| FR2253389A5
              (pm)
            
            * | 1973-12-04 | 1975-06-27 | France Etat |  | 
        
          | US3925002A
              (en)
            
            * | 1974-11-11 | 1975-12-09 | Gen Motors Corp | Air preheating combustion apparatus | 
        
          | US3938324A
              (en)
            
            * | 1974-12-12 | 1976-02-17 | General Motors Corporation | Premix combustor with flow constricting baffle between combustion and dilution zones | 
        
          | US3930368A
              (en)
            
            * | 1974-12-12 | 1976-01-06 | General Motors Corporation | Combustion liner air valve | 
        
          | US3958416A
              (en)
            
            * | 1974-12-12 | 1976-05-25 | General Motors Corporation | Combustion apparatus | 
        
          | US4045956A
              (en)
            
            * | 1974-12-18 | 1977-09-06 | United Technologies Corporation | Low emission combustion chamber | 
        
          | US3973395A
              (en)
            
            * | 1974-12-18 | 1976-08-10 | United Technologies Corporation | Low emission combustion chamber | 
        
          | US4058977A
              (en)
            
            * | 1974-12-18 | 1977-11-22 | United Technologies Corporation | Low emission combustion chamber | 
        
          | DE2629761A1
              (de)
            
            * | 1976-07-02 | 1978-01-05 | Volkswagenwerk Ag | Brennkammer fuer gasturbinen | 
        
          | GB1592858A
              (en)
            
            * | 1977-01-21 | 1981-07-08 | Rolls Royce | Combustion equipment for gas turbine engines | 
        
          | US4246757A
              (en)
            
            * | 1979-03-27 | 1981-01-27 | General Electric Company | Combustor including a cyclone prechamber and combustion process for gas turbines fired with liquid fuel | 
        
          | US4269466A
              (en)
            
            * | 1979-11-23 | 1981-05-26 | Amp Incorporated | Connector and strain relief for flat transmission cable | 
        
          | US4263780A
              (en)
            
            * | 1979-09-28 | 1981-04-28 | General Motors Corporation | Lean prechamber outflow combustor with sets of primary air entrances | 
        
          | DE2949388A1
              (de)
            
            * | 1979-12-07 | 1981-06-11 | Kraftwerk Union AG, 4330 Mülheim | Brennkammer fuer gasturbinen und verfahren zum betrieb der brennkammer | 
        
          | FR2471480A1
              (fr)
            
            * | 1979-12-13 | 1981-06-19 | Snecma | Dispositif d'injection pour chambre a combustion de moteur a turbine | 
        
          | DE3164647D1
              (en)
            
            * | 1980-03-05 | 1984-08-16 | Hitachi Ltd | A gas turbine combustor | 
        
          | US4735044A
              (en)
            
            * | 1980-11-25 | 1988-04-05 | General Electric Company | Dual fuel path stem for a gas turbine engine | 
        
          | US4467610A
              (en)
            
            * | 1981-04-17 | 1984-08-28 | General Electric Company | Gas turbine fuel system | 
        
          | US4404806A
              (en)
            
            * | 1981-09-04 | 1983-09-20 | General Motors Corporation | Gas turbine prechamber and fuel manifold structure | 
        
          | DE3209135A1
              (de)
            
            * | 1982-03-12 | 1983-09-15 | Kraftwerk Union AG, 4330 Mülheim | Gasturbinenbrennkammer | 
        
          | JP2644745B2
              (ja)
            
            * | 1987-03-06 | 1997-08-25 | 株式会社日立製作所 | ガスタービン用燃焼器 | 
        
          | JPH0816531B2
              (ja)
            
            * | 1987-04-03 | 1996-02-21 | 株式会社日立製作所 | ガスタ−ビン燃焼器 | 
        
          | JP2516822Y2
              (ja)
            
            * | 1988-08-04 | 1996-11-13 | 川崎重工業株式会社 | ガスタービン用燃焼器 | 
        
          | DE4435266A1
              (de)
            
            * | 1994-10-01 | 1996-04-04 | Abb Management Ag | Brenner | 
        
          | US5669218A
              (en)
            
            * | 1995-05-31 | 1997-09-23 | Dresser-Rand Company | Premix fuel nozzle | 
        
          | US5813232A
              (en)
            
            * | 1995-06-05 | 1998-09-29 | Allison Engine Company, Inc. | Dry low emission combustor for gas turbine engines | 
        
          | GB2351343A
              (en)
            
            * | 1999-06-22 | 2000-12-27 | Alstom Gas Turbines Ltd | Telescopically-moveable combustion chamber | 
        
          | US6539721B2
              (en)
            
            * | 2001-07-10 | 2003-04-01 | Pratt & Whitney Canada Corp. | Gas-liquid premixer | 
        
          | SE523082C2
              (sv)
            
            * | 2001-11-20 | 2004-03-23 | Volvo Aero Corp | Anordning vid en brännkammare hos en gasturbin för reglering av inflöde av gas till brännkammarens förbränningszon | 
        
          | US7028484B2
              (en) | 2002-08-30 | 2006-04-18 | Pratt & Whitney Canada Corp. | Nested channel ducts for nozzle construction and the like | 
        
          | US7654088B2
              (en)
            
            * | 2004-02-27 | 2010-02-02 | Pratt & Whitney Canada Corp. | Dual conduit fuel manifold for gas turbine engine | 
        
          | US20060156733A1
              (en) | 2005-01-14 | 2006-07-20 | Pratt & Whitney Canada Corp. | Integral heater for fuel conveying member | 
        
          | US7565807B2
              (en) | 2005-01-18 | 2009-07-28 | Pratt & Whitney Canada Corp. | Heat shield for a fuel manifold and method | 
        
          | US7533531B2
              (en) | 2005-04-01 | 2009-05-19 | Pratt & Whitney Canada Corp. | Internal fuel manifold with airblast nozzles | 
        
          | US7540157B2
              (en) | 2005-06-14 | 2009-06-02 | Pratt & Whitney Canada Corp. | Internally mounted fuel manifold with support pins | 
        
          | US7559201B2
              (en) | 2005-09-08 | 2009-07-14 | Pratt & Whitney Canada Corp. | Redundant fuel manifold sealing arrangement | 
        
          | DE102005062079A1
              (de)
            
