HK1121217A1 - Rotary injector - Google Patents

Rotary injector

Info

Publication number
HK1121217A1
HK1121217A1 HK08112690.0A HK08112690A HK1121217A1 HK 1121217 A1 HK1121217 A1 HK 1121217A1 HK 08112690 A HK08112690 A HK 08112690A HK 1121217 A1 HK1121217 A1 HK 1121217A1
Authority
HK
Hong Kong
Prior art keywords
rotary injector
injector
rotary
Prior art date
Application number
HK08112690.0A
Other languages
English (en)
Inventor
Jamey J Condeveaux
Guido J Defever
Original Assignee
Williams Internat Co
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Williams Internat Co filed Critical Williams Internat Co
Publication of HK1121217A1 publication Critical patent/HK1121217A1/xx

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/22—Fuel supply systems
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
    • F02K3/08—Plants including a gas turbine driving a compressor or a ducted fan with supplementary heating of the working fluid; Control thereof
    • F02K3/10—Plants including a gas turbine driving a compressor or a ducted fan with supplementary heating of the working fluid; Control thereof by after-burners
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • F23R3/38—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply comprising rotary fuel injection means
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2240/00—Components
    • F05D2240/35—Combustors or associated equipment
    • F05D2240/36—Fuel vaporizer

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Fuel-Injection Apparatus (AREA)
  • Nozzles (AREA)
  • Electrostatic Spraying Apparatus (AREA)
HK08112690.0A 2003-05-22 2008-11-20 Rotary injector HK1121217A1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US10/249,967 US6925812B2 (en) 2003-05-22 2003-05-22 Rotary injector

Publications (1)

Publication Number Publication Date
HK1121217A1 true HK1121217A1 (en) 2009-04-17

Family

ID=34192848

Family Applications (1)

Application Number Title Priority Date Filing Date
HK08112690.0A HK1121217A1 (en) 2003-05-22 2008-11-20 Rotary injector

Country Status (9)

Country Link
US (1) US6925812B2 (ja)
EP (1) EP1627139A2 (ja)
JP (1) JP4484874B2 (ja)
CN (2) CN100552200C (ja)
CA (1) CA2526029A1 (ja)
HK (1) HK1121217A1 (ja)
IL (1) IL171935A (ja)
RU (1) RU2333424C2 (ja)
WO (1) WO2005028843A2 (ja)

Families Citing this family (25)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6988367B2 (en) * 2004-04-20 2006-01-24 Williams International Co. L.L.C. Gas turbine engine cooling system and method
EP1875058A4 (en) * 2005-04-25 2011-03-30 Williams Int Co Llc SYSTEM AND METHOD FOR COOLING A GAS TURBINE ENGINE
US7685824B2 (en) * 2005-09-09 2010-03-30 The Regents Of The University Of Michigan Rotary ramjet turbo-generator
US7568343B2 (en) * 2005-09-12 2009-08-04 Florida Turbine Technologies, Inc. Small gas turbine engine with multiple burn zones
US7685822B1 (en) 2005-11-09 2010-03-30 Florida Turbine Technologies, Inc. Rotary cup fuel injector
US7937946B1 (en) 2005-12-21 2011-05-10 Florida Turbine Technologies, Inc. Small gas turbine engine with lubricated bearings
US20070144180A1 (en) * 2005-12-22 2007-06-28 Honeywell International, Inc. Dual bayonet engagement and method of assembling a combustor liner in a gas turbine engine
US20080264035A1 (en) * 2007-04-25 2008-10-30 Ricciardo Mark J Coolant flow swirler for a rocket engine
US20090236442A1 (en) * 2007-12-10 2009-09-24 Tdc Products B.V. Injection device for an internal combustion engine
NL2001069C2 (nl) * 2007-12-10 2009-06-11 Tdc Products B V Inspuitinrichting voor verbrandingsmotor.
EP2232138A2 (en) * 2007-12-10 2010-09-29 TDC Products B.V. Injection device for an internal combustion engine
GB0724633D0 (en) * 2007-12-18 2008-01-30 Limpsfield Engineering Ltd Rotating gas distribution design
US8006500B1 (en) * 2008-01-29 2011-08-30 Florida Turbine Technologies, Inc. Swirl combustor with counter swirl fuel slinger
US8763405B2 (en) * 2008-04-09 2014-07-01 Williams International Co., L.L.C. Gas turbine engine rotary injection system and method
WO2009126847A1 (en) * 2008-04-09 2009-10-15 Williams International Co., L.L.C. Gas turbine engine cooling system and method
US9464527B2 (en) 2008-04-09 2016-10-11 Williams International Co., Llc Fuel-cooled bladed rotor of a gas turbine engine
WO2010096817A2 (en) 2009-02-23 2010-08-26 Williams International Co., L.L.C. Combustion system
KR101122062B1 (ko) * 2010-05-04 2012-03-14 국방과학연구소 가스터빈용 회전연료노즐
KR101204891B1 (ko) 2010-07-30 2012-11-26 삼성테크윈 주식회사 터보제트 엔진 및 터보팬 엔진
WO2015095763A1 (en) 2013-12-19 2015-06-25 United Technologies Corporation Self-pumping fuel injector for a gas turbine engine and method of operation
FR3037384B1 (fr) * 2015-06-11 2017-06-23 Turbomeca Module de chambre de combustion cvc de turbomachine comportant une prechambre de combustion
FR3050255B1 (fr) * 2016-04-13 2019-10-25 Safran Helicopter Engines Injecteurs ameliores pour chambre de combustion de turbine a gaz
RU174790U1 (ru) * 2017-03-06 2017-11-02 Публичное акционерное общество "Научно-производственное объединение "Сатурн" Устройство для распыливания топлива в камере сгорания газотурбинного двигателя
US20200041130A1 (en) * 2018-07-31 2020-02-06 Hotstart, Inc. Combustor Systems
USD910717S1 (en) 2018-07-31 2021-02-16 Hotstart, Inc. Rotary atomizer

