FR3090049B1 - Turbomachine comportant un alternateur entre deux elements contrarotatifs - Google Patents

Turbomachine comportant un alternateur entre deux elements contrarotatifs Download PDF

Info

Publication number
FR3090049B1
FR3090049B1 FR1872793A FR1872793A FR3090049B1 FR 3090049 B1 FR3090049 B1 FR 3090049B1 FR 1872793 A FR1872793 A FR 1872793A FR 1872793 A FR1872793 A FR 1872793A FR 3090049 B1 FR3090049 B1 FR 3090049B1
Authority
FR
France
Prior art keywords
alternator
fan
low pressure
pressure shaft
contrarotary
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
FR1872793A
Other languages
English (en)
Other versions
FR3090049A1 (fr
Inventor
Alexandre Jean-Marie Tan-Kim
Julien Fabien Patrick Becoulet
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
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 filed Critical Safran Aircraft Engines SAS
Priority to FR1872793A priority Critical patent/FR3090049B1/fr
Priority to US16/709,990 priority patent/US11041400B2/en
Publication of FR3090049A1 publication Critical patent/FR3090049A1/fr
Application granted granted Critical
Publication of FR3090049B1 publication Critical patent/FR3090049B1/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
    • 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
    • F01D1/00—Non-positive-displacement machines or engines, e.g. steam turbines
    • F01D1/24—Non-positive-displacement machines or engines, e.g. steam turbines characterised by counter-rotating rotors subjected to same working fluid stream without intermediate stator blades or the like
    • 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
    • F01D15/10—Adaptations for driving, or combinations with, electric generators
    • 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
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/02—Blade-carrying members, e.g. rotors
    • F01D5/026—Shaft to shaft connections
    • 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
    • F02C7/06—Arrangements of bearings; Lubricating
    • 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
    • F02K3/06—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 with front fan
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16H—GEARING
    • F16H57/00—General details of gearing
    • F16H57/02—Gearboxes; Mounting gearing therein
    • 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
    • F05D2220/70—Application in combination with
    • F05D2220/76—Application in combination with an electrical generator
    • 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
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16H—GEARING
    • F16H57/00—General details of gearing
    • F16H57/02—Gearboxes; Mounting gearing therein
    • F16H2057/02039—Gearboxes for particular applications
    • F16H2057/02069—Gearboxes for particular applications for industrial applications
    • F16H2057/02073—Reduction gearboxes for industry

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Connection Of Motors, Electrical Generators, Mechanical Devices, And The Like (AREA)

Abstract

L'invention propose une turbomachine à engrenages comportant une soufflante (16), un arbre basse pression (28) qui entraine la soufflante (16) en rotation autour de l'axe principal (A) de la turbomachine (10), un réducteur (40) de vitesse interposé entre la soufflante (16) et l'arbre basse pression (28), et un alternateur (52) entrainé notamment par l'arbre basse pression (28), caractérisée en ce que l'alternateur (52) comporte un inducteur (54) et un induit (56) dont l'un de l'inducteur (54) et de l'induit (56) est solidaire de la soufflante (16) et l'autre de l'inducteur (54) et de l'induit (56) est solidaire de l'arbre basse pression (28). Figure pour l’abrégé : Figure 3
FR1872793A 2018-12-12 2018-12-12 Turbomachine comportant un alternateur entre deux elements contrarotatifs Active FR3090049B1 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
FR1872793A FR3090049B1 (fr) 2018-12-12 2018-12-12 Turbomachine comportant un alternateur entre deux elements contrarotatifs
US16/709,990 US11041400B2 (en) 2018-12-12 2019-12-11 Turbomachine comprising an alternator between two counter-rotating elements

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1872793A FR3090049B1 (fr) 2018-12-12 2018-12-12 Turbomachine comportant un alternateur entre deux elements contrarotatifs

Publications (2)

Publication Number Publication Date
FR3090049A1 FR3090049A1 (fr) 2020-06-19
FR3090049B1 true FR3090049B1 (fr) 2021-01-15

Family

ID=66641041

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1872793A Active FR3090049B1 (fr) 2018-12-12 2018-12-12 Turbomachine comportant un alternateur entre deux elements contrarotatifs

Country Status (2)

Country Link
US (1) US11041400B2 (fr)
FR (1) FR3090049B1 (fr)

