PL3354876T3 - Architektura silnika turbospalinowego z układem sprężarki dzielonej - Google Patents

Architektura silnika turbospalinowego z układem sprężarki dzielonej

Info

Publication number
PL3354876T3
PL3354876T3 PL18154161T PL18154161T PL3354876T3 PL 3354876 T3 PL3354876 T3 PL 3354876T3 PL 18154161 T PL18154161 T PL 18154161T PL 18154161 T PL18154161 T PL 18154161T PL 3354876 T3 PL3354876 T3 PL 3354876T3
Authority
PL
Poland
Prior art keywords
gas turbine
turbine engine
compressor system
engine architecture
split compressor
Prior art date
Application number
PL18154161T
Other languages
English (en)
Inventor
Ghislain Plante
Patrick Valois
Jean Dubreuil
Daniel Blais
Original Assignee
Pratt & Whitney Canada Corp.
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 Pratt & Whitney Canada Corp. filed Critical Pratt & Whitney Canada Corp.
Publication of PL3354876T3 publication Critical patent/PL3354876T3/pl

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C3/00Gas-turbine plants characterised by the use of combustion products as the working fluid
    • F02C3/04Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor
    • F02C3/107Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor with two or more rotors connected by power transmission
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/02Aircraft characterised by the type or position of power plants
    • B64D27/10Aircraft characterised by the type or position of power plants of gas-turbine type 
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00Features, 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
    • F02C7/36Power transmission arrangements between the different shafts of the gas turbine plant, or between the gas-turbine plant and the power user
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2220/00Application
    • F05D2220/30Application in turbines
    • F05D2220/32Application in turbines in gas turbines
    • F05D2220/325Application in turbines in gas turbines to drive unshrouded, high solidity propeller
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2250/00Geometry
    • F05D2250/30Arrangement of components
    • F05D2250/31Arrangement of components according to the direction of their main axis or their axis of rotation
    • F05D2250/312Arrangement of components according to the direction of their main axis or their axis of rotation the axes being parallel to each other
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00Function
    • F05D2260/40Transmission of power
    • F05D2260/403Transmission of power through the shape of the drive components
    • F05D2260/4031Transmission of power through the shape of the drive components as in toothed gearing
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00Function
    • F05D2260/40Transmission of power
    • F05D2260/403Transmission of power through the shape of the drive components
    • F05D2260/4031Transmission of power through the shape of the drive components as in toothed gearing
    • F05D2260/40311Transmission of power through the shape of the drive components as in toothed gearing of the epicyclical, planetary or differential type
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/60Efficient 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)
  • Structures Of Non-Positive Displacement Pumps (AREA)
PL18154161T 2017-01-30 2018-01-30 Architektura silnika turbospalinowego z układem sprężarki dzielonej PL3354876T3 (pl)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US15/419,160 US20180216525A1 (en) 2017-01-30 2017-01-30 Gas turbine engine architecture with split compressor system
EP18154161.6A EP3354876B1 (en) 2017-01-30 2018-01-30 Gas turbine engine architecture with split compressor system

Publications (1)

Publication Number Publication Date
PL3354876T3 true PL3354876T3 (pl) 2020-09-21

Family

ID=61132037

Family Applications (1)

Application Number Title Priority Date Filing Date
PL18154161T PL3354876T3 (pl) 2017-01-30 2018-01-30 Architektura silnika turbospalinowego z układem sprężarki dzielonej

Country Status (4)

Country Link
US (1) US20180216525A1 (pl)
EP (1) EP3354876B1 (pl)
CA (1) CA2991839A1 (pl)
PL (1) PL3354876T3 (pl)

