ES2002016A6 - Un sincronizador de fase perfeccionado para helices de aviones - Google Patents

Un sincronizador de fase perfeccionado para helices de aviones

Info

Publication number
ES2002016A6
ES2002016A6 ES8602286A ES8602286A ES2002016A6 ES 2002016 A6 ES2002016 A6 ES 2002016A6 ES 8602286 A ES8602286 A ES 8602286A ES 8602286 A ES8602286 A ES 8602286A ES 2002016 A6 ES2002016 A6 ES 2002016A6
Authority
ES
Spain
Prior art keywords
providing
control
propeller
signal
engine power
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.)
Expired
Application number
ES8602286A
Other languages
English (en)
Inventor
Kermit Ivan Harner
Roy Wilfred Schneider
Mark Linn Harris
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.)
Raytheon Technologies Corp
Original Assignee
United Technologies 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 United Technologies Corp filed Critical United Technologies Corp
Publication of ES2002016A6 publication Critical patent/ES2002016A6/es
Expired legal-status Critical Current

Links

Classifications

    • 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
    • B64C11/50—Phase synchronisation between multiple propellers
    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02P—CONTROL OR REGULATION OF ELECTRIC MOTORS, ELECTRIC GENERATORS OR DYNAMO-ELECTRIC CONVERTERS; CONTROLLING TRANSFORMERS, REACTORS OR CHOKE COILS
    • H02P5/00—Arrangements specially adapted for regulating or controlling the speed or torque of two or more electric motors
    • H02P5/46—Arrangements specially adapted for regulating or controlling the speed or torque of two or more electric motors for speed regulation of two or more dynamo-electric motors in relation to one another
    • H02P5/52—Arrangements specially adapted for regulating or controlling the speed or torque of two or more electric motors for speed regulation of two or more dynamo-electric motors in relation to one another additionally providing control of relative angular displacement
    • H02P5/56—Speed and position comparison between the motors by electrical means
    • 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)
  • Power Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Control Of Vehicle Engines Or Engines For Specific Uses (AREA)
  • Electrical Control Of Air Or Fuel Supplied To Internal-Combustion Engine (AREA)
  • Control Of Velocity Or Acceleration (AREA)
  • Motor Power Transmission Devices (AREA)
  • Shafts, Cranks, Connecting Bars, And Related Bearings (AREA)

Abstract

UN SINCRONIZADOR DE FASE (10) PERFECCIONADO PARA HELICE ESCLAVA, EL CUAL INCLUYE UN PRIMER CONTROL (14) QUE RESPONDE A UNA SEÑAL DE DIFERENCIA DE FASE (28) Y UNA SEÑAL DE REFERENCIA DE DIFERENCIA DE FASE (26) PARA PROPORCIONAR UNA SEÑAL DE ERROR DE FASE (112) Y PARA PROPORCIONAR UNA SEÑAL DERIVADA DE REFERENCIA DE LA VELOCIDAD DE LA HELICE (40) PARA UN MANDO DE GOBIERNO DE VELOCIDAD (46), Y TAMBIEN INCLUYE, DE ACUERDO CON EL PRESENTE INVENTO, UN SEGUNDO CONTROL (12) QUE RESPONDE A LA SEÑAL DE ERROR DE FASE (112) A FIN DE PROPORCIONAR UNA SEÑAL DERIVADA DE REFERENCIA DE LA POTENCIA DEL MOTOR (80) PARA UN CONTROL DE LA POTENCIA DEL MOTOR, A FIN DE PROPORCIONAR UNA CANTIDAD MUY LIMITADA DE CONTROL PARA EL AJUSTE DE LA VELOCIDAD DE LA HELICE DENTRO DE LA BANDA MUERTA DEL MANDO DE GOBIERNO DE LA VELOCIDAD DE LA HELICE, MIENTRAS QUE EL MISMO TIEMPO MANTIENE LA POTENCIA DEL MOTOR SUSTANCIALMENTE AL NIVEL DE POTENCIA DE GOBIERNO.
ES8602286A 1985-09-30 1986-09-29 Un sincronizador de fase perfeccionado para helices de aviones Expired ES2002016A6 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US06/781,585 US4653981A (en) 1985-09-30 1985-09-30 Propeller synchrophaser

Publications (1)

Publication Number Publication Date
ES2002016A6 true ES2002016A6 (es) 1988-07-01

Family

ID=25123248

Family Applications (1)

Application Number Title Priority Date Filing Date
ES8602286A Expired ES2002016A6 (es) 1985-09-30 1986-09-29 Un sincronizador de fase perfeccionado para helices de aviones

Country Status (8)

Country Link
US (1) US4653981A (es)
EP (1) EP0221002B1 (es)
JP (1) JPS6280197A (es)
CN (1) CN1011215B (es)
BR (1) BR8604680A (es)
CA (1) CA1284682C (es)
DE (1) DE3687300T2 (es)
ES (1) ES2002016A6 (es)