            * | 2005-12-22 | 2007-07-12 | Rolls-Royce Deutschland Ltd & Co Kg | Magervormischbrenner mit einer Zerstäuberlippe | 
        
          | US7607226B2
              (en) | 2006-03-03 | 2009-10-27 | Pratt & Whitney Canada Corp. | Internal fuel manifold with turned channel having a variable cross-sectional area | 
        
          | US7942002B2
              (en) | 2006-03-03 | 2011-05-17 | Pratt & Whitney Canada Corp. | Fuel conveying member with side-brazed sealing members | 
        
          | US7854120B2
              (en) | 2006-03-03 | 2010-12-21 | Pratt & Whitney Canada Corp. | Fuel manifold with reduced losses | 
        
          | US7624577B2
              (en) | 2006-03-31 | 2009-12-01 | Pratt & Whitney Canada Corp. | Gas turbine engine combustor with improved cooling | 
        
          | US8096130B2
              (en) | 2006-07-20 | 2012-01-17 | Pratt & Whitney Canada Corp. | Fuel conveying member for a gas turbine engine | 
        
          | US8353166B2
              (en) | 2006-08-18 | 2013-01-15 | Pratt & Whitney Canada Corp. | Gas turbine combustor and fuel manifold mounting arrangement | 
        
          | US7765808B2
              (en) | 2006-08-22 | 2010-08-03 | Pratt & Whitney Canada Corp. | Optimized internal manifold heat shield attachment | 
        
          | US8033113B2
              (en) | 2006-08-31 | 2011-10-11 | Pratt & Whitney Canada Corp. | Fuel injection system for a gas turbine engine | 
        
          | US7703289B2
              (en) | 2006-09-18 | 2010-04-27 | Pratt & Whitney Canada Corp. | Internal fuel manifold having temperature reduction feature | 
        
          | US7775047B2
              (en) | 2006-09-22 | 2010-08-17 | Pratt & Whitney Canada Corp. | Heat shield with stress relieving feature | 
        
          | US7926286B2
              (en) | 2006-09-26 | 2011-04-19 | Pratt & Whitney Canada Corp. | Heat shield for a fuel manifold | 
        
          | US8572976B2
              (en) | 2006-10-04 | 2013-11-05 | Pratt & Whitney Canada Corp. | Reduced stress internal manifold heat shield attachment | 
        
          | US7716933B2
              (en)
            
            * | 2006-10-04 | 2010-05-18 | Pratt & Whitney Canada Corp. | Multi-channel fuel manifold | 
        
          | US20080104961A1
              (en)
            
            * | 2006-11-08 | 2008-05-08 | Ronald Scott Bunker | Method and apparatus for enhanced mixing in premixing devices | 
        
          | US7856825B2
              (en) | 2007-05-16 | 2010-12-28 | Pratt & Whitney Canada Corp. | Redundant mounting system for an internal fuel manifold | 
        
          | US8096104B2
              (en)
            
            * | 2007-05-31 | 2012-01-17 | United Technologies Corporation | Fluidic vectoring for exhaust nozzle | 
        
          | US8146365B2
              (en) | 2007-06-14 | 2012-04-03 | Pratt & Whitney Canada Corp. | Fuel nozzle providing shaped fuel spray | 
        
          | US8096132B2
              (en)
            
            * | 2008-02-20 | 2012-01-17 | Flexenergy Energy Systems, Inc. | Air-cooled swirlerhead | 
        
          | US8887390B2
              (en) | 2008-08-15 | 2014-11-18 | Dresser-Rand Company | Method for correcting downstream deflection in gas turbine nozzles | 
        
          | US9181813B2
              (en) | 2012-07-05 | 2015-11-10 | Siemens Aktiengesellschaft | Air regulation for film cooling and emission control of combustion gas structure | 
        
          | EP3015772B1
              (en)
            
            * | 2014-10-31 | 2020-01-08 | Ansaldo Energia Switzerland AG | Combustor arrangement for a gas turbine | 
        
          | JP2018531395A
              (ja)
            
            * | 2015-07-21 | 2018-10-25 | フルイドセンス インターナショナル インコーポレイテッド | 液体中または空気中の粒子検出システムおよび方法 | 
        
          | US10995699B2
              (en)
            
            * | 2018-02-19 | 2021-05-04 | Mra Systems, Llc. | Thrust reverser cascade | 
        
          | US11592178B2
              (en)
            
            * | 2018-05-15 | 2023-02-28 | Air Products And Chemicals, Inc. | System and method of improving combustion stability in a gas turbine | 
        
          | US10989413B2
              (en)
            
            * | 2019-07-17 | 2021-04-27 | General Electric Company | Axial retention assembly for combustor components of a gas turbine engine | 
        
          | CN112483260A
              (zh)
            
            * | 2020-12-15 | 2021-03-12 | 通化师范学院 | 一种燃气轮机的启动设备 | 
        
          | US11428411B1
              (en) | 2021-05-18 | 2022-08-30 | General Electric Company | Swirler with rifled venturi for dynamics mitigation | 
        
          | US20240263786A1
              (en)
            
            * | 2023-02-02 | 2024-08-08 | Pratt & Whitney Canada Corp. | Central air passage with radial fuel distributor |