FR3041934B1 - Ensemble de propulsion d'un aeronef - Google Patents

Ensemble de propulsion d'un aeronef Download PDF

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Publication number
FR3041934B1
FR3041934B1 FR1559455A FR1559455A FR3041934B1 FR 3041934 B1 FR3041934 B1 FR 3041934B1 FR 1559455 A FR1559455 A FR 1559455A FR 1559455 A FR1559455 A FR 1559455A FR 3041934 B1 FR3041934 B1 FR 3041934B1
Authority
FR
France
Prior art keywords
aircraft
propeller assembly
propeller
assembly
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.)
Active
Application number
FR1559455A
Other languages
English (en)
Other versions
FR3041934A1 (fr
Inventor
Marc Michel Curlier Augustin
Endy Bersot Jean-Francois
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.)
Safran Aircraft Engines SAS
Original Assignee
Safran Aircraft Engines SAS
SNECMA SAS
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 Safran Aircraft Engines SAS, SNECMA SAS filed Critical Safran Aircraft Engines SAS
Priority to FR1559455A priority Critical patent/FR3041934B1/fr
Publication of FR3041934A1 publication Critical patent/FR3041934A1/fr
Application granted granted Critical
Publication of FR3041934B1 publication Critical patent/FR3041934B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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
    • 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
    • F02C7/36—Power transmission arrangements between the different shafts of the gas turbine plant, or between the gas-turbine plant and the power user
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D35/00—Transmitting power from power plants to propellers or rotors; Arrangements of transmissions
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D15/00—Adaptations of machines or engines for special use; Combinations of engines with devices driven thereby
    • F01D15/12—Combinations with mechanical gearing
    • 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
    • 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
    • F05D2260/00—Function
    • F05D2260/40—Transmission of power
    • F05D2260/403—Transmission of power through the shape of the drive components
    • F05D2260/4031—Transmission of power through the shape of the drive components as in toothed gearing
    • F05D2260/40311—Transmission of power through the shape of the drive components as in toothed gearing of the epicyclical, planetary or differential type

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
FR1559455A 2015-10-05 2015-10-05 Ensemble de propulsion d'un aeronef Active FR3041934B1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR1559455A FR3041934B1 (fr) 2015-10-05 2015-10-05 Ensemble de propulsion d'un aeronef

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1559455 2015-10-05
FR1559455A FR3041934B1 (fr) 2015-10-05 2015-10-05 Ensemble de propulsion d'un aeronef

Publications (2)

Publication Number Publication Date
FR3041934A1 FR3041934A1 (fr) 2017-04-07
FR3041934B1 true FR3041934B1 (fr) 2018-07-13

Family

ID=55299598

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1559455A Active FR3041934B1 (fr) 2015-10-05 2015-10-05 Ensemble de propulsion d'un aeronef

Country Status (1)

Country Link
FR (1) FR3041934B1 (fr)

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1124823B (de) * 1959-05-02 1962-03-01 Daimler Benz Ag Antrieb fuer Flugzeuge
US3054577A (en) * 1961-02-27 1962-09-18 Forschungszentrums Der Luftfah Power plant for jet propelled aircraft
US4222235A (en) * 1977-07-25 1980-09-16 General Electric Company Variable cycle engine
DE3713249A1 (de) * 1987-04-18 1988-11-03 Schulze Walter Antriebseinrichtung fuer ein flugzeug
DE102008062813A1 (de) * 2008-12-23 2010-07-15 Rolls-Royce Deutschland Ltd & Co Kg Flugzeug mit einer Heck-Propeller-Triebwerksanordnung
GB2506464B (en) * 2013-04-24 2015-08-19 Rolls Royce Plc An Aircraft Powerplant
US9878796B2 (en) * 2014-03-27 2018-01-30 United Technologies Corporation Hybrid drive for gas turbine engine

Also Published As

Publication number Publication date
FR3041934A1 (fr) 2017-04-07

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