FR1006682A - Procédés de surcharge pour les turbo-réacteurs à deux flux - Google Patents

Procédés de surcharge pour les turbo-réacteurs à deux flux

Info

Publication number
FR1006682A
FR1006682A FR1006682DA FR1006682A FR 1006682 A FR1006682 A FR 1006682A FR 1006682D A FR1006682D A FR 1006682DA FR 1006682 A FR1006682 A FR 1006682A
Authority
FR
France
Prior art keywords
reactors
overload
processes
stream turbo
turbo
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
Other languages
English (en)
Inventor
Rene Anxionnaz
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.)
Rateau SA
Original Assignee
Rateau SA
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 Rateau SA filed Critical Rateau SA
Application granted granted Critical
Publication of FR1006682A publication Critical patent/FR1006682A/fr
Expired legal-status Critical Current

Links

Classifications

    • 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
    • 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
    • F02C3/305Increasing the power, speed, torque or efficiency of a gas turbine or the thrust of a turbojet engine by injecting or adding water, steam or other fluids
    • 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
    • F02C6/00Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas- turbine plants for special use
    • F02C6/003Gas-turbine plants with heaters between turbine stages
FR1006682D 1948-02-10 1948-02-10 Procédés de surcharge pour les turbo-réacteurs à deux flux Expired FR1006682A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1006682T 1948-02-10

Publications (1)

Publication Number Publication Date
FR1006682A true FR1006682A (fr) 1952-04-25

Family

ID=9565986

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1006682D Expired FR1006682A (fr) 1948-02-10 1948-02-10 Procédés de surcharge pour les turbo-réacteurs à deux flux

Country Status (1)

Country Link
FR (1) FR1006682A (fr)

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE963203C (de) * 1952-05-06 1957-05-02 Alfred Buechi Propellerturbinentriebwerk
DE1043722B (de) * 1954-01-16 1958-11-13 Oskar August Schaetzle Dipl In Dreiwellenstrahltriebwerk mit biegungssteifen UEbertragungsgliedern
DE1131467B (de) * 1959-04-30 1962-06-14 Daimler Benz Ag Verbundtriebwerk zum Antrieb von Flugzeugen
DE1151985B (de) * 1959-11-18 1963-07-25 Otto Lutz Dr Ing Gasturbinen-Triebwerksanlage mit einer Nutzleistungsturbine, mit der Moeglichkeit kurzzeitiger Leistungssteigerung
EP0620362A1 (fr) * 1993-04-08 1994-10-19 ABB Management AG Turbine à gaz
EP0887539A3 (fr) * 1997-06-26 2000-02-23 Asea Brown Boveri AG Turboréacteur
FR2923263A1 (fr) * 2007-11-07 2009-05-08 Turbomeca Sa Turbomoteur comportant des moyens pour chauffer l'air entrant dans la turbine libre
US20140250904A1 (en) * 2013-03-05 2014-09-11 Rolls-Royce Canada, Ltd. Capacity control of turbine by the use of a reheat combustor in multi shaft engine
CN111197534A (zh) * 2020-03-10 2020-05-26 田国庆 一种混合动力航空发动机
RU198144U1 (ru) * 2019-06-03 2020-06-19 Вадим Александрович Иванов Двухконтурный турбопрямоточный реактивный двигатель
US20220243667A1 (en) * 2021-02-01 2022-08-04 General Electric Company Aircraft propulsion system with inter-turbine burner

Cited By (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE963203C (de) * 1952-05-06 1957-05-02 Alfred Buechi Propellerturbinentriebwerk
DE1043722B (de) * 1954-01-16 1958-11-13 Oskar August Schaetzle Dipl In Dreiwellenstrahltriebwerk mit biegungssteifen UEbertragungsgliedern
DE1131467B (de) * 1959-04-30 1962-06-14 Daimler Benz Ag Verbundtriebwerk zum Antrieb von Flugzeugen
DE1151985B (de) * 1959-11-18 1963-07-25 Otto Lutz Dr Ing Gasturbinen-Triebwerksanlage mit einer Nutzleistungsturbine, mit der Moeglichkeit kurzzeitiger Leistungssteigerung
EP0620362A1 (fr) * 1993-04-08 1994-10-19 ABB Management AG Turbine à gaz
CH687269A5 (de) * 1993-04-08 1996-10-31 Abb Management Ag Gasturbogruppe.
EP0887539A3 (fr) * 1997-06-26 2000-02-23 Asea Brown Boveri AG Turboréacteur
EP2058488A1 (fr) * 2007-11-07 2009-05-13 Turbomeca Turbomoteur comportant des moyens pour chauffer l'air entrant dans la turbine libre
FR2923263A1 (fr) * 2007-11-07 2009-05-08 Turbomeca Sa Turbomoteur comportant des moyens pour chauffer l'air entrant dans la turbine libre
US20140250904A1 (en) * 2013-03-05 2014-09-11 Rolls-Royce Canada, Ltd. Capacity control of turbine by the use of a reheat combustor in multi shaft engine
CN105121811A (zh) * 2013-03-05 2015-12-02 工业涡轮(英国)有限公司 多轴发动机中通过使用再热燃烧器的涡轮容量控制
CN105121811B (zh) * 2013-03-05 2018-03-13 工业涡轮(英国)有限公司 燃气涡轮发动机和控制其核心参数的方法
US10036317B2 (en) * 2013-03-05 2018-07-31 Industrial Turbine Company (Uk) Limited Capacity control of turbine by the use of a reheat combustor in multi shaft engine
RU198144U1 (ru) * 2019-06-03 2020-06-19 Вадим Александрович Иванов Двухконтурный турбопрямоточный реактивный двигатель
CN111197534A (zh) * 2020-03-10 2020-05-26 田国庆 一种混合动力航空发动机
CN111197534B (zh) * 2020-03-10 2021-01-29 田国庆 一种混合动力航空发动机
US20220243667A1 (en) * 2021-02-01 2022-08-04 General Electric Company Aircraft propulsion system with inter-turbine burner
US11859539B2 (en) * 2021-02-01 2024-01-02 General Electric Company Aircraft propulsion system with inter-turbine burner

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