PL435034A1 - Zespoły silnika napędowego zapewniające dostęp do elementów składowych w komorach pędnych - Google Patents

Zespoły silnika napędowego zapewniające dostęp do elementów składowych w komorach pędnych

Info

Publication number
PL435034A1
PL435034A1 PL435034A PL43503420A PL435034A1 PL 435034 A1 PL435034 A1 PL 435034A1 PL 435034 A PL435034 A PL 435034A PL 43503420 A PL43503420 A PL 43503420A PL 435034 A1 PL435034 A1 PL 435034A1
Authority
PL
Poland
Prior art keywords
propulsion
components
chambers
driving
providing access
Prior art date
Application number
PL435034A
Other languages
English (en)
Inventor
Mirosław Czarnik
Tomasz Edward BERDOWSKI
Paweł Zdrojewski
Łukasz Maciej Janczak
Maciej GRUNWALD
Original Assignee
General Electric Company Polska Spółka Z Ograniczoną Odpowiedzialnością
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 General Electric Company Polska Spółka Z Ograniczoną Odpowiedzialnością filed Critical General Electric Company Polska Spółka Z Ograniczoną Odpowiedzialnością
Priority to PL435034A priority Critical patent/PL435034A1/pl
Priority to US17/381,360 priority patent/US20220055759A1/en
Priority to EP21188878.9A priority patent/EP3957829A1/en
Priority to CN202110960829.6A priority patent/CN114076029A/zh
Publication of PL435034A1 publication Critical patent/PL435034A1/pl

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
    • 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
    • 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
    • B64D29/00—Power-plant nacelles, fairings, or cowlings
    • B64D29/02—Power-plant nacelles, fairings, or cowlings associated with wings
    • 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
    • F02C6/00—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use
    • F02C6/20—Adaptations of gas-turbine plants for driving vehicles
    • F02C6/206—Adaptations of gas-turbine plants for driving vehicles the vehicles being airscrew driven
    • 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 
    • B64D27/12—Aircraft characterised by the type or position of power plants of gas-turbine type  within, or attached to, wings
    • 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
    • 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
    • F01D5/005—Repairing methods or devices
    • 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
    • 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
    • F02C7/32—Arrangement, mounting, or driving, of auxiliaries
    • 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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
    • B64F5/00—Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
    • B64F5/40—Maintaining or repairing aircraft
    • 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
    • F05D2230/00—Manufacture
    • F05D2230/72—Maintenance
    • 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
    • F05D2230/00—Manufacture
    • F05D2230/80—Repairing, retrofitting or upgrading methods
    • 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)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Connection Of Motors, Electrical Generators, Mechanical Devices, And The Like (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Superconductive Dynamoelectric Machines (AREA)
  • Rotary Pumps (AREA)
  • Portable Nailing Machines And Staplers (AREA)

Abstract

Przedmiotem zgłoszenia przedstawionym na rysunku są zespoły silnika napędowego zapewniające dostęp do elementów składowych w komorach pędnych. Ujawniono silniki napędowe oraz sposoby uzyskiwania dostępu do elementów składowych w komorach pędnych silników napędowych. Silnik napędowy zawiera zewnętrzną obudowę silnika, która zawiera komorę pędną znajdującą się w jej wnętrzu. Komora pędna jest usytuowana osiowo między sprężarką niskiego ciśnienia a wentylatorem silnika napędowego. W komorze pędnej umieszczony jest przetwornik elektryczny.
PL435034A 2020-08-20 2020-08-20 Zespoły silnika napędowego zapewniające dostęp do elementów składowych w komorach pędnych PL435034A1 (pl)

Priority Applications (4)

Application Number Priority Date Filing Date Title
PL435034A PL435034A1 (pl) 2020-08-20 2020-08-20 Zespoły silnika napędowego zapewniające dostęp do elementów składowych w komorach pędnych
US17/381,360 US20220055759A1 (en) 2020-08-20 2021-07-21 Propulsion engine assemblies providing access to components within propulsor cavities
EP21188878.9A EP3957829A1 (en) 2020-08-20 2021-07-30 Propulsion engine assemblies providing access to components within propulsor cavities
CN202110960829.6A CN114076029A (zh) 2020-08-20 2021-08-20 提供接近推进器腔内的构件的推进发动机组件

