UA91023C2 - Газотурбинный двигатель и стартер-генератор для газотурбинного двигателя - Google Patents

Газотурбинный двигатель и стартер-генератор для газотурбинного двигателя

Info

Publication number
UA91023C2
UA91023C2 UAA200700715A UAA200700715A UA91023C2 UA 91023 C2 UA91023 C2 UA 91023C2 UA A200700715 A UAA200700715 A UA A200700715A UA A200700715 A UAA200700715 A UA A200700715A UA 91023 C2 UA91023 C2 UA 91023C2
Authority
UA
Ukraine
Prior art keywords
turbomachine
starter
integral generator
pressure compressor
generator
Prior art date
Application number
UAA200700715A
Other languages
English (en)
Ukrainian (uk)
Inventor
Филипп Пьер Винсен Буйер
Энтони Лоран
Стефан Русселен
Original Assignee
Снекма
Испано-Сюиза
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 Снекма, Испано-Сюиза filed Critical Снекма
Publication of UA91023C2 publication Critical patent/UA91023C2/ru

Links

Classifications

    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02K—DYNAMO-ELECTRIC MACHINES
    • H02K7/00—Arrangements for handling mechanical energy structurally associated with dynamo-electric machines, e.g. structural association with mechanical driving motors or auxiliary dynamo-electric machines
    • H02K7/14—Structural association with mechanical loads, e.g. with hand-held machine tools or fans
    • 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
    • F01D9/00—Stators
    • F01D9/06—Fluid supply conduits to nozzles or the like
    • F01D9/065—Fluid supply or removal conduits traversing the working fluid flow, e.g. for lubrication-, cooling-, or sealing fluids
    • 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
    • F02C7/26—Starting; Ignition
    • F02C7/268—Starting drives for the rotor, acting directly on the rotor of the gas turbine to be started
    • 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
    • F02C7/26—Starting; Ignition
    • F02C7/268—Starting drives for the rotor, acting directly on the rotor of the gas turbine to be started
    • F02C7/275—Mechanical drives
    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02K—DYNAMO-ELECTRIC MACHINES
    • H02K5/00—Casings; Enclosures; Supports
    • H02K5/04—Casings or enclosures characterised by the shape, form or construction thereof
    • H02K5/22—Auxiliary parts of casings not covered by groups H02K5/06-H02K5/20, e.g. shaped to form connection boxes or terminal boxes
    • H02K5/225—Terminal boxes or connection arrangements
    • 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
    • F05D2260/85—Starting

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Power Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Connection Of Motors, Electrical Generators, Mechanical Devices, And The Like (AREA)
  • Motor Or Generator Cooling System (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

Газотурбинный двигатель содержит электрический стартер-генератор (26), выполненный с возможностью установки и демонтажа путем осевого поступательного перемещения в переднем отсеке (18) газотурбинного двигателя между компрессором низкого давления и компрессором высокого давления и соединенный с электрическими кабелями (34), проложенными внутри конструктивных стояков (12) промежуточного картера (10) газотурбинного двигателя.
UAA200700715A 2006-01-24 2007-01-23 Газотурбинный двигатель и стартер-генератор для газотурбинного двигателя UA91023C2 (ru)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0600617A FR2896537B1 (fr) 2006-01-24 2006-01-24 Turbomachine a generateur-demarreur integre

Publications (1)

Publication Number Publication Date
UA91023C2 true UA91023C2 (ru) 2010-06-25

Family

ID=37075518

Family Applications (1)

Application Number Title Priority Date Filing Date
UAA200700715A UA91023C2 (ru) 2006-01-24 2007-01-23 Газотурбинный двигатель и стартер-генератор для газотурбинного двигателя

Country Status (7)

Country Link
US (2) US7619331B2 (ru)
EP (1) EP1811132B1 (ru)
JP (1) JP4800978B2 (ru)
CA (1) CA2575343C (ru)
FR (1) FR2896537B1 (ru)
RU (1) RU2406829C2 (ru)
UA (1) UA91023C2 (ru)

