FR3041990B1 - Ensemble de propulsion d'un aeronef - Google Patents

Ensemble de propulsion d'un aeronef Download PDF

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Publication number
FR3041990B1
FR3041990B1 FR1559443A FR1559443A FR3041990B1 FR 3041990 B1 FR3041990 B1 FR 3041990B1 FR 1559443 A FR1559443 A FR 1559443A FR 1559443 A FR1559443 A FR 1559443A FR 3041990 B1 FR3041990 B1 FR 3041990B1
Authority
FR
France
Prior art keywords
aircraft
turbine
propeller assembly
propeller
series
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
FR1559443A
Other languages
English (en)
Other versions
FR3041990A1 (fr
Inventor
Marc Michel Curlier Augustin
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 FR1559443A priority Critical patent/FR3041990B1/fr
Priority to GB1616669.6A priority patent/GB2544400B/en
Priority to US15/285,117 priority patent/US10364038B2/en
Publication of FR3041990A1 publication Critical patent/FR3041990A1/fr
Application granted granted Critical
Publication of FR3041990B1 publication Critical patent/FR3041990B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • 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
    • B64D35/04—Transmitting power from power plants to propellers or rotors; Arrangements of transmissions characterised by the transmission driving a plurality of propellers or rotors
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C11/00—Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
    • B64C11/46—Arrangements of, or constructional features peculiar to, multiple propellers
    • 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
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/02—Aircraft characterised by the type or position of power plants
    • B64D27/10—Aircraft characterised by the type or position of power plants of gas-turbine type 
    • 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
    • B64D35/02—Transmitting power from power plants to propellers or rotors; Arrangements of transmissions specially adapted for specific power plants
    • 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
    • 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
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
    • F02K3/02—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber
    • F02K3/04—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type
    • 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
    • F05D2220/323—Application in turbines in gas turbines for aircraft propulsion, e.g. jet engines
    • 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
    • F05D2240/00—Components
    • F05D2240/35—Combustors or associated equipment
    • 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
    • Y—GENERAL 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S464/00—Rotary shafts, gudgeons, housings, and flexible couplings for rotary shafts
    • Y10S464/904—Homokinetic coupling
    • Y10S464/906—Torque transmitted via radially spaced balls

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Motor Power Transmission Devices (AREA)

Abstract

La présente invention porte sur ensemble de propulsion d'un aéronef comprenant une turbine (5), au moins une hélice (10, 10') déportée par rapport à la turbine et un mécanisme (16) de transmission de puissance entre la turbine et l'hélice, caractérisé par le fait que le mécanisme de transmission (16) comprend en série deux joints homocinétiques (15, 17) avec une liaison à glissière.
FR1559443A 2015-10-05 2015-10-05 Ensemble de propulsion d'un aeronef Active FR3041990B1 (fr)

Priority Applications (3)

Application Number Priority Date Filing Date Title
FR1559443A FR3041990B1 (fr) 2015-10-05 2015-10-05 Ensemble de propulsion d'un aeronef
GB1616669.6A GB2544400B (en) 2015-10-05 2016-09-30 Propulsion unit for an aircraft
US15/285,117 US10364038B2 (en) 2015-10-05 2016-10-04 Propulsion unit for an aircraft

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1559443 2015-10-05
FR1559443A FR3041990B1 (fr) 2015-10-05 2015-10-05 Ensemble de propulsion d'un aeronef

Publications (2)

Publication Number Publication Date
FR3041990A1 FR3041990A1 (fr) 2017-04-07
FR3041990B1 true FR3041990B1 (fr) 2019-03-22

Family

ID=54545352

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1559443A Active FR3041990B1 (fr) 2015-10-05 2015-10-05 Ensemble de propulsion d'un aeronef

Country Status (3)

Country Link
US (1) US10364038B2 (fr)
FR (1) FR3041990B1 (fr)
GB (1) GB2544400B (fr)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US11156128B2 (en) 2018-08-22 2021-10-26 General Electric Company Embedded electric machine
CN112173094B (zh) * 2020-09-24 2023-12-26 成都沃飞天驭科技有限公司 一种多旋翼电动飞机的安全控制系统及方法

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1916442A (en) * 1929-08-21 1933-07-04 Alfred H Rzeppa Universal joint
FR935413A (fr) * 1946-10-28 1948-06-18 Dispositif d'actionnement des hélices d'un avion
US2875599A (en) * 1955-04-29 1959-03-03 Benjamin F Gregory Universal joint and lubricant retaining housing therefor
US3485462A (en) * 1967-08-28 1969-12-23 Spence William Aircraft propeller and jet drive
US4871130A (en) * 1988-06-21 1989-10-03 Walter Schulze Propulsion apparatus for an aircraft
US7540450B2 (en) * 2004-07-16 2009-06-02 Pratt & Whitney Canada Corp. Aircraft propulsion system
US8118683B2 (en) * 2005-09-27 2012-02-21 Shaft-Form-Engineering Gmbh Joint shaft and roller displacement UNIT THEREFOR
US7752834B2 (en) * 2006-10-25 2010-07-13 United Technologies Corporation Aircraft propulsion systems
US8960592B1 (en) * 2011-07-19 2015-02-24 D. Anthony Windisch VTOL propulsion for aircraft
FR3016189B1 (fr) * 2014-01-07 2018-09-28 Safran Aircraft Engines Dispositif de reduction epicycloidal pour l'entrainement en rotation des ensembles de pales d'une turbomachine a reducteur
FR3042009B1 (fr) * 2015-10-05 2018-07-13 Safran Aircraft Engines Turbo moteur a soufflantes deportees avec un systeme differentiel

Also Published As

Publication number Publication date
GB201616669D0 (en) 2016-11-16
US10364038B2 (en) 2019-07-30
US20170096231A1 (en) 2017-04-06
FR3041990A1 (fr) 2017-04-07
GB2544400B (en) 2021-06-02
GB2544400A (en) 2017-05-17

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