FR2665485A1 - Moteur a turbine a gaz. - Google Patents

Moteur a turbine a gaz. Download PDF

Info

Publication number
FR2665485A1
FR2665485A1 FR8317447A FR8317447A FR2665485A1 FR 2665485 A1 FR2665485 A1 FR 2665485A1 FR 8317447 A FR8317447 A FR 8317447A FR 8317447 A FR8317447 A FR 8317447A FR 2665485 A1 FR2665485 A1 FR 2665485A1
Authority
FR
France
Prior art keywords
compressor
outlet
flow
gas turbine
turbine engine
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.)
Pending
Application number
FR8317447A
Other languages
English (en)
French (fr)
Inventor
Roberts
Derek Aubrey
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 FR2665485A1 publication Critical patent/FR2665485A1/fr
Pending 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)
  • Control Of Turbines (AREA)
  • Supercharger (AREA)
FR8317447A 1982-03-23 1983-11-02 Moteur a turbine a gaz. Pending FR2665485A1 (fr)

Applications Claiming Priority (1)

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

Publications (1)

Publication Number Publication Date
FR2665485A1 true FR2665485A1 (fr) 1992-02-07

Family

ID=10529218

Family Applications (1)

Application Number Title Priority Date Filing Date
FR8317447A Pending FR2665485A1 (fr) 1982-03-23 1983-11-02 Moteur a turbine a gaz.

Country Status (3)

Country Link
DE (1) DE3341126A1 (enrdf_load_stackoverflow)
FR (1) FR2665485A1 (enrdf_load_stackoverflow)
GB (1) GB2242172B (enrdf_load_stackoverflow)

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

Citations (9)

* 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
US3841091A (en) * 1973-05-21 1974-10-15 Gen Electric Multi-mission tandem propulsion system
FR2243330A1 (enrdf_load_stackoverflow) * 1973-09-06 1975-04-04 Nasa
US3913321A (en) * 1972-11-17 1975-10-21 Rolls Royce 1971 Ltd Gas turbine engine power plant
US3972349A (en) * 1974-06-20 1976-08-03 United Technologies Corporation Variable ratio bypass gas turbine engine with flow diverter
FR2298001A1 (fr) * 1975-01-16 1976-08-13 Avon Rubber Co Ltd Dispositif gonflable de fermeture d'un moteur a reaction
US4038818A (en) * 1972-05-25 1977-08-02 Rolls-Royce (1971) Limited Gas turbine power plant having series-parallel valve arrangement
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
GB1511723A (en) * 1975-05-01 1978-05-24 Rolls Royce Variable stator vane actuating mechanism

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4222234A (en) * 1977-07-25 1980-09-16 General Electric Company Dual fan engine for VTOL pitch control

Patent Citations (9)

* 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
US4038818A (en) * 1972-05-25 1977-08-02 Rolls-Royce (1971) Limited Gas turbine power plant having series-parallel valve arrangement
US3913321A (en) * 1972-11-17 1975-10-21 Rolls Royce 1971 Ltd Gas turbine engine power plant
US3841091A (en) * 1973-05-21 1974-10-15 Gen Electric Multi-mission tandem propulsion system
FR2243330A1 (enrdf_load_stackoverflow) * 1973-09-06 1975-04-04 Nasa
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
FR2298001A1 (fr) * 1975-01-16 1976-08-13 Avon Rubber Co Ltd Dispositif gonflable de fermeture d'un moteur a reaction
GB1511723A (en) * 1975-05-01 1978-05-24 Rolls Royce Variable stator vane actuating mechanism

Also Published As

Publication number Publication date
GB2242172A (en) 1991-09-25
GB2242172B (en) 1991-12-11
DE3341126A1 (de) 1991-12-12
DE3341126C2 (enrdf_load_stackoverflow) 1993-03-11

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