ES2537477R1 - Sistema de propulsión de hélice no-carenada contrarrotativo - Google Patents

Sistema de propulsión de hélice no-carenada contrarrotativo Download PDF

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Publication number
ES2537477R1
ES2537477R1 ES201430981A ES201430981A ES2537477R1 ES 2537477 R1 ES2537477 R1 ES 2537477R1 ES 201430981 A ES201430981 A ES 201430981A ES 201430981 A ES201430981 A ES 201430981A ES 2537477 R1 ES2537477 R1 ES 2537477R1
Authority
ES
Spain
Prior art keywords
propulsion
propulsion system
propeller
contrarrotative
carenada
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.)
Granted
Application number
ES201430981A
Other languages
English (en)
Other versions
ES2537477B2 (es
ES2537477A2 (es
Inventor
Sina S. Golshany
David Miles Huntly
Adriana W. Blom
Todd R. Erickson
Paul R. Tretow
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.)
Boeing Co
Original Assignee
Boeing Co
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 Boeing Co filed Critical Boeing Co
Publication of ES2537477A2 publication Critical patent/ES2537477A2/es
Publication of ES2537477R1 publication Critical patent/ES2537477R1/es
Application granted granted Critical
Publication of ES2537477B2 publication Critical patent/ES2537477B2/es
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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C11/00—Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
    • B64C11/46—Arrangements of, or constructional features peculiar to, multiple propellers
    • B64C11/48—Units of two or more coaxial propellers
    • 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
    • B64D35/00—Transmitting power from power plants to propellers or rotors; Arrangements of transmissions
    • 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
    • B64D35/00—Transmitting power from power plants to propellers or rotors; Arrangements of transmissions
    • B64D35/04—Transmitting power from power plants to propellers or rotors; Arrangements of transmissions characterised by the transmission driving a plurality of propellers or rotors
    • B64D35/06—Transmitting power from power plants to propellers or rotors; Arrangements of transmissions characterised by the transmission driving a plurality of propellers or rotors the propellers or rotors being counter-rotating
    • 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
    • B64C—AEROPLANES; HELICOPTERS
    • B64C11/00—Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
    • B64C11/46—Arrangements of, or constructional features peculiar to, multiple propellers
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/04—Helicopters
    • B64C27/08—Helicopters with two or more rotors
    • B64C27/10—Helicopters with two or more rotors arranged coaxially
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/04—Helicopters
    • B64C27/12—Rotor drives
    • 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
    • B64D2027/005—Aircraft with an unducted turbofan comprising contra-rotating rotors, e.g. contra-rotating open rotors [CROR]
    • 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
    • B64D35/00—Transmitting power from power plants to propellers or rotors; Arrangements of transmissions
    • B64D35/04—Transmitting power from power plants to propellers or rotors; Arrangements of transmissions characterised by the transmission driving a plurality of propellers or rotors
    • 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
    • F02C3/06—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor the compressor comprising only axial stages
    • F02C3/067—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor the compressor comprising only axial stages having counter-rotating rotors
    • 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
    • F02C3/36—Open cycles
    • 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
    • F05D2220/325—Application in turbines in gas turbines to drive unshrouded, high solidity propeller
    • 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
    • F16D—COUPLINGS FOR TRANSMITTING ROTATION; CLUTCHES; BRAKES
    • F16D33/00—Rotary fluid couplings or clutches of the hydrokinetic type
    • F16D33/06—Rotary fluid couplings or clutches of the hydrokinetic type controlled by changing the amount of liquid in the working circuit
    • F16D33/16—Rotary fluid couplings or clutches of the hydrokinetic type controlled by changing the amount of liquid in the working circuit by means arranged externally of the coupling or clutch
    • 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)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Hydraulic Clutches, Magnetic Clutches, Fluid Clutches, And Fluid Joints (AREA)
  • Motor Power Transmission Devices (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Arrangement And Driving Of Transmission Devices (AREA)
  • Control Of Positive-Displacement Air Blowers (AREA)
  • Ultra Sonic Daignosis Equipment (AREA)
  • Tires In General (AREA)
  • Transmission Devices (AREA)

Abstract

La presente invención divulga un sistema de propulsión de hélice no-carenada contrarrotativo con objeto, entre otros, de reducir los niveles efectivos de ruido generados por los propulsores contrarrotativos. El sistema de propulsión comprende un motor, un conjunto de accionamiento acoplado al motor, un primer eje de accionamiento rotativo en un primer sentido alrededor de un primer eje, una primera hélice acoplada al primer eje de accionamiento para girar en el primer sentido, y un conjunto de embrague para desembragar selectivamente la primera hélice del primer eje de accionamiento.
ES201430981A 2013-09-19 2014-06-30 Sistema de propulsión de hélice no-carenada contrarrotativo Active ES2537477B2 (es)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US14/032,163 US9835093B2 (en) 2013-09-19 2013-09-19 Contra-rotating open fan propulsion system
US14/032163 2013-09-19

Publications (3)

Publication Number Publication Date
ES2537477A2 ES2537477A2 (es) 2015-06-08
ES2537477R1 true ES2537477R1 (es) 2016-02-05
ES2537477B2 ES2537477B2 (es) 2016-11-14

Family

ID=51869462

Family Applications (1)

