IT1225431B - Complesso ad ugello per combustibile per turbomotori a gas. - Google Patents

Complesso ad ugello per combustibile per turbomotori a gas.

Info

Publication number
IT1225431B
IT1225431B IT8841696A IT4169688A IT1225431B IT 1225431 B IT1225431 B IT 1225431B IT 8841696 A IT8841696 A IT 8841696A IT 4169688 A IT4169688 A IT 4169688A IT 1225431 B IT1225431 B IT 1225431B
Authority
IT
Italy
Prior art keywords
fuel
gas turbo
turbo engines
nozzle complex
nozzle
Prior art date
Application number
IT8841696A
Other languages
English (en)
Italian (it)
Other versions
IT8841696A0 (it
Inventor
Leroy Dixon Mclaurin
David You Koon Toy
Original Assignee
Westinghouse Electric Corp
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 Westinghouse Electric Corp filed Critical Westinghouse Electric Corp
Publication of IT8841696A0 publication Critical patent/IT8841696A0/it
Application granted granted Critical
Publication of IT1225431B publication Critical patent/IT1225431B/it

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23D—BURNERS
    • F23D11/00—Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space
    • F23D11/005—Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space with combinations of different spraying or vaporising means
    • F23D11/007—Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space with combinations of different spraying or vaporising means combination of means covered by sub-groups F23D11/10 and F23D11/24
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23D—BURNERS
    • F23D11/00—Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space
    • F23D11/24—Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space by pressurisation of the fuel before a nozzle through which it is sprayed by a substantial pressure reduction into a space
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23D—BURNERS
    • F23D2211/00—Thermal dilatation prevention or compensation

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Nozzles For Spraying Of Liquid Fuel (AREA)
  • Fuel-Injection Apparatus (AREA)
IT8841696A 1987-10-23 1988-10-21 Complesso ad ugello per combustibile per turbomotori a gas. IT1225431B (it)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US11189087A 1987-10-23 1987-10-23

Publications (2)

Publication Number Publication Date
IT8841696A0 IT8841696A0 (it) 1988-10-21
IT1225431B true IT1225431B (it) 1990-11-13

Family

ID=22340987

Family Applications (1)

Application Number Title Priority Date Filing Date
IT8841696A IT1225431B (it) 1987-10-23 1988-10-21 Complesso ad ugello per combustibile per turbomotori a gas.

Country Status (6)

Country Link
JP (1) JPH01134028A (enrdf_load_html_response)
CA (1) CA1283551C (enrdf_load_html_response)
DE (1) DE3833279A1 (enrdf_load_html_response)
FR (1) FR2622252B1 (enrdf_load_html_response)
GB (1) GB2211594B (enrdf_load_html_response)
IT (1) IT1225431B (enrdf_load_html_response)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE19539246A1 (de) * 1995-10-21 1997-04-24 Asea Brown Boveri Airblast-Zerstäuberdüse
RU2396487C1 (ru) * 2009-04-02 2010-08-10 Государственное образовательное учреждение высшего профессионального образования "Казанский государственный энергетический университет" (КГЭУ) Форсунка
US8561553B2 (en) * 2009-12-17 2013-10-22 Babcock Power Services, Inc. Solid fuel nozzle tip assembly
US9404655B2 (en) * 2012-01-20 2016-08-02 General Electric Company Process of fabricating a fuel nozzle assembly
US10060628B2 (en) * 2015-03-26 2018-08-28 General Electric Company Systems and methods for creating a seal about a liquid fuel injector in a gas turbine engine
CN115751380B (zh) * 2022-11-24 2025-01-28 保定市玄云涡喷动力设备研发有限公司 一种微型雾化喷头

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2973150A (en) * 1958-05-12 1961-02-28 Chrysler Corp Fuel nozzle for gas turbine engine
US2968925A (en) * 1959-11-25 1961-01-24 William E Blevans Fuel nozzle head for anti-coking
US4154056A (en) * 1977-09-06 1979-05-15 Westinghouse Electric Corp. Fuel nozzle assembly for a gas turbine engine
CA1259197A (en) * 1985-02-13 1989-09-12 Alan D. Bennett High reliability fuel oil nozzle for a gas turbine

Also Published As

Publication number Publication date
IT8841696A0 (it) 1988-10-21
JPH05539B2 (enrdf_load_html_response) 1993-01-06
FR2622252B1 (fr) 1993-04-23
DE3833279A1 (de) 1989-05-03
GB8824501D0 (en) 1988-11-23
JPH01134028A (ja) 1989-05-26
CA1283551C (en) 1991-04-30
GB2211594A (en) 1989-07-05
FR2622252A1 (fr) 1989-04-28
GB2211594B (en) 1991-05-29

Similar Documents

Publication Publication Date Title
GB2206159B (en) A gas turbine engine having a dual manifold fuel system.
GB2199375B (en) A turbofan gas turbine engine.
DE3866856D1 (de) Brennkammer fuer eine gasturbine.
IT8423443A0 (it) Complesso di combustione per motore a turbina a gas.
IT1225427B (it) Complesso a ugello distributore di combustibile per un turbomotore a gas.
IT1216546B (it) Complesso di telaio di turbomotore a gas.
IT8422791A0 (it) Combustore schermato specialmente per turbomotori a gas.
IT1227060B (it) Iniettore vorticizzatore bimodale per combustore di turbina a gas.
IT8321934A0 (it) Carburatore per turbomotore a gas.
DE3265642D1 (en) Fuel nozzle assembly for a gas turbine engine
IT8523205A0 (it) Potenziatore per turbomotore a gas.
GB2199900B (en) A turbopropeller or turbofan gas turbine engine
DE3472829D1 (en) Fuel nozzle for gas turbine engine
IL65659A (en) Exhaust nozzle for gas turbine engine
GB2196390B (en) Intake for turbopropeller gas turbine engine.
IT1240296B (it) Assieme rotorico per turbomotore a gas
GB2102936B (en) Fuel injector for gas turbine engines
DE3566013D1 (en) Two dimensional gas turbine engine exhaust nozzle
IL65660A (en) Exhaust nozzle for gas turbine engine
IT8119348A0 (it) Complesso di aspirazione per turbomotori a gas.
DE68909572D1 (de) Integrierter brennstoffduesendeckel fuer eine gasturbinenbrennkammer.
IT8521926A0 (it) Ugello di scarico orientabile per un motore a turbina a gas.
DE3680351D1 (de) Brennoelduese fuer eine gasturbine.
IT1213558B (it) Valvola dosatrice del combustibile per motori a turbina a gas.
GB2164613B (en) Vectorable exhaust nozzle for gas turbine engines

Legal Events

Date Code Title Description
TA Fee payment date (situation as of event date), data collected since 19931001

Effective date: 19971028