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US11415063B2 (en) 2016-09-15 2022-08-16 Pratt & Whitney Canada Corp. Reverse-flow gas turbine engine
US10883424B2 (en) 2016-07-19 2021-01-05 Pratt & Whitney Canada Corp. Multi-spool gas turbine engine architecture
US10465611B2 (en) 2016-09-15 2019-11-05 Pratt & Whitney Canada Corp. Reverse flow multi-spool gas turbine engine with aft-end accessory gearbox drivingly connected to both high pressure spool and low pressure spool
US11035293B2 (en) 2016-09-15 2021-06-15 Pratt & Whitney Canada Corp. Reverse flow gas turbine engine with offset RGB
US10815899B2 (en) 2016-11-15 2020-10-27 Pratt & Whitney Canada Corp. Gas turbine engine accessories arrangement
US10808624B2 (en) 2017-02-09 2020-10-20 Pratt & Whitney Canada Corp. Turbine rotor with low over-speed requirements
US10746188B2 (en) 2017-03-14 2020-08-18 Pratt & Whitney Canada Corp. Inter-shaft bearing connected to a compressor boost system
EP3418195B1 (en) * 2017-06-21 2021-10-20 General Electric Company Polska sp. z o.o. Exhaust stub for an aircraft engine assembly
EP3653859B1 (en) 2018-08-08 2024-02-07 Pratt & Whitney Canada Corp. Multi-engine system and method
US11629665B2 (en) 2018-09-11 2023-04-18 Pratt & Whitney Canada Corp. Gas turbine engine and method of creating classes of same
GB201913389D0 (en) * 2019-09-03 2019-10-30 Lewis Stephen Desmond Reduced weight gas turbine
US11668245B2 (en) * 2020-01-28 2023-06-06 Pratt & Whitney Canada Corp. Gas turbine engine with clutch system between low-pressure compressor and low-pressure turbine
US12397924B2 (en) * 2024-02-02 2025-08-26 Rtx Corporation Open rotor aircraft propulsion system with bypass flowpath
US12221932B1 (en) * 2024-04-30 2025-02-11 Saudi Arabian Oil Company Integrated gas turbine energy recovery system for efficiency enhancement

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US2929207A (en) * 1955-08-08 1960-03-22 Adolphe C Peterson Axial flow gas turbine
GB1102591A (en) * 1964-05-22 1968-02-07 Auto Transmissions Ltd Power transmission system for a gas turbine engine
US3488947A (en) * 1967-11-24 1970-01-13 Boeing Co Torque transfer apparatus for a free shaft gas turbine engine
DE2006138A1 (de) * 1970-02-11 1971-08-19 Daimler Benz Ag Gasturbine zum Antrieb von Kraftfahr
US4055949A (en) * 1973-05-08 1977-11-01 Societe Nationale D'etude Et De Construction De Moteurs D'aviation Multiflow gas turbine power plant
US6960060B2 (en) * 2003-11-20 2005-11-01 General Electric Company Dual coolant turbine blade
US7055303B2 (en) * 2003-12-22 2006-06-06 Pratt & Whitney Canada Corp. Gas turbine engine architecture
US7691028B2 (en) * 2006-05-02 2010-04-06 Conocophillips Company Mechanical soft-start system for rotating industrial equipment
US8169100B2 (en) * 2008-01-30 2012-05-01 Pratt & Whitney Canada Corp. Torque transmission for an aircraft engine
US8146370B2 (en) * 2008-05-21 2012-04-03 Honeywell International Inc. Turbine drive system with lock-up clutch and method
US8176725B2 (en) * 2009-09-09 2012-05-15 United Technologies Corporation Reversed-flow core for a turbofan with a fan drive gear system
US20130031912A1 (en) * 2011-08-01 2013-02-07 Hamilton Sundstrand Corporation Gas turbine start architecture
US8935912B2 (en) * 2011-12-09 2015-01-20 United Technologies Corporation Gas turbine engine with variable overall pressure ratio
US8459038B1 (en) * 2012-02-09 2013-06-11 Williams International Co., L.L.C. Two-spool turboshaft engine control system and method
US9239004B2 (en) * 2012-03-27 2016-01-19 United Technologies Corporation Reverse core gear turbofan
DE102013213518A1 (de) * 2013-07-10 2015-01-15 Rolls-Royce Deutschland Ltd & Co Kg Turbofan-Triebwerk
GB201600180D0 (en) * 2016-01-06 2016-02-17 Rolls Royce Plc Gas turbine engine
US9745860B1 (en) * 2016-11-02 2017-08-29 Jay HASKIN Power transmission system for turbine or compressor having counter-rotating blades

Also Published As

Publication number Publication date
EP3354876A1 (en) 2018-08-01
CA2991839A1 (en) 2018-07-30
EP3354876B1 (en) 2020-04-01
US20180216525A1 (en) 2018-08-02

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