,
place = {United States},
year = {2015},
month = {9}
}

Patent:

Save / Share: