GB2242172B - Gas turbine engine - Google Patents

Gas turbine engine

Info

Publication number
GB2242172B
GB2242172B GB8328254A GB8328254A GB2242172B GB 2242172 B GB2242172 B GB 2242172B GB 8328254 A GB8328254 A GB 8328254A GB 8328254 A GB8328254 A GB 8328254A GB 2242172 B GB2242172 B GB 2242172B
Authority
GB
United Kingdom
Prior art keywords
gas turbine
turbine engine
engine
gas
turbine
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 - Fee Related
Application number
GB8328254A
Other languages
English (en)
Other versions
GB2242172A (en
Inventor
Derek Aubrey Roberts
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.)
Rolls Royce PLC
Original Assignee
Rolls Royce PLC
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 Rolls Royce PLC filed Critical Rolls Royce PLC
Publication of GB2242172A publication Critical patent/GB2242172A/en
Application granted granted Critical
Publication of GB2242172B publication Critical patent/GB2242172B/en
Anticipated expiration legal-status Critical
Expired - Fee Related 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
    • F02C6/00—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use
    • F02C6/04—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output
    • F02C6/06—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output providing compressed gas
    • 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
    • F02C3/13—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor having variable working fluid interconnections between turbines or compressors or stages of different rotors
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2220/00—Application
    • F05D2220/30—Application in turbines
    • F05D2220/32—Application in turbines in gas turbines
    • F05D2220/328—Application in turbines in gas turbines providing direct vertical lift

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Supercharger (AREA)
  • Control Of Turbines (AREA)
GB8328254A 1982-03-23 1983-03-18 Gas turbine engine Expired - Fee Related GB2242172B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB8208521 1982-03-23

Publications (2)

Publication Number Publication Date
GB2242172A GB2242172A (en) 1991-09-25
GB2242172B true GB2242172B (en) 1991-12-11

Family

ID=10529218

Family Applications (1)

Application Number Title Priority Date Filing Date
GB8328254A Expired - Fee Related GB2242172B (en) 1982-03-23 1983-03-18 Gas turbine engine

Country Status (3)

Country Link
DE (1) DE3341126A1 (en:Method)
FR (1) FR2665485A1 (en:Method)
GB (1) GB2242172B (en:Method)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2313580B (en) 1996-05-31 2000-02-23 Astovl Limited An aircraft power plant
AT406574B (de) * 1999-02-11 2000-06-26 Bobleter Ortwin Antriebseinrichtung für ein fluggerät
FR3158709A1 (fr) * 2024-01-30 2025-08-01 Ascendance Flight Technologies Dispositif d’entrée d’air pour aéronef à décollage vertical

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2879014A (en) * 1957-07-02 1959-03-24 Bell Aircraft Corp Jet propelled airplane with jet diverter
GB1389347A (en) * 1972-05-25 1975-04-03 Rolls Royce Gas turbine power plant
GB1415679A (en) * 1972-11-17 1975-11-26 Rolls Royce Gas turbine engine powerplant
US3841091A (en) * 1973-05-21 1974-10-15 Gen Electric Multi-mission tandem propulsion system
US4033119A (en) * 1973-09-06 1977-07-05 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Dual cycle aircraft turbine engine
FR2355169A1 (fr) * 1974-03-23 1978-01-13 Rolls Royce Perfectionnements aux avions a decollage et atterrissage vertical ou court et aux turbomoteurs pour ces avions
US3972349A (en) * 1974-06-20 1976-08-03 United Technologies Corporation Variable ratio bypass gas turbine engine with flow diverter
GB1497153A (en) * 1975-01-16 1978-01-05 Avon Rubber Co Ltd Inflatable bung
GB1511723A (en) * 1975-05-01 1978-05-24 Rolls Royce Variable stator vane actuating mechanism
US4222234A (en) * 1977-07-25 1980-09-16 General Electric Company Dual fan engine for VTOL pitch control

Also Published As

Publication number Publication date
FR2665485A1 (fr) 1992-02-07
GB2242172A (en) 1991-09-25
DE3341126C2 (en:Method) 1993-03-11
DE3341126A1 (de) 1991-12-12

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Legal Events

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

Effective date: 19970318