Global to push GA events into
skip to main content

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

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