FR1262452A - Grupe propulseur à turbine à gaz - Google Patents

Grupe propulseur à turbine à gaz

Info

Publication number
FR1262452A
FR1262452A FR833069A FR833069A FR1262452A FR 1262452 A FR1262452 A FR 1262452A FR 833069 A FR833069 A FR 833069A FR 833069 A FR833069 A FR 833069A FR 1262452 A FR1262452 A FR 1262452A
Authority
FR
France
Prior art keywords
gas turbine
thruster unit
turbine thruster
unit
gas
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
FR833069A
Other languages
English (en)
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.)
Pratt and Whitney Canada Corp
Original Assignee
Pratt and Whitney Aircraft of Canada Ltd
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 Pratt and Whitney Aircraft of Canada Ltd filed Critical Pratt and Whitney Aircraft of Canada Ltd
Application granted granted Critical
Publication of FR1262452A publication Critical patent/FR1262452A/fr
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
    • F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
    • F02C3/04—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor
    • F02C3/10—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor with another turbine driving an output shaft but not driving the compressor
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D35/00—Transmitting power from power plant to propellers or rotors; Arrangements of transmissions
    • 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
    • F02C6/00—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas- turbine plants for special use
    • F02C6/20—Adaptations of gas-turbine plants for driving vehicles
    • F02C6/206—Adaptations of gas-turbine plants for driving vehicles the vehicles being airscrew driven
    • 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
    • F02C7/20—Mounting or supporting of plant; Accommodating heat expansion or creep
    • 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
    • F02C7/32—Arrangement, mounting, or driving, of auxiliaries

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Supercharger (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
FR833069A 1959-07-17 1960-07-15 Grupe propulseur à turbine à gaz Expired FR1262452A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US827850A US3152443A (en) 1959-07-17 1959-07-17 Gas turbine powerplant

Publications (1)

Publication Number Publication Date
FR1262452A true FR1262452A (fr) 1961-05-26

Family

ID=25250325

Family Applications (1)

Application Number Title Priority Date Filing Date
FR833069A Expired FR1262452A (fr) 1959-07-17 1960-07-15 Grupe propulseur à turbine à gaz

Country Status (2)

Country Link
US (1) US3152443A (fr)
FR (1) FR1262452A (fr)

Cited By (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3173255A (en) * 1962-02-27 1965-03-16 Volvo Ab Gas turbine plant
FR2545538A1 (fr) * 1983-05-02 1984-11-09 Mtu Muenchen Gmbh Propulseur a turbines a gaz avec des dispositifs pour minimiser l'interstice des aubes
FR2556413A1 (fr) * 1983-12-09 1985-06-14 Teledyne Ind Systeme d'entrainement d'accessoires dans un moteur a turbine
EP0298014A1 (fr) * 1987-06-29 1989-01-04 United Technologies Corporation Modularité du moteur
WO2010086422A1 (fr) 2009-01-30 2010-08-05 Hispano Suiza Ensemble d'un agb et d'un reservoir d'huile
EP3321488A1 (fr) * 2016-11-15 2018-05-16 Pratt & Whitney Canada Corp. Arrangement d'accessoires de moteur à turbine à gaz
US10393027B2 (en) 2016-07-19 2019-08-27 Pratt & Whitney Canada Corp. Gas turbine engine shaft architecture and associated method of disassembly
US10465611B2 (en) 2016-09-15 2019-11-05 Pratt & Whitney Canada Corp. Reverse flow multi-spool gas turbine engine with aft-end accessory gearbox drivingly connected to both high pressure spool and low pressure spool
US10746188B2 (en) 2017-03-14 2020-08-18 Pratt & Whitney Canada Corp. Inter-shaft bearing connected to a compressor boost system
US10808624B2 (en) 2017-02-09 2020-10-20 Pratt & Whitney Canada Corp. Turbine rotor with low over-speed requirements
US11035293B2 (en) 2016-09-15 2021-06-15 Pratt & Whitney Canada Corp. Reverse flow gas turbine engine with offset RGB
US11408352B2 (en) 2016-09-15 2022-08-09 Pratt & Whitney Canada Corp. Reverse-flow gas turbine engine
US11536153B2 (en) 2018-08-08 2022-12-27 Pratt & Whitney Canada Corp. Turboshaft gas turbine engine

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3271949A (en) * 1963-04-26 1966-09-13 Williams Res Corp Gas turbine
US3520134A (en) * 1969-02-26 1970-07-14 United Aircraft Corp Sectional annular combustion chamber
US3516252A (en) * 1969-02-26 1970-06-23 United Aircraft Corp Fuel manifold system
US4074914A (en) * 1975-07-28 1978-02-21 United Technologies Corporation High pressure lightweight flanges
US9982676B2 (en) * 2014-11-18 2018-05-29 Rolls-Royce North American Technologies Inc. Split axial-centrifugal compressor
US10329943B2 (en) 2014-11-18 2019-06-25 Rolls-Royce North American Technologies Inc. Split axial-centrifugal compressor
US10533559B2 (en) 2016-12-20 2020-01-14 Pratt & Whitney Canada Corp. Reverse flow engine architecture
FR3061241B1 (fr) * 2016-12-23 2021-01-01 Safran Aircraft Engines Turbopropulseur a flux inverse
US11168828B2 (en) * 2017-05-02 2021-11-09 Pratt & Whitney Canada Corp. Gas turbine engine casing arrangement
US10836499B2 (en) 2017-08-22 2020-11-17 General Electric Company Turbine engine with single wall cantilevered architecture
CN114233412B (zh) * 2021-11-12 2023-10-20 中国航发南方工业有限公司 用于火焰筒内体与涡轮导向器组装的辅助安装装置及安装方法