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
PL435034A PL435034A1 (pl) 2020-08-20 2020-08-20 Zespoły silnika napędowego zapewniające dostęp do elementów składowych w komorach pędnych

Publications (1)

Publication Number Publication Date
PL435034A1 true PL435034A1 (pl) 2022-02-21

Family

ID=77167991

Family Applications (1)

Application Number Title Priority Date Filing Date
PL435034A PL435034A1 (pl) 2020-08-20 2020-08-20 Zespoły silnika napędowego zapewniające dostęp do elementów składowych w komorach pędnych

Country Status (4)

Country Link
US (1) US20220055759A1 (pl)
EP (1) EP3957829A1 (pl)
CN (1) CN114076029A (pl)
PL (1) PL435034A1 (pl)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US11753144B2 (en) * 2021-10-15 2023-09-12 General Electric Company Unducted propulsion system
US11572827B1 (en) 2021-10-15 2023-02-07 General Electric Company Unducted propulsion system

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US3859785A (en) * 1973-12-17 1975-01-14 Curtiss Wright Corp Turbine engine with integral compressor and alternator rotor
FR2712250B1 (fr) * 1993-11-10 1995-12-29 Hispano Suiza Sa Procédé et dispositif de commande de variation du pas des pales d'un rotor.
FR2906568B1 (fr) * 2006-10-02 2012-01-06 Aircelle Sa Structure d'entree d'air deposable pour nacelle de turboreacteur.
GB0713527D0 (en) * 2007-07-12 2007-08-22 Rolls Royce Plc A Synchronous electrical machine
US20140157757A1 (en) * 2007-09-21 2014-06-12 United Technologies Corporation Gas turbine engine compressor arrangement
US20140157753A1 (en) * 2007-09-21 2014-06-12 United Technologies Corporation Gas turbine engine compressor arrangement
US20140157755A1 (en) * 2007-09-21 2014-06-12 United Technologies Corporation Gas turbine engine compressor arrangement
US20140157754A1 (en) * 2007-09-21 2014-06-12 United Technologies Corporation Gas turbine engine compressor arrangement
US20140157752A1 (en) * 2007-09-21 2014-06-12 United Technologies Corporation Gas turbine engine compressor arrangement
US20140165534A1 (en) * 2007-09-21 2014-06-19 United Technologies Corporation Gas turbine engine compressor arrangement
US20140157756A1 (en) * 2007-09-21 2014-06-12 United Technologies Corporation Gas turbine engine compressor arrangement
US8519555B2 (en) * 2010-11-29 2013-08-27 Pratt & Whitney Canada Corp. Combination low spool generator and ram air turbine generator
FR3004700B1 (fr) * 2013-04-19 2015-04-03 Aircelle Sa Nacelle pour turboreacteur d’aeronef a levre avant etendue
US11131208B2 (en) * 2016-09-01 2021-09-28 Rolls-Royce North American Technologies, Inc. Embedded electric generator in turbine engine
US11230385B2 (en) * 2017-06-08 2022-01-25 General Electric Company Hybrid-electric propulsion system for an aircraft
FR3086643B1 (fr) * 2018-09-28 2021-05-28 Safran Nacelles Nacelle pour aeronef et entree d'air associee
FR3087823B1 (fr) * 2018-10-26 2020-11-13 Safran Aircraft Engines Module de soufflante equipe d'une machine electrique pour une turbomachine d'aeronef
US11846196B2 (en) * 2020-02-21 2023-12-19 Rtx Corporation After-fan system with electrical motor for gas turbine engines

Also Published As

Publication number Publication date
EP3957829A1 (en) 2022-02-23
US20220055759A1 (en) 2022-02-24
CN114076029A (zh) 2022-02-22

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