Application Number Title Priority Date Filing Date
ES201430981A Active ES2537477B2 (es) 2013-09-19 2014-06-30 Sistema de propulsión de hélice no-carenada contrarrotativo

Country Status (4)

Country Link
US (1) US9835093B2 (es)
CN (1) CN104443400B (es)
ES (1) ES2537477B2 (es)
GB (1) GB2520383B (es)

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US9951763B2 (en) * 2014-05-09 2018-04-24 Westinghouse Air Brake Technologies Corporation Compressor cooled by a temperature controlled fan
WO2016053408A1 (en) 2014-10-01 2016-04-07 Sikorsky Aircraft Corporation Acoustic signature variation of aircraft utilizing a clutch
US10018058B2 (en) 2015-07-14 2018-07-10 The Boeing Company Laterally reinforced variable pitch rotor
CN105570342A (zh) * 2016-02-18 2016-05-11 太仓钰丰机械工程有限公司 一种带有双螺旋叶片的硅油风扇离合器
US10526070B2 (en) 2016-03-23 2020-01-07 Amazon Technologies, Inc. Aerial vehicle propulsion mechanism with coaxially aligned propellers
US10583914B2 (en) 2016-03-23 2020-03-10 Amazon Technologies, Inc. Telescoping propeller blades for aerial vehicles
US10399666B2 (en) * 2016-03-23 2019-09-03 Amazon Technologies, Inc. Aerial vehicle propulsion mechanism with coaxially aligned and independently rotatable propellers
US10723440B2 (en) 2016-03-23 2020-07-28 Amazon Technologies, Inc. Aerial vehicle with different propeller blade configurations
US11305874B2 (en) 2016-03-23 2022-04-19 Amazon Technologies, Inc. Aerial vehicle adaptable propeller blades
US10526069B1 (en) * 2016-09-08 2020-01-07 Northrop Grumman Systems Corporation Collapsible large diameter propeller for quiet aircraft
US10737801B2 (en) * 2016-10-31 2020-08-11 Rolls-Royce Corporation Fan module with rotatable vane ring power system
US10618667B2 (en) 2016-10-31 2020-04-14 Rolls-Royce Corporation Fan module with adjustable pitch blades and power system
US20180118364A1 (en) * 2016-11-03 2018-05-03 The Boeing Company System and method for augmenting a primary powerplant
US10465606B2 (en) 2017-02-08 2019-11-05 General Electric Company Counter rotating turbine with reversing reduction gearbox
US10801442B2 (en) 2017-02-08 2020-10-13 General Electric Company Counter rotating turbine with reversing reduction gear assembly
US10823114B2 (en) 2017-02-08 2020-11-03 General Electric Company Counter rotating turbine with reversing reduction gearbox
US10683900B2 (en) 2017-03-29 2020-06-16 Pratt & Whitney Canada Corp. Clutch device for gas turbine engines
US10663036B2 (en) 2017-06-13 2020-05-26 General Electric Company Gas turbine engine with rotating reversing compound gearbox
US10774008B2 (en) 2017-09-21 2020-09-15 General Electric Company Ceramic matrix composite articles
US10329201B2 (en) 2017-09-21 2019-06-25 General Electric Company Ceramic matrix composite articles formation method
US10696391B2 (en) 2017-11-16 2020-06-30 Textron Innovations Inc. Extended range quad tiltrotor aircraft
US10752352B2 (en) * 2017-12-07 2020-08-25 Textron Innovations Inc. Dual rotor propulsion systems for tiltrotor aircraft
US10989114B2 (en) 2018-03-07 2021-04-27 The Boeing Company Systems and methods for cooling bleed air from an aircraft engine
US20190283864A1 (en) * 2018-03-16 2019-09-19 Hamilton Sundstrand Corporation Counter-rotating propeller system with capability to stop rotation of one row
US11712637B1 (en) 2018-03-23 2023-08-01 Steven M. Hoffberg Steerable disk or ball
US20200017229A1 (en) * 2018-07-13 2020-01-16 Bell Helicopter Textron Inc. Fan clutch for convertible engine
US10738694B1 (en) 2018-08-23 2020-08-11 United Technologies Corporation Turbofan with motorized rotating inlet guide vane
FR3087849B1 (fr) * 2018-10-26 2020-11-20 Safran Aircraft Engines Turbomachine a double helices non carenees
US11118535B2 (en) 2019-03-05 2021-09-14 General Electric Company Reversing gear assembly for a turbo machine
US11428160B2 (en) 2020-12-31 2022-08-30 General Electric Company Gas turbine engine with interdigitated turbine and gear assembly
US11396376B1 (en) 2021-01-04 2022-07-26 Cameron Carnegie Y-shaped airliner and associated methods
CN113217226B (zh) * 2021-06-02 2022-08-02 中国航发湖南动力机械研究所 桨扇涡轮一体式发动机
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Also Published As

Publication number Publication date
GB2520383A (en) 2015-05-20
GB2520383B (en) 2016-02-10
ES2537477B2 (es) 2016-11-14
US20150078888A1 (en) 2015-03-19
ES2537477A2 (es) 2015-06-08
CN104443400B (zh) 2018-09-04
GB201416083D0 (en) 2014-10-29
US9835093B2 (en) 2017-12-05
CN104443400A (zh) 2015-03-25

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