Family Cites Families (24)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US903657A (en) * 1905-12-19 1908-11-10 Carl Beckmann Explosion-turbine.
US1736799A (en) * 1927-12-05 1929-11-26 Emil J P Planert Humidifier
US1940758A (en) * 1929-11-29 1933-12-26 Metallgesellschaft Ag Process for burning phosphorus
US2177245A (en) * 1936-06-29 1939-10-24 Edwin L Dennis Rotary gas burner
US2479777A (en) * 1943-05-22 1949-08-23 Lockheed Aircraft Corp Fuel injection means for gas turbine power plants for aircraft
US2518881A (en) * 1947-06-25 1950-08-15 Daniel And Florence Guggenheim Fuel feeding and cooling construction for rotating combustion chambers
US2720750A (en) * 1947-11-04 1955-10-18 Helmut R Schelp Revolving fuel injection system for jet engines and gas turbines
US2508420A (en) * 1948-09-21 1950-05-23 Westinghouse Electric Corp Combustion apparatus
US2866313A (en) * 1950-04-14 1958-12-30 Power Jets Res & Dev Ltd Means for cooling turbine-blades by liquid jets
BE507258A (ja) * 1950-12-02
US2775864A (en) * 1951-04-10 1957-01-01 Gen Motors Corp Jet propulsion engine with afterburner
US2766071A (en) * 1954-03-11 1956-10-09 Defensor A G Apparatus for atomizing liquids
US2914912A (en) * 1955-10-24 1959-12-01 Gen Electric Combustion system for thermal powerplant
US2981066A (en) * 1956-04-12 1961-04-25 Elmer G Johnson Turbo machine
CH398182A (de) * 1962-11-14 1965-08-31 Saurer Ag Adolph Gasturbinenanlage
US3286473A (en) * 1963-06-26 1966-11-22 North American Aviation Inc Fixed injector and turbopump assembly
US3307359A (en) * 1963-06-26 1967-03-07 North American Aviation Inc Turbopump assembly
FR2155925B1 (ja) * 1971-10-15 1974-05-31 Bertin & Cie
US4769996A (en) * 1987-01-27 1988-09-13 Teledyne Industries, Inc. Fuel transfer system for multiple concentric shaft gas turbine engines
US4870825A (en) * 1988-06-09 1989-10-03 Williams International Corporation Rotary fuel injection system
US5224713A (en) * 1991-08-28 1993-07-06 General Electric Company Labyrinth seal with recirculating means for reducing or eliminating parasitic leakage through the seal
US5323602A (en) * 1993-05-06 1994-06-28 Williams International Corporation Fuel/air distribution and effusion cooling system for a turbine engine combustor burner
US5713327A (en) * 1997-01-03 1998-02-03 Tilton; Charles L. Liquid fuel injection device with pressure-swirl atomizers
IL164183A0 (en) * 1999-03-10 2005-12-18 Williams Int Co Llc A rotor system for a rocket engine

Also Published As

Publication number Publication date
WO2005028843A3 (en) 2005-05-12
JP2006526133A (ja) 2006-11-16
WO2005028843A2 (en) 2005-03-31
CN101201015A (zh) 2008-06-18
CA2526029A1 (en) 2005-03-31
US20050039463A1 (en) 2005-02-24
EP1627139A2 (en) 2006-02-22
IL171935A (en) 2009-09-22
IL171935A0 (en) 2006-04-10
RU2333424C2 (ru) 2008-09-10
US6925812B2 (en) 2005-08-09
CN1795323A (zh) 2006-06-28
CN100552200C (zh) 2009-10-21
JP4484874B2 (ja) 2010-06-16
RU2005140159A (ru) 2006-05-27

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Legal Events

Date Code Title Description
PC Patent ceased (i.e. patent has lapsed due to the failure to pay the renewal fee)

Effective date: 20130521