FR2094662A5 - - Google Patents

Info

Publication number
FR2094662A5
FR2094662A5 FR7023976A FR7023976A FR2094662A5 FR 2094662 A5 FR2094662 A5 FR 2094662A5 FR 7023976 A FR7023976 A FR 7023976A FR 7023976 A FR7023976 A FR 7023976A FR 2094662 A5 FR2094662 A5 FR 2094662A5
Authority
FR
France
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
FR7023976A
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to FR7023976A priority Critical patent/FR2094662A5/fr
Priority to DE19702051657 priority patent/DE2051657A1/de
Priority to US137819A priority patent/US3908362A/en
Priority to GB02188/71A priority patent/GB1299692A/en
Application granted granted Critical
Publication of FR2094662A5 publication Critical patent/FR2094662A5/fr
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D27/00Control, e.g. regulation, of pumps, pumping installations or pumping systems specially adapted for elastic fluids
    • F04D27/02Surge control
    • F04D27/0246Surge control by varying geometry within the pumps, e.g. by adjusting vanes
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C3/00Gas-turbine plants characterised by the use of combustion products as the working fluid
    • F02C3/20Gas-turbine plants characterised by the use of combustion products as the working fluid using a special fuel, oxidant, or dilution fluid to generate the combustion products
    • F02C3/30Adding water, steam or other fluids for influencing combustion, e.g. to obtain cleaner exhaust gases
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00Features, 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
    • F02C7/12Cooling of plants
    • F02C7/14Cooling of plants of fluids in the plant, e.g. lubricant or fuel
    • F02C7/141Cooling of plants of fluids in the plant, e.g. lubricant or fuel of working fluid
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C9/00Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
    • F02C9/48Control of fuel supply conjointly with another control of the plant
    • F02C9/56Control of fuel supply conjointly with another control of the plant with power transmission control
    • F02C9/58Control of fuel supply conjointly with another control of the plant with power transmission control with control of a variable-pitch propeller
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K3/00Plants including a gas turbine driving a compressor or a ducted fan
    • F02K3/02Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber
    • F02K3/04Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type
    • F02K3/06Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type with front fan
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/60Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Geometry (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Control Of Turbines (AREA)
FR7023976A 1970-06-29 1970-06-29 Expired FR2094662A5 (fr)

Priority Applications (4)

Application Number Priority Date Filing Date Title
FR7023976A FR2094662A5 (fr) 1970-06-29 1970-06-29
DE19702051657 DE2051657A1 (de) 1970-06-29 1970-10-21 Verbesserungen an Zweistrom Turbinen Strahltriebwerken
US137819A US3908362A (en) 1970-06-29 1971-04-27 Bypass turbojet with variable pitch low pressure compressor for thermal load control
GB02188/71A GB1299692A (en) 1970-06-29 1971-04-29 Improvements to bypass gas turbine engines

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR7023976A FR2094662A5 (fr) 1970-06-29 1970-06-29

Publications (1)

Publication Number Publication Date
FR2094662A5 true FR2094662A5 (fr) 1972-02-04

Family

ID=9057955

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7023976A Expired FR2094662A5 (fr) 1970-06-29 1970-06-29

Country Status (4)

Country Link
US (1) US3908362A (fr)
DE (1) DE2051657A1 (fr)
FR (1) FR2094662A5 (fr)
GB (1) GB1299692A (fr)

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4083181A (en) * 1976-06-14 1978-04-11 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Gas turbine engine with recirculating bleed
US4275560A (en) * 1978-12-27 1981-06-30 General Electric Company Blocker door actuation system
US4292802A (en) * 1978-12-27 1981-10-06 General Electric Company Method and apparatus for increasing compressor inlet pressure
US5174105A (en) * 1990-11-09 1992-12-29 General Electric Company Hot day m & i gas turbine engine and method of operation
US7550218B2 (en) * 2001-10-11 2009-06-23 Airbus Deutschland Gmbh Apparatus for producing water onboard of a craft driven by a power plant
CA2502951C (fr) * 2002-10-24 2013-05-21 Airbus Deutschland Gmbh Dispositif pour produire de l'eau a bord d'un avion
US7665959B2 (en) 2005-07-20 2010-02-23 United Technologies Corporation Rack and pinion variable vane synchronizing mechanism for inner diameter vane shroud
US7628579B2 (en) * 2005-07-20 2009-12-08 United Technologies Corporation Gear train variable vane synchronizing mechanism for inner diameter vane shroud
US7588415B2 (en) * 2005-07-20 2009-09-15 United Technologies Corporation Synch ring variable vane synchronizing mechanism for inner diameter vane shroud
US7753647B2 (en) * 2005-07-20 2010-07-13 United Technologies Corporation Lightweight cast inner diameter vane shroud for variable stator vanes
GB201907257D0 (en) * 2019-05-23 2019-07-10 Rolls Royce Plc Gas turbine engine

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2686631A (en) * 1948-05-08 1954-08-17 United Aircraft Corp Coolant injection system for gas turbines
US3097700A (en) * 1959-03-27 1963-07-16 Szydlowski Joseph Gas turbine control method and system
US3100964A (en) * 1959-11-25 1963-08-20 Gen Motors Corp Water injection system for a multistage compressor
FR1260184A (fr) * 1960-03-25 1961-05-05 Perfectionnements apportés aux procédés et dispositifs de commande et de régulation des turbomoteurs entraînant une hélice ou un rotor d'hélicoptère
US3476486A (en) * 1966-04-12 1969-11-04 Dowty Rotol Ltd Gas turbine engines

Also Published As

Publication number Publication date
GB1299692A (en) 1972-12-13
DE2051657A1 (de) 1972-03-23
US3908362A (en) 1975-09-30

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