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2610565A (en) 2021-09-08 2023-03-15 Rolls Royce Plc An improved gas turbine engine
EP4148250A1 (fr) 2021-09-08 2023-03-15 Rolls-Royce plc Moteur à turbine à gaz améliorée
GB2610572A (en) * 2021-09-08 2023-03-15 Rolls Royce Plc An improved gas turbine engine
GB2610571A (en) * 2021-09-08 2023-03-15 Rolls Royce Plc An improved gas turbine engine
EP4148263A1 (fr) * 2021-09-08 2023-03-15 Rolls-Royce plc Moteur à turbine à gaz amélioré
GB2610573A (en) * 2021-09-08 2023-03-15 Rolls Royce Plc An improved gas turbine engine
GB2610568A (en) 2021-09-08 2023-03-15 Rolls Royce Plc An improved gas turbine engine
GB202118041D0 (en) * 2021-12-14 2022-01-26 Rolls Royce Plc Restarting a gas turbine engine

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8375695B2 (en) * 2009-06-30 2013-02-19 General Electric Company Aircraft gas turbine engine counter-rotatable generator
US9915164B2 (en) * 2014-05-20 2018-03-13 United Technologies Corporation Geared turbofan with high speed generator
JP6554282B2 (ja) * 2014-12-24 2019-07-31 川崎重工業株式会社 航空機用エンジン装置
FR3054264B1 (fr) * 2016-07-25 2020-07-03 Safran Aircraft Engines Turbomachine a reducteur a train epicycloidal

Also Published As

Publication number Publication date
FR3090049A1 (fr) 2020-06-19
US11041400B2 (en) 2021-06-22
US20200191010A1 (en) 2020-06-18

Similar Documents

Publication Publication Date Title
FR3090049B1 (fr) Turbomachine comportant un alternateur entre deux elements contrarotatifs
US8456051B2 (en) High reliability generator with dual drive path
FR3066552B1 (fr) Assemblage sur un arbre de turbomachine d'un disque aubage monobloc et d'un rotor de compresseur basse pression a au moins deux etages d'aubes mobiles
FR3048675B1 (fr) Alimentation en air d'un circuit de conditionnement d'air d'une cabine d'un aeronef
ATE368802T1 (de) Hydraulischer drehzahlsteigernder antrieb für wasserströmungsturbine
FR3050504B1 (fr) Reducteur cycloidal avec rattrapage automatique de jeu et systeme de direction assistee pourvu d’un tel reducteur
FR3061242B1 (fr) Turbomachine comportant un moyen de decouplage d'une soufflante
FR3022587B1 (fr) Dispositif et procede de lubrification d’un palier a roulement de turbomachine
FR3083386B1 (fr) Ensemble ralentisseur electromagnetique et generatrice et vehicule comportant un tel ensemble
FR3074476B1 (fr) Turbopropulseur d'aeronef comportant une helice non carenee
FR3049007B1 (fr) Turboreacteur ayant un groupe lubrification des paliers simplifie
FR3015569B1 (fr) Carter pour un ensemble propulsif
FR3060061B1 (fr) Turbomachine a turbine libre pour aeronef
WO2019024848A3 (fr) Réducteur de vitesse ayant une boucle de câble en forme de poisson
FR3042249B3 (fr) Transmission entre un moteur a combustion et un element faisant office de compresseur, et installation de compression munie d'une transmission de ce type
FR3058470B1 (fr) Turbopropulseur comprenant un generateur de gaz et une boite d'accessoires accouplee a une extremite arriere d'un arbre haute pression du generateur de gaz
FR3051405B1 (fr) Appareil de transmission de puissance
FR3058587B1 (fr) Compresseur electrique avec roulement ameliore
FR3104192B1 (fr) Turbomachine a turbine contrarotative pour un aeronef
FR3073569B1 (fr) Turbopropulseur comportant un mecanisme de reduction integrant un dispositif de generation de courant
GB973388A (en) Accessory power drive mechanism for a gas turbine engine
BR112018006791A2 (pt) compressor
FR3046402B1 (fr) Systeme de changement de pas pour turbopropulseur a doublet d'helices contrarotatives amont
BRPI0406171A (pt) Dispositivo anti-retorno em uma engrenagem
FR3058481B1 (fr) Compresseur axial comportant des rotors juxtaposes tournant dans des directions inverses

Legal Events

Date Code Title Description
PLFP Fee payment

Year of fee payment: 2

PLSC Publication of the preliminary search report

Effective date: 20200619

PLFP Fee payment

Year of fee payment: 3

PLFP Fee payment

Year of fee payment: 4

PLFP Fee payment

Year of fee payment: 5

PLFP Fee payment

Year of fee payment: 6