PL4077887T3 - Turbogenerator do statku powietrznego, zawierający ulepszony układ olejowy - Google Patents

Turbogenerator do statku powietrznego, zawierający ulepszony układ olejowy

Info

Publication number
PL4077887T3
PL4077887T3 PL20845787.9T PL20845787T PL4077887T3 PL 4077887 T3 PL4077887 T3 PL 4077887T3 PL 20845787 T PL20845787 T PL 20845787T PL 4077887 T3 PL4077887 T3 PL 4077887T3
Authority
PL
Poland
Prior art keywords
turbogenerator
aircraft
oil system
improved oil
improved
Prior art date
Application number
PL20845787.9T
Other languages
English (en)
Inventor
Camel SERGHINE
Denis Antoine Julien REAL
Original Assignee
Safran Helicopter Engines
Safran Power Units
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 Helicopter Engines, Safran Power Units filed Critical Safran Helicopter Engines
Publication of PL4077887T3 publication Critical patent/PL4077887T3/pl

Links

Classifications

    • 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
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/18—Lubricating arrangements
    • 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
    • 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
    • B64D27/24—Aircraft characterised by the type or position of power plants using steam or spring force
    • 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
    • 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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B01—PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
    • B01D—SEPARATION
    • B01D45/00—Separating dispersed particles from gases or vapours by gravity, inertia, or centrifugal forces
    • B01D45/04—Separating dispersed particles from gases or vapours by gravity, inertia, or centrifugal forces by utilising inertia
    • B01D45/08—Separating dispersed particles from gases or vapours by gravity, inertia, or centrifugal forces by utilising inertia by impingement against baffle separators
    • 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
    • B64D27/026—Aircraft characterised by the type or position of power plants comprising different types of power plants, e.g. combination of a piston engine and a gas-turbine
    • 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
    • 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
    • F05D2260/60—Fluid transfer
    • F05D2260/609—Deoiling or demisting
    • 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
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Connection Of Motors, Electrical Generators, Mechanical Devices, And The Like (AREA)
  • Motor Or Generator Cooling System (AREA)
PL20845787.9T 2019-12-20 2020-12-18 Turbogenerator do statku powietrznego, zawierający ulepszony układ olejowy PL4077887T3 (pl)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1915265A FR3105298B1 (fr) 2019-12-20 2019-12-20 Turbogenerateur pour aeronef, comprenant un système d’huile amélioré
PCT/FR2020/052522 WO2021123657A1 (fr) 2019-12-20 2020-12-18 Turbogenerateur pour aeronef, comprenant un système d'huile amélioré

Publications (1)

Publication Number Publication Date
PL4077887T3 true PL4077887T3 (pl) 2024-04-08

Family

ID=69811333

Family Applications (1)

Application Number Title Priority Date Filing Date
PL20845787.9T PL4077887T3 (pl) 2019-12-20 2020-12-18 Turbogenerator do statku powietrznego, zawierający ulepszony układ olejowy

Country Status (6)

Country Link
US (1) US11891907B2 (pl)
EP (1) EP4077887B1 (pl)
CN (1) CN114929994B (pl)
FR (1) FR3105298B1 (pl)
PL (1) PL4077887T3 (pl)
WO (1) WO2021123657A1 (pl)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20220371742A1 (en) * 2021-05-19 2022-11-24 Avco Corporation Integrated alternator for aerial vehicle engine

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1264170A (fr) * 1960-07-05 1961-06-19 Lindes Eismaschinen Ag Séparateur d'huile pour gaz
JP5568596B2 (ja) * 2012-05-30 2014-08-06 川崎重工業株式会社 航空機用エンジンのギヤボックス一体型発電装置
FR3007463B1 (fr) * 2013-06-21 2017-10-20 Hispano-Suiza Boitier d'accessoires de turbomachine equipe d'un separateur air/huile
GB201615491D0 (en) * 2016-09-13 2016-10-26 Delta Motorsport Ltd Improvements in or relating to gas turbine generators
FR3056635B1 (fr) * 2016-09-26 2020-05-29 Safran Helicopter Engines Systeme de deshuilage d'un melange air/huile de pressurisation d'etancheites d'une turbomachine
DE102017128483A1 (de) * 2017-11-30 2019-06-06 Rolls-Royce Deutschland Ltd & Co Kg Flugtriebwerk
GB201808855D0 (en) * 2018-05-31 2018-07-18 Rolls Royce Plc Oil recovery system
CN109441637B (zh) * 2018-09-03 2020-07-24 北京航空航天大学 一种利用氮气增压油箱的飞机富余电力综合系统和方法

Also Published As

Publication number Publication date
US20230026754A1 (en) 2023-01-26
CN114929994B (zh) 2024-08-20
FR3105298A1 (fr) 2021-06-25
CN114929994A (zh) 2022-08-19
EP4077887B1 (fr) 2023-11-22
US11891907B2 (en) 2024-02-06
WO2021123657A1 (fr) 2021-06-24
FR3105298B1 (fr) 2021-12-03
EP4077887A1 (fr) 2022-10-26

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