JPS5342897B2
(en)
*
|
1972-11-09 |
1978-11-15 |
|
|
GB1488666A
(en)
*
|
1973-11-29 |
1977-10-12 |
Agfa Gevaert |
Apparatus for incinerating non-halogenated waste solvents
|
US4036434A
(en)
*
|
1974-07-15 |
1977-07-19 |
Aerojet-General Corporation |
Fluid delivery nozzle with fluid purged face
|
JPS5827235Y2
(en)
*
|
1977-10-17 |
1983-06-13 |
三井液化ガス株式会社 |
Oil and gas co-firing burner
|
US4253301A
(en)
*
|
1978-10-13 |
1981-03-03 |
General Electric Company |
Fuel injection staged sectoral combustor for burning low-BTU fuel gas
|
US4327547A
(en)
*
|
1978-11-23 |
1982-05-04 |
Rolls-Royce Limited |
Fuel injectors
|
GB2050592B
(en)
*
|
1979-06-06 |
1983-03-16 |
Rolls Royce |
Gas turbine
|
US4288980A
(en)
*
|
1979-06-20 |
1981-09-15 |
Brown Boveri Turbomachinery, Inc. |
Combustor for use with gas turbines
|
US4311277A
(en)
*
|
1979-06-20 |
1982-01-19 |
Lucas Industries Limited |
Fuel injector
|
FR2461816A1
(en)
*
|
1979-07-16 |
1981-02-06 |
Lucas Industries Ltd |
Gas turbine engine fuel injector - has passage provided into which gas supply passage opens downstream of air swirler arrangement
|
GB2055186B
(en)
*
|
1979-08-01 |
1983-05-25 |
Rolls Royce |
Gas turbine engine dual fuel injector
|
US4412808A
(en)
*
|
1980-06-19 |
1983-11-01 |
Trw Inc. |
Dual fueled burner gun
|
US4735044A
(en)
*
|
1980-11-25 |
1988-04-05 |
General Electric Company |
Dual fuel path stem for a gas turbine engine
|
GB2102936B
(en)
*
|
1981-07-28 |
1985-02-13 |
Rolls Royce |
Fuel injector for gas turbine engines
|
EP0095788B1
(en)
*
|
1982-05-28 |
1985-12-18 |
BBC Aktiengesellschaft Brown, Boveri & Cie. |
Gas turbine combustion chamber and method of operating it
|
DE3526482C1
(en)
*
|
1985-07-24 |
1986-12-18 |
Deutsche Babcock Werke AG, 4200 Oberhausen |
Burners for burning liquid fuel
|
CH672541A5
(en)
*
|
1986-12-11 |
1989-11-30 |
Bbc Brown Boveri & Cie |
|
US4854127A
(en)
*
|
1988-01-14 |
1989-08-08 |
General Electric Company |
Bimodal swirler injector for a gas turbine combustor
|
US4930703A
(en)
*
|
1988-12-22 |
1990-06-05 |
General Electric Company |
Integral fuel nozzle cover for gas turbine combustor
|
US5203796A
(en)
*
|
1990-08-28 |
1993-04-20 |
General Electric Company |
Two stage v-gutter fuel injection mixer
|
JP2839777B2
(en)
*
|
1991-12-24 |
1998-12-16 |
株式会社東芝 |
Fuel injection nozzle for gas turbine combustor
|
US5222357A
(en)
*
|
1992-01-21 |
1993-06-29 |
Westinghouse Electric Corp. |
Gas turbine dual fuel nozzle
|
IT1263683B
(en)
*
|
1992-08-21 |
1996-08-27 |
Westinghouse Electric Corp |
NOZZLE COMPLEX FOR FUEL FOR A GAS TURBINE
|
US6360992B1
(en)
|
1996-06-28 |
2002-03-26 |
Honeywell International Inc. |
Hybrid deicing system and method of operation
|
US6047926A
(en)
*
|
1996-06-28 |
2000-04-11 |
Alliedsignal Inc. |
Hybrid deicing system and method of operation
|
DE19905995A1
(en)
*
|
1999-02-15 |
2000-08-17 |
Asea Brown Boveri |
Injection lance or nozzle for liquid and gaseous fuel in combustion chamber is part of secondary or tertiary burner around which flows hot gas jet in main flow direction
|
US6547163B1
(en)
*
|
1999-10-01 |
2003-04-15 |
Parker-Hannifin Corporation |
Hybrid atomizing fuel nozzle
|
US6539724B2
(en)
*
|
2001-03-30 |
2003-04-01 |
Delavan Inc |
Airblast fuel atomization system
|
ITFI20010211A1
(en)
*
|
2001-11-09 |
2003-05-09 |
Enel Produzione Spa |
LOW NO NO DIFFUSION FLAME COMBUSTOR FOR GAS TURBINES
|
DE50211068D1
(en)
*
|
2001-12-20 |
2007-11-22 |
Alstom Technology Ltd |
Method for injecting a fuel / air mixture into a combustion chamber
|
GB2404729B
(en)
*
|
2003-08-08 |
2008-01-23 |
Rolls Royce Plc |
Fuel injection
|
DE10353423B3
(en)
*
|
2003-11-15 |
2005-04-14 |
Eads Space Transportation Gmbh |
Rocket motor casing has cooling passages for fuel or liquid oxygen within concentric structure
|
US7117678B2
(en)
*
|
2004-04-02 |
2006-10-10 |
Pratt & Whitney Canada Corp. |
Fuel injector head
|
US7674671B2
(en)
|
2004-12-13 |
2010-03-09 |
Optomec Design Company |
Aerodynamic jetting of aerosolized fluids for fabrication of passive structures
