GB1301615A - - Google Patents

Info

Publication number
GB1301615A
GB1301615A GB1015371A GB1015371A GB1301615A GB 1301615 A GB1301615 A GB 1301615A GB 1015371 A GB1015371 A GB 1015371A GB 1015371 A GB1015371 A GB 1015371A GB 1301615 A GB1301615 A GB 1301615A
Authority
GB
United Kingdom
Prior art keywords
blades
fan
ring
engine
rotated
Prior art date
Legal status (The legal status 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 status listed.)
Expired
Application number
GB1015371A
Other languages
English (en)
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 filed Critical
Publication of GB1301615A publication Critical patent/GB1301615A/en
Expired legal-status Critical Current

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
    • F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
    • F02C9/16—Control of working fluid flow
    • 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
    • F02C7/26—Starting; Ignition
    • F02C7/268—Starting drives for the rotor, acting directly on the rotor of the gas turbine to be started
    • F02C7/27—Fluid drives

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
GB1015371A 1970-04-23 1971-04-20 Expired GB1301615A (enrdf_load_stackoverflow)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR7014874A FR2085470B1 (enrdf_load_stackoverflow) 1970-04-23 1970-04-23

Publications (1)

Publication Number Publication Date
GB1301615A true GB1301615A (enrdf_load_stackoverflow) 1973-01-04

Family

ID=9054487

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1015371A Expired GB1301615A (enrdf_load_stackoverflow) 1970-04-23 1971-04-20

Country Status (3)

Country Link
DE (1) DE2119626A1 (enrdf_load_stackoverflow)
FR (1) FR2085470B1 (enrdf_load_stackoverflow)
GB (1) GB1301615A (enrdf_load_stackoverflow)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2455179A1 (fr) * 1979-04-23 1980-11-21 Gen Electric Systeme de manoeuvre d'un element monte a l'interieur d'un carter
US5224337A (en) * 1991-05-22 1993-07-06 Mitsubishi Jukogyo Kabushiki Kaisha Operating method for gas turbine with variable inlet vanes
RU2221157C1 (ru) * 2003-01-31 2004-01-10 Федеральное государственное унитарное предприятие "Центральный институт авиационного моторостроения им. П.И.Баранова" Способ запуска авиационного двухконтурного турбореактивного двигателя (трдд) с большой степенью двухконтурности и устройство для его осуществления
WO2006006953A3 (en) * 2003-12-30 2006-04-06 Honeywell Int Inc Gas turbine engine electromechanical variable inlet guide vane actuation system
CN115234378A (zh) * 2022-06-27 2022-10-25 中国航发哈尔滨东安发动机有限公司 一种燃气涡轮发动机起动器

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2834822C2 (de) * 1978-08-09 1981-09-17 MTU Motoren- und Turbinen-Union München GmbH, 8000 München Einrichtung zur Verdichterluftentnahme bei Gasturbinentriebwerken
FR2526491A1 (fr) * 1982-05-04 1983-11-10 Snecma Dispositif de reglage de la perte de charge d'au moins un des flux dans un turboreacteur multiflux
RU2312239C1 (ru) * 2006-02-20 2007-12-10 Николай Борисович Болотин Силовая установка газотурбовоза

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2989848A (en) * 1959-11-25 1961-06-27 Philip R Paiement Apparatus for air impingement starting of a turbojet engine
FR1377306A (fr) * 1963-05-31 1964-11-06 Rolls Royce Compresseur ou ventilateur à courants axiaux et moteur à turbine à gaz équipé de cet appareil
FR1376192A (fr) * 1963-12-03 1964-10-23 Gen Electric Dispositif d'antigivrage avec un système de valve de réglage de l'écoulement d'un fluide à haute température dans une turbine à gaz
FR1377199A (fr) * 1963-12-17 1964-10-31 Rolls Royce Moteur à turbine à gaz
FR86421E (fr) * 1964-09-15 1966-02-04 Rolls Royce Compresseur ou ventilateur à courants axiaux et moteur à turbine à gaz équipé de cet appareil

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2455179A1 (fr) * 1979-04-23 1980-11-21 Gen Electric Systeme de manoeuvre d'un element monte a l'interieur d'un carter
US5224337A (en) * 1991-05-22 1993-07-06 Mitsubishi Jukogyo Kabushiki Kaisha Operating method for gas turbine with variable inlet vanes
RU2221157C1 (ru) * 2003-01-31 2004-01-10 Федеральное государственное унитарное предприятие "Центральный институт авиационного моторостроения им. П.И.Баранова" Способ запуска авиационного двухконтурного турбореактивного двигателя (трдд) с большой степенью двухконтурности и устройство для его осуществления
WO2006006953A3 (en) * 2003-12-30 2006-04-06 Honeywell Int Inc Gas turbine engine electromechanical variable inlet guide vane actuation system
US7096657B2 (en) 2003-12-30 2006-08-29 Honeywell International, Inc. Gas turbine engine electromechanical variable inlet guide vane actuation system
CN115234378A (zh) * 2022-06-27 2022-10-25 中国航发哈尔滨东安发动机有限公司 一种燃气涡轮发动机起动器

Also Published As

Publication number Publication date
FR2085470B1 (enrdf_load_stackoverflow) 1974-05-03
FR2085470A1 (enrdf_load_stackoverflow) 1971-12-24
DE2119626A1 (de) 1971-11-11

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Legal Events

Date Code Title Description
PS Patent sealed
PCNP Patent ceased through non-payment of renewal fee