IT951457B - Dispositivo di controllo di turbine a gas - Google Patents

Dispositivo di controllo di turbine a gas

Info

Publication number
IT951457B
IT951457B IT2319672A IT2319672A IT951457B IT 951457 B IT951457 B IT 951457B IT 2319672 A IT2319672 A IT 2319672A IT 2319672 A IT2319672 A IT 2319672A IT 951457 B IT951457 B IT 951457B
Authority
IT
Italy
Prior art keywords
control device
gas turbine
turbine control
gas
turbine
Prior art date
Application number
IT2319672A
Other languages
English (en)
Original Assignee
United Aircraft Canada
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 United Aircraft Canada filed Critical United Aircraft Canada
Application granted granted Critical
Publication of IT951457B publication Critical patent/IT951457B/it

Links

Classifications

    • 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
    • F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/26—Controlling the air flow

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Combustion Of Fluid Fuel (AREA)
IT2319672A 1971-04-15 1972-04-15 Dispositivo di controllo di turbine a gas IT951457B (it)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB953071A GB1385903A (en) 1971-04-15 1971-04-15 Continuous combustion device

Publications (1)

Publication Number Publication Date
IT951457B true IT951457B (it) 1973-06-30

Family

ID=9873786

Family Applications (1)

Application Number Title Priority Date Filing Date
IT2319672A IT951457B (it) 1971-04-15 1972-04-15 Dispositivo di controllo di turbine a gas

Country Status (4)

Country Link
CA (1) CA961279A (it)
DE (1) DE2218123A1 (it)
GB (1) GB1385903A (it)
IT (1) IT951457B (it)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4296599A (en) * 1979-03-30 1981-10-27 General Electric Company Turbine cooling air modulation apparatus
US4459803A (en) * 1982-02-19 1984-07-17 The United States Of America As Represented By The Secretary Of The Air Force Variable inlet vane assembly for a gas turbine combustion
WO2011018853A1 (ja) * 2009-08-13 2011-02-17 三菱重工業株式会社 燃焼器
DE102019213936A1 (de) * 2019-09-12 2021-03-18 Rolls-Royce Deutschland Ltd & Co Kg Brennkammerbaugruppe mit drehbarem Verstellelement an einer äußeren Brennkammerwandung für die Beeinflussung einer Mischluftströmung
CN115585479B (zh) * 2022-11-14 2024-11-05 哈尔滨广瀚动力技术发展有限公司 一种燃气轮机扩压装置

Also Published As

Publication number Publication date
DE2218123A1 (de) 1972-11-02
GB1385903A (en) 1975-03-05
CA961279A (en) 1975-01-21

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