GB1572124A - Gas turbine engine - Google Patents

Gas turbine engine Download PDF

Info

Publication number
GB1572124A
GB1572124A GB11123/77A GB1112377A GB1572124A GB 1572124 A GB1572124 A GB 1572124A GB 11123/77 A GB11123/77 A GB 11123/77A GB 1112377 A GB1112377 A GB 1112377A GB 1572124 A GB1572124 A GB 1572124A
Authority
GB
United Kingdom
Prior art keywords
casing
engine
turbine
stator
outer casing
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
GB11123/77A
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.)
MTU Aero Engines AG
Original Assignee
MTU Motoren und Turbinen Union Muenchen GmbH
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 MTU Motoren und Turbinen Union Muenchen GmbH filed Critical MTU Motoren und Turbinen Union Muenchen GmbH
Publication of GB1572124A publication Critical patent/GB1572124A/en
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/08Cooling; Heating; Heat-insulation
    • 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
    • F02C3/14Gas-turbine plants characterised by the use of combustion products as the working fluid characterised by the arrangement of the combustion chamber in the plant
    • F02C3/145Gas-turbine plants characterised by the use of combustion products as the working fluid characterised by the arrangement of the combustion chamber in the plant the combustion chamber being in the reverse flow-type
    • 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)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
GB11123/77A 1976-04-17 1977-03-16 Gas turbine engine Expired GB1572124A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE2617024A DE2617024C2 (de) 1976-04-17 1976-04-17 Gasturbinentriebwerk

Publications (1)

Publication Number Publication Date
GB1572124A true GB1572124A (en) 1980-07-23

Family

ID=5975666

Family Applications (1)

Application Number Title Priority Date Filing Date
GB11123/77A Expired GB1572124A (en) 1976-04-17 1977-03-16 Gas turbine engine

Country Status (4)

Country Link
US (1) US4171614A (enExample)
DE (1) DE2617024C2 (enExample)
FR (1) FR2348366A1 (enExample)
GB (1) GB1572124A (enExample)

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2907748C2 (de) * 1979-02-28 1987-02-12 MTU Motoren- und Turbinen-Union München GmbH, 8000 München Einrichtung zur Minimierung und Konstanthaltung des Schaufelspitzenspiels einer axial durchströmten Hochdruckturbine eines Gasturbinentriebwerks
DE3022861C2 (de) * 1980-06-19 1983-12-08 M.A.N. Maschinenfabrik Augsburg-Nürnberg AG, 4200 Oberhausen Strömungsmaschine, insbesondere Heißgasturbine, und Verfahren zur selbsttätigen kontinuierlichen Beeinflussung des Labyrinthdichtugsspieles der Strömungsmaschine
US4993220A (en) * 1989-07-24 1991-02-19 Sundstrand Corporation Axial flow gas turbine engine combustor
US5667358A (en) * 1995-11-30 1997-09-16 Westinghouse Electric Corporation Method for reducing steady state rotor blade tip clearance in a land-based gas turbine to improve efficiency
US7214029B2 (en) * 2004-07-01 2007-05-08 Richter Donald L Laminar air turbine
US8864492B2 (en) * 2011-06-23 2014-10-21 United Technologies Corporation Reverse flow combustor duct attachment
US10385774B2 (en) 2016-09-19 2019-08-20 United Technologies Corporation Split compressor turbine engine
US12546227B2 (en) * 2024-02-09 2026-02-10 Rtx Corporation Cooling nozzle vanes of a turbine engine

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB666416A (en) * 1948-02-09 1952-02-13 Lysholm Alf Gas turbine power plant for jet propulsion
US2962256A (en) * 1956-03-28 1960-11-29 Napier & Son Ltd Turbine blade shroud rings
US3034298A (en) * 1958-06-12 1962-05-15 Gen Motors Corp Turbine cooling system
US3228190A (en) * 1962-08-16 1966-01-11 Power Jets Res & Dev Ltd Gas turbine plant
US3427000A (en) * 1966-11-14 1969-02-11 Westinghouse Electric Corp Axial flow turbine structure
US3575528A (en) * 1968-10-28 1971-04-20 Gen Motors Corp Turbine rotor cooling
BE756582A (fr) * 1969-10-02 1971-03-01 Gen Electric Ecran circulaire et support d'ecran avec dispositif de reglage de la temperature pour turbomachine
US3722215A (en) * 1971-03-30 1973-03-27 A Polyakov Gas-turbine plant
US3864056A (en) * 1973-07-27 1975-02-04 Westinghouse Electric Corp Cooled turbine blade ring assembly
US3892497A (en) * 1974-05-14 1975-07-01 Westinghouse Electric Corp Axial flow turbine stationary blade and blade ring locking arrangement

Also Published As

Publication number Publication date
DE2617024C2 (de) 1985-09-26
FR2348366A1 (fr) 1977-11-10
FR2348366B1 (enExample) 1980-04-11
US4171614A (en) 1979-10-23
DE2617024A1 (de) 1977-10-27

Similar Documents

Publication Publication Date Title
US5645397A (en) Turbine vane assembly with multiple passage cooled vanes
US3269120A (en) Gas turbine engine with compressor and turbine passages in a single rotor element
US2640319A (en) Cooling of gas turbines
US4697981A (en) Rotor thrust balancing
US2471892A (en) Reactive propulsion power plant having radial flow compressor and turbine means
US6612807B2 (en) Frame hub heating system
GB2154669A (en) Turbine stator nozzle
US3250512A (en) Gas turbine engine
US4466239A (en) Gas turbine engine with improved air cooling circuit
US3224194A (en) Gas turbine engine
US5273396A (en) Arrangement for defining improved cooling airflow supply path through clearance control ring and shroud
EP1446565B1 (en) Turbine engine with air cooled turbine
US4009569A (en) Diffuser-burner casing for a gas turbine engine
CN103161608B (zh) 采用轴流斜流串列复合压缩系统单转子微小型涡扇发动机
EP1173656B1 (en) High pressure turbine cooling of gas turbine engine
SE467316B (sv) Turbinmotorenhet med baktill monterade utloppsstyrskolvar
CA2042220A1 (en) Aft entry cooling system and method for an aircraft engine
JPH07208208A (ja) ガスタービンエンジン用汚染防止スラスト釣り合いシステム
US2922278A (en) Coaxial combustion products generator and turbine
US3824030A (en) Diaphragm and labyrinth seal assembly for gas turbines
US2441488A (en) Continuous combustion contraflow gas turbine
US5267831A (en) Axial flow gas turbines
US2682363A (en) Gas turbine engine
US4231704A (en) Cooling fluid bleed for axis of turbine rotor
US4183211A (en) Propulsion system for supersonic aircraft

Legal Events

Date Code Title Description
PS Patent sealed [section 19, patents act 1949]
PCNP Patent ceased through non-payment of renewal fee

Effective date: 19930316