Families Citing this family (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4928241A (en) * 1985-05-28 1990-05-22 General Electric Company Aircraft propeller control
US5170365A (en) * 1985-12-12 1992-12-08 General Electric Company Propeller speed and phase sensor
US4772180A (en) * 1986-08-29 1988-09-20 General Electric Company Aircraft thrust control
US4772179A (en) * 1986-08-29 1988-09-20 General Electric Company Aircraft thrust control
GB2211635B (en) * 1987-10-28 1992-02-05 Fokker Aircraft Control system for synchrophasing aircraft propellers
US4934825A (en) * 1987-12-22 1990-06-19 United Technologies Corporation Propeller phase control apparatus
US5058376A (en) * 1988-11-21 1991-10-22 General Electric Company Turbofan synchrophaser
US5136841A (en) * 1989-02-27 1992-08-11 Zimmerman Ward H Aircraft propulsion control system
US5044155A (en) * 1989-02-27 1991-09-03 The Boeing Company Aircraft propulsion control system
US5027277A (en) * 1989-04-11 1991-06-25 United Technologies Corporation Method for synchrophaser measurement and synchrophaser control
US5042965A (en) * 1989-06-16 1991-08-27 United Technologies Corporation Propeller synchrophaser control with trajectory logic
US5551649A (en) * 1989-10-20 1996-09-03 Fokker Aircraft B.V. Propeller blade position controller
US5093791A (en) * 1990-06-01 1992-03-03 United Technologies Corporation Variable gain synchrophasing
GB9017598D0 (en) * 1990-08-10 1990-09-26 Dowty Aerospace Gloucester A propeller control system
US5291410A (en) * 1991-09-19 1994-03-01 Allied-Signal Inc. Circuitry for synchronizing the speed of a plurality of engines by sequentially averaging phase difference with a reference phase representing a desired speed
US5715162A (en) * 1992-10-13 1998-02-03 United Technologies Corporation Correlative filter for a synchrophaser
US5453943A (en) * 1994-02-18 1995-09-26 United Technologies Corporation Adaptive synchrophaser for reducing aircraft cabin noise and vibration
US5740029A (en) * 1996-02-21 1998-04-14 Westinghouse Air Brake Company Software algorithm providing dynamic configuration of dead band control criteria within a micro based real time process control environment
US8651811B2 (en) * 2005-11-16 2014-02-18 Hamilton Sundstrand Control logic for a propeller system
FR3071816B1 (fr) * 2017-09-29 2020-05-29 Airbus Helicopters Drone de type multirotor comportant une unite de gestion de la vitesse de rotation de chacun des rotors et procede de commande d'un tel drone

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2877854A (en) * 1955-12-27 1959-03-17 United Aircraft Corp Synchrophaser resetting mechanism for variable pitch aircraft propellers
US2878426A (en) * 1955-12-27 1959-03-17 United Aircraft Corp Signal limiting means for synchronizer
US2887621A (en) * 1956-01-31 1959-05-19 Curtiss Wright Corp Speed and phase synchronizers
US2986223A (en) * 1956-05-10 1961-05-30 Cook Electric Co Follow-up system
US2979135A (en) * 1956-06-01 1961-04-11 Cook Electric Co Phase synchronizing system
US3007529A (en) * 1956-12-24 1961-11-07 Gen Motors Corp Synchronizing and synchrophasing system for propellers
US2847617A (en) * 1957-03-28 1958-08-12 Curtiss Wright Corp Phase synchronizing system
US3079531A (en) * 1958-01-30 1963-02-26 Havilland Aircraft Company De Aircraft propeller engine speed controls
US3479822A (en) * 1968-03-27 1969-11-25 Us Navy Engine synchronizer
US3689175A (en) * 1970-08-11 1972-09-05 Piqua Aircraft Co Inc Apparatus for controlling the speed and phase of engines
US4245955A (en) * 1978-12-14 1981-01-20 The Cessna Aircraft Company Phase and speed control system
GB2101363A (en) * 1981-05-15 1983-01-12 British Aerospace Engine speed control

Also Published As

Publication number Publication date
BR8604680A (pt) 1987-06-16
CN86106717A (zh) 1987-04-01
JPS6280197A (ja) 1987-04-13
DE3687300D1 (de) 1993-01-28
EP0221002B1 (en) 1992-12-16
CN1011215B (zh) 1991-01-16
US4653981A (en) 1987-03-31
DE3687300T2 (de) 1993-04-15
CA1284682C (en) 1991-06-04
EP0221002A3 (en) 1988-03-16
EP0221002A2 (en) 1987-05-06

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Legal Events

Date Code Title Description
SA6 Expiration date (snapshot 920101)

Free format text: 2006-09-29