|
US7536862B2
(en)
*
|
2005-09-01 |
2009-05-26 |
General Electric Company |
Fuel nozzle for gas turbine engines
|
EP2002185B8
(en)
*
|
2006-03-31 |
2016-09-14 |
General Electric Technology GmbH |
Fuel lance for a gas turbine plant and a method of operating a fuel lance
|
JP4739275B2
(en)
*
|
2006-08-11 |
2011-08-03 |
Jx日鉱日石エネルギー株式会社 |
Burner
|
US20080078183A1
(en)
*
|
2006-10-03 |
2008-04-03 |
General Electric Company |
Liquid fuel enhancement for natural gas swirl stabilized nozzle and method
|
US7934380B2
(en)
*
|
2006-10-26 |
2011-05-03 |
Rolls-Royce Power Engineering Plc |
Method and apparatus for isolating inactive fuel passages
|
US8015815B2
(en)
*
|
2007-04-18 |
2011-09-13 |
Parker-Hannifin Corporation |
Fuel injector nozzles, with labyrinth grooves, for gas turbine engines
|
FR2915989B1
(en)
*
|
2007-05-10 |
2011-05-20 |
Saint Gobain Emballage |
LOW NOX MIXED INJECTOR
|
TWI482662B
(en)
*
|
2007-08-30 |
2015-05-01 |
Optomec Inc |
Mechanically integrated and closely coupled print head and mist source
|
DE102008013540A1
(en)
*
|
2008-03-11 |
2009-09-24 |
Microjet Gmbh |
Device for generating and spraying an aerosol
|
US7992390B2
(en)
*
|
2008-09-23 |
2011-08-09 |
Pratt & Whitney Canada Corp. |
External rigid fuel manifold
|
US8141363B2
(en)
*
|
2009-10-08 |
2012-03-27 |
General Electric Company |
Apparatus and method for cooling nozzles
|
US20110100015A1
(en)
*
|
2009-11-05 |
2011-05-05 |
General Electric Company |
Gas turbine system to inhibit coke formation and methods of use
|
WO2012090071A2
(en)
|
2010-12-30 |
2012-07-05 |
Royce Power Engineering Plc |
Method and apparatus for isolating inactive fluid passages
|
JP5618337B2
(en)
*
|
2012-02-28 |
2014-11-05 |
三菱日立パワーシステムズ株式会社 |
Gas turbine combustor
|
US10619855B2
(en)
*
|
2012-09-06 |
2020-04-14 |
United Technologies Corporation |
Fuel delivery system with a cavity coupled fuel injector
|
CN103486592B
(en)
*
|
2013-10-23 |
2016-08-31 |
中国船舶重工集团公司第七�三研究所 |
Gas-liquid double fuel integrated spray nozzle
|
CN103759260B
(en)
*
|
2014-01-07 |
2015-11-25 |
孙升科 |
A kind of atomizing lance
|
US10132240B2
(en)
|
2014-08-14 |
2018-11-20 |
Siemens Aktiengesellschaft |
Multi-functional fuel nozzle with a dual-orifice atomizer
|
EP3180568B1
(en)
|
2014-08-14 |
2019-04-10 |
Siemens Aktiengesellschaft |
Multi-functional fuel nozzle with a heat shield
|
US9958152B2
(en)
|
2014-08-14 |
2018-05-01 |
Siemens Aktiengesellschaft |
Multi-functional fuel nozzle with an atomizer array
|
US10443855B2
(en)
*
|
2014-10-23 |
2019-10-15 |
Siemens Aktiengesellschaft |
Flexible fuel combustion system for turbine engines
|
US10994473B2
(en)
|
2015-02-10 |
2021-05-04 |
Optomec, Inc. |
Fabrication of three dimensional structures by in-flight curing of aerosols
|
EP3073097B1
(en)
*
|
2015-03-27 |
2019-06-12 |
Ansaldo Energia Switzerland AG |
Integrated dual fuel delivery system
|
TWI767087B
(en)
|
2017-11-13 |
2022-06-11 |
美商阿普托麥克股份有限公司 |
Methods for controlling the flow of an aerosol in a print head of an aerosol jet printing system, and apparatuses for depositing an aerosol
|
US11754287B2
(en)
|
2020-09-11 |
2023-09-12 |
Raytheon Technologies Corporation |
Fuel injector assembly for a turbine engine
|
US11421883B2
(en)
|
2020-09-11 |
2022-08-23 |
Raytheon Technologies Corporation |
Fuel injector assembly with a helical swirler passage for a turbine engine
|
US11649964B2
(en)
|
2020-12-01 |
2023-05-16 |
Raytheon Technologies Corporation |
Fuel injector assembly for a turbine engine
|
TW202247905A
(en)
|
2021-04-29 |
2022-12-16 |
美商阿普托麥克股份有限公司 |
High reliability sheathed transport path for aerosol jet devices
|
US11808455B2
(en)
|
2021-11-24 |
2023-11-07 |
Rtx Corporation |
Gas turbine engine combustor with integral fuel conduit(s)
|
US11846249B1
(en)
|
2022-09-02 |
2023-12-19 |
Rtx Corporation |
Gas turbine engine with integral bypass duct
|
US12116934B2
(en)
|
2023-02-10 |
2024-10-15 |
Rtx Corporation |
Turbine engine fuel injector with oxygen circuit
|