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

Rodriguez, Jose L.

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

Patent · Tue Sep 15 00:00:00 EDT 2015

OSTI ID:1214598

Rodriguez, Jose L.

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.

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Research Organization:: Siemens Energy, Inc., Orlando, FL (United States)

Sponsoring Organization:: USDOE

DOE Contract Number:: FC26-05NT42644

Assignee:: Siemens Energy, Inc. (Orlando, FL)

Patent Number(s):: 9,134,029

Application Number:: 14/024,892

OSTI ID:: 1214598

Resource Relation:: Patent File Date: 2013 Sep 12

Country of Publication:: United States

Language:: English

References (18)

Turbojet Aircraft Engine with Thrust Augmentation Hall, James R.; Singelmann, Dietrich E. https://doi.org/https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/2857740 US Patent Document 2857740	patent	October 1958
Turbine engine with combustor premix system Teets, J. Michael https://doi.org/https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/4429527 US Patent Document 4,429,527	patent	February 1984
Gas turbine engine cooling airflow modulator Hull, Peter R. https://doi.org/https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/4462204 US Patent Document 4,462,204	patent	July 1984
Gas turbine engine operating process Paul, Marius A. https://doi.org/https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/4845941 US Patent Document 4,845,941	patent	July 1989
Gas turbine engine cooling supply circuit Bourneuf, John J.; Lenahan, Dean T.; Demers, Daniel Edward https://doi.org/https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/5555721 US Patent Document 5,555,721	patent	September 1996
Deswirler system for centrifugal compressor Moussa, Zaher Milad https://doi.org/https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/6279322 US Patent Document 6,279,322	patent	August 2001
Discrete passage diffuser Roberts, Douglas Allan; Leblanc, Andre; Kacker, Suresh Chandra https://doi.org/https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/6589015 US Patent Document 6,589,015	patent	July 2003
Turbine engine having turbine cooled with diverted compressor intermediate pressure air Liu, Xiaoliu https://doi.org/https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/6647730 US Patent Document 6,647,730	patent	November 2003
Hybrid vane island diffuser Sasu, Ioan; Roberts, Doug; Morenko, Oleg https://doi.org/https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/7025566 US Patent Document 7,025,566	patent	April 2006
System for ventilating a combustion chamber wall in a turbomachine Commaret, Patrice Andre; Hernandez, Didier Hippolyte; Locatelli, David https://doi.org/https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/7827798 US Patent Document 7,827,798	patent	November 2010
Ceramic regenerator for a gas turbine engine Wilson, Jr., Jack W.; Ryznic, John E. https://doi.org/https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/7861510 US Patent Document 7,861,510	patent	January 2011
Cooling structure for outer surface of a gas turbine case Shteyman, Yevgeniy; Tsai, Frank; Marshall, James F. https://doi.org/https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/8079804 US Patent Document 8,079,804	patent	December 2011
Turbine cooling air from a centrifugal compressor Ottaviano, Marcus Joseph; Parks, Robert John; Noon, John Lawrence https://doi.org/https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/8087249 US Patent Document 8,087,249	patent	January 2012
Compressor diffuser Schott, Carl Gerard; Widener, Stanley Kevin; Salunkhe, Anil L. https://doi.org/https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/8133017 US Patent Document 8,133,017	patent	March 2012
Diffuser-nozzle assembly for a turbomachine Hernandez, Didier Hippolyte; Lunel, Romain Nicolas https://doi.org/https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/8142148 US Patent Document 8,142,148	patent	March 2012
Assembly for directing combustion gas Charron, Richard C.; Nordlund, Raymond S.; Morrison, Jay A. https://doi.org/https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/8276389 US Patent Document 8,276,389	patent	October 2012
Casing of a Gas Turbine Engine Maltson, John David https://doi.org/https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/20100031673 US Patent Application 12/524766; 20100031673	patent-application	February 2010
Tangential Combustor Johns, David; Humanchuk, Craig https://doi.org/https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/20110259015 US Patent Application 12/768385; 20110259015	patent-application	October 2011

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