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2687860A (en) * 1949-04-13 1954-08-31 Chrysler Corp Mounting
US2608057A (en) * 1949-12-24 1952-08-26 A V Roe Canada Ltd Gas turbine nozzle box
GB689353A (en) * 1950-03-09 1953-03-25 Lysholm Alf Improvements in centrifugal compressors
US2738647A (en) * 1951-07-03 1956-03-20 Boeing Co Gas turbine engine frame structure
US2672010A (en) * 1951-07-14 1954-03-16 United Aircraft Corp Pressurized lubrication system for gas turbines
US2895295A (en) * 1952-04-04 1959-07-21 Solar Aircraft Co Variable speed gas turbine
US2971334A (en) * 1955-01-04 1961-02-14 Solar Aircraft Co Gas turbine engine adaptable for multi-purpose use
US2969644A (en) * 1955-10-24 1961-01-31 Williams Res Corp Drive means for a regenerator in a reexpansion gas turbine engine
US2960306A (en) * 1956-01-16 1960-11-15 Gen Motors Corp Turbine
US2956404A (en) * 1956-10-02 1960-10-18 Avco Mfg Corp Fuel vaporizer
US2916874A (en) * 1957-01-31 1959-12-15 United Aircraft Corp Engine construction
FR1198540A (fr) * 1957-05-01 1959-12-08 Avco Mfg Corp Groupe moto-propulseur à turbine à gaz
US3088278A (en) * 1957-05-01 1963-05-07 Avco Mfg Corp Gas turbine engine

Cited By (26)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3173255A (en) * 1962-02-27 1965-03-16 Volvo Ab Gas turbine plant
FR2545538A1 (fr) * 1983-05-02 1984-11-09 Mtu Muenchen Gmbh Propulseur a turbines a gaz avec des dispositifs pour minimiser l'interstice des aubes
FR2556413A1 (fr) * 1983-12-09 1985-06-14 Teledyne Ind Systeme d'entrainement d'accessoires dans un moteur a turbine
EP0298014A1 (fr) * 1987-06-29 1989-01-04 United Technologies Corporation Modularité du moteur
WO2010086422A1 (fr) 2009-01-30 2010-08-05 Hispano Suiza Ensemble d'un agb et d'un reservoir d'huile
FR2941744A1 (fr) * 2009-01-30 2010-08-06 Hispano Suiza Sa Ensemble d'un boitier de relais d'accessoires et d'un reservoir d'huile
CN102301097A (zh) * 2009-01-30 2011-12-28 伊斯帕诺-絮扎公司 包括agb和储油器的组件
US8905191B2 (en) 2009-01-30 2014-12-09 Hispano Suiza Assembly including an AGB and an oil tank
CN102301097B (zh) * 2009-01-30 2015-07-01 伊斯帕诺-絮扎公司 包括附属装置齿轮箱和储油器的组件
US10883424B2 (en) 2016-07-19 2021-01-05 Pratt & Whitney Canada Corp. Multi-spool gas turbine engine architecture
US10458340B2 (en) 2016-07-19 2019-10-29 Pratt & Whitney Canada Corp. Turbine shaft power take-off
US10690061B2 (en) 2016-07-19 2020-06-23 Pratt & Whitney Canada Corp. Gear train architecture for a multi-spool gas turbine engine
US10767567B2 (en) 2016-07-19 2020-09-08 Pratt & Whitney Canada Corp. Multi-spool gas turbine engine architecture
US10393027B2 (en) 2016-07-19 2019-08-27 Pratt & Whitney Canada Corp. Gas turbine engine shaft architecture and associated method of disassembly
US11041443B2 (en) 2016-09-15 2021-06-22 Pratt & Whitney Canada Corp. Multi-spool gas turbine engine architecture
US10465611B2 (en) 2016-09-15 2019-11-05 Pratt & Whitney Canada Corp. Reverse flow multi-spool gas turbine engine with aft-end accessory gearbox drivingly connected to both high pressure spool and low pressure spool
US11555453B2 (en) 2016-09-15 2023-01-17 Pratt & Whitney Canada Corp. Reverse-flow gas turbine engine
US11415063B2 (en) 2016-09-15 2022-08-16 Pratt & Whitney Canada Corp. Reverse-flow gas turbine engine
US11408352B2 (en) 2016-09-15 2022-08-09 Pratt & Whitney Canada Corp. Reverse-flow gas turbine engine
US11035293B2 (en) 2016-09-15 2021-06-15 Pratt & Whitney Canada Corp. Reverse flow gas turbine engine with offset RGB
EP3321488A1 (fr) * 2016-11-15 2018-05-16 Pratt & Whitney Canada Corp. Arrangement d'accessoires de moteur à turbine à gaz
US10815899B2 (en) 2016-11-15 2020-10-27 Pratt & Whitney Canada Corp. Gas turbine engine accessories arrangement
US10808624B2 (en) 2017-02-09 2020-10-20 Pratt & Whitney Canada Corp. Turbine rotor with low over-speed requirements
US10746188B2 (en) 2017-03-14 2020-08-18 Pratt & Whitney Canada Corp. Inter-shaft bearing connected to a compressor boost system
US11536153B2 (en) 2018-08-08 2022-12-27 Pratt & Whitney Canada Corp. Turboshaft gas turbine engine
US11920479B2 (en) 2018-08-08 2024-03-05 Pratt & Whitney Canada Corp. Multi-engine system and method

Also Published As

Publication number Publication date
US3152443A (en) 1964-10-13

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