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

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:: Rodriguez, Jose L.

Issue Date:: 2015-09-15

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

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Works referenced in this record:

Cooling structure for outer surface of a gas turbine case
patent, December 2011

Shteyman, Yevgeniy; Tsai, Frank; Marshall, James
US Patent Document 8,079,804
URL: http://patft.uspto.gov/netacgi/nph-Parser?Sect2=PTO1&Sect2=HITOFF&p=1&u=/netahtml/PTO/search-bool.html&r=1&f=G&l=50&d=PALL&RefSrch=yes&Query=PN/8079804

Assembly for directing combustion gas
patent, October 2012

Charron, Richard C.; Nordlun, Raymond S.; Morrison, Jay A.
US Patent Document 8,276,389
URL: http://patft.uspto.gov/netacgi/nph-Parser?Sect2=PTO1&Sect2=HITOFF&p=1&u=/netahtml/PTO/search-bool.html&r=1&f=G&l=50&d=PALL&RefSrch=yes&Query=PN/8276389

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