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FR2896537B1 (fr) * 2006-01-24 2011-07-29 Snecma Turbomachine a generateur-demarreur integre
FR2942271B1 (fr) * 2009-02-16 2011-05-13 Hispano Suiza Sa Moteur aeronautique avec refroidissement d'un dispositif electrique de demarrage
ITCO20100067A1 (it) * 2010-12-23 2012-06-24 Nuovo Pignone Spa Connessione elettrica per turbomacchina e metodo
JP5290345B2 (ja) * 2011-03-31 2013-09-18 株式会社小松製作所 発電電動機および作業機械
JP5358609B2 (ja) * 2011-03-31 2013-12-04 株式会社小松製作所 発電電動機および作業機械
JP5416158B2 (ja) * 2011-03-31 2014-02-12 株式会社小松製作所 発電電動機および作業機械
EP2571145B1 (en) * 2011-09-13 2017-08-02 General Electric Technology GmbH Connection arrangement for windings of electric machines
US9410447B2 (en) * 2012-07-30 2016-08-09 United Technologies Corporation Forward compartment service system for a geared architecture gas turbine engine
US9097134B2 (en) * 2012-09-14 2015-08-04 Pratt & Whitney Canada Corp. Air cooling design for tail-cone generator installation
US9856746B2 (en) 2013-03-14 2018-01-02 United Technologies Corporation Heatshield discourager seal for a gas turbine engine
CN105164388B (zh) * 2013-03-15 2017-05-31 联合工艺公司 仪器传递支柱
DE102013107144A1 (de) * 2013-07-08 2015-01-22 Valeo Systèmes d'Essuyage Gehäuseelement für einen Wischermotor, Verfahren zum Herstellen eines Gehäuseelements sowie Wischermotor
EP3246526B1 (en) * 2016-05-18 2021-03-24 Rolls-Royce Corporation Control of low pressure shaft generator for gas turbine engine
US10308366B2 (en) 2016-08-22 2019-06-04 General Electric Company Embedded electric machine
US11022042B2 (en) 2016-08-29 2021-06-01 Rolls-Royce North American Technologies Inc. Aircraft having a gas turbine generator with power assist
BE1025139B1 (fr) 2017-04-14 2018-11-20 Safran Aero Boosters S.A. Connecteur electrique pour carter de turbomachine
RU2727655C2 (ru) * 2018-06-13 2020-07-22 Никита Владимирович Гусев Малоразмерный газотурбинный двигатель
US11156128B2 (en) 2018-08-22 2021-10-26 General Electric Company Embedded electric machine
FR3087823B1 (fr) * 2018-10-26 2020-11-13 Safran Aircraft Engines Module de soufflante equipe d'une machine electrique pour une turbomachine d'aeronef
US20200325821A1 (en) 2019-04-09 2020-10-15 Rolls-Royce North American Technologies Inc. Starter/generator
US11047251B2 (en) 2019-07-17 2021-06-29 Rolls-Royce Corporation Routing for electrical communication in gas turbine engines
FR3103852B1 (fr) * 2019-12-03 2021-10-22 Safran Aircraft Engines Module electrique pour une turbomachine d’aeronef
FR3103853B1 (fr) 2019-12-03 2021-11-05 Safran Aircraft Engines Raccordement electrique d’une machine electrique dans une turbomachine d’aeronef
FR3103854B1 (fr) * 2019-12-03 2022-01-28 Safran Aircraft Engines Raccordement electrique d’une machine electrique dans une turbomachine d’aeronef
FR3103851B1 (fr) * 2019-12-03 2021-11-05 Safran Aircraft Engines Barre rigide pour le raccordement electrique d’une machine dans une turbomachine d’aeronef
US11637475B2 (en) * 2020-03-09 2023-04-25 Hamilton Sundstrand Corporation Terminal block for integrated tail cone and mounted generator
FR3114351B1 (fr) 2020-09-18 2022-08-12 Safran Aircraft Engines Raccordement electrique d’une machine electrique dans une turbomachine d’aeronef
US11852024B2 (en) * 2020-12-18 2023-12-26 Ge Aviation Systems Llc Electrical strut for a turbine engine
US11661856B2 (en) 2021-03-19 2023-05-30 Rolls-Royce North American Technologies Inc. Gas turbine engine with embedded generator
RU206951U1 (ru) * 2021-06-09 2021-10-04 федеральное государственное бюджетное образовательное учреждение высшего образования «Уфимский государственный авиационный технический университет» Дисковый стартер-генератор, интегрированный в двухконтурный турбореактивный двигатель
FR3124543B1 (fr) 2021-06-23 2023-05-12 Safran Aircraft Engines Turbomachine d’aeronef equipee d’une machine electrique
GB2613076B (en) * 2021-10-15 2024-06-05 Rtx Corp Electric machine within a turbine engine
FR3129537B1 (fr) 2021-11-22 2023-12-01 Safran Aircraft Engines Systeme de connexion electrique protegee par boitier imperdable
FR3129427A1 (fr) 2021-11-22 2023-05-26 Safran Aircraft Engines Carter d’echappement comportant un bras creux traverse par un element conducteur de transmission de puissance
EP4280429A1 (en) * 2022-05-17 2023-11-22 Hamilton Sundstrand Corporation Ceramic sleeve for a stator housing of an electrical machine
FR3141486A1 (fr) * 2022-10-28 2024-05-03 Safran Nacelles Aube directrice de turbomachine intégrant un dispositif de distribution électrique
US20240266916A1 (en) * 2023-02-07 2024-08-08 Hamilton Sundstrand Corporation Generator with moisture seals

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Also Published As

Publication number Publication date
EP1811132A1 (fr) 2007-07-25
US20070217905A1 (en) 2007-09-20
FR2896537B1 (fr) 2011-07-29
FR2896537A1 (fr) 2007-07-27
RU2406829C2 (ru) 2010-12-20
CA2575343A1 (fr) 2007-07-24
US20090309432A1 (en) 2009-12-17
US7619331B2 (en) 2009-11-17
JP2007198378A (ja) 2007-08-09
EP1811132B1 (fr) 2014-10-15
JP4800978B2 (ja) 2011-10-26
CA2575343C (fr) 2014-06-10
US7855483B2 (en) 2010-12-21
RU2007102520A (ru) 2008-07-27

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