CA1246717A - Rotorcraft load factor enhancer - Google Patents

Rotorcraft load factor enhancer

Info

Publication number
CA1246717A
CA1246717A CA000458431A CA458431A CA1246717A CA 1246717 A CA1246717 A CA 1246717A CA 000458431 A CA000458431 A CA 000458431A CA 458431 A CA458431 A CA 458431A CA 1246717 A CA1246717 A CA 1246717A
Authority
CA
Canada
Prior art keywords
rotor speed
signal
load factor
pitch rate
rotor
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
CA000458431A
Other languages
English (en)
French (fr)
Inventor
James J. Howlett
Dean E. Cooper
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
Application granted granted Critical
Publication of CA1246717A publication Critical patent/CA1246717A/en
Expired legal-status Critical Current

Links

Classifications

    • GPHYSICS
    • G05CONTROLLING; REGULATING
    • G05DSYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
    • G05D1/08Control of attitude, i.e. control of roll, pitch, or yaw
    • G05D1/0808Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft
    • G05D1/0858Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft specially adapted for vertical take-off of aircraft
    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02PCONTROL OR REGULATION OF ELECTRIC MOTORS, ELECTRIC GENERATORS OR DYNAMO-ELECTRIC CONVERTERS; CONTROLLING TRANSFORMERS, REACTORS OR CHOKE COILS
    • H02P23/00Arrangements or methods for the control of AC motors characterised by a control method other than vector control
    • H02P23/16Controlling the angular speed of one shaft

Landscapes

  • Engineering & Computer Science (AREA)
  • Power Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Automation & Control Theory (AREA)
  • Control Of Turbines (AREA)
  • Control Of The Air-Fuel Ratio Of Carburetors (AREA)
  • Fuel-Injection Apparatus (AREA)
  • Controls For Constant Speed Travelling (AREA)
  • Control Of Vehicle Engines Or Engines For Specific Uses (AREA)
CA000458431A 1983-08-01 1984-07-09 Rotorcraft load factor enhancer Expired CA1246717A (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US51933283A 1983-08-01 1983-08-01
US519,332 1983-08-01

Publications (1)

Publication Number Publication Date
CA1246717A true CA1246717A (en) 1988-12-13

Family

ID=24067852

Family Applications (1)

Application Number Title Priority Date Filing Date
CA000458431A Expired CA1246717A (en) 1983-08-01 1984-07-09 Rotorcraft load factor enhancer

Country Status (7)

Country Link
JP (1) JPH0733159B2 (de)
CA (1) CA1246717A (de)
DE (1) DE3428224C2 (de)
FR (1) FR2550161B1 (de)
GB (1) GB2144244B (de)
IL (1) IL72461A (de)
IT (1) IT1174616B (de)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB8807676D0 (en) * 1988-03-31 1988-05-05 Westland Helicopters Helicopter control systems
US4998202A (en) * 1989-05-19 1991-03-05 United Technologies Corporation Helicopter, high rotor load speed enhancement
US5265825A (en) * 1991-08-27 1993-11-30 United Technologies Corporation Helicopter engine control having yaw input anticipation
US5314147A (en) * 1991-08-27 1994-05-24 United Technologies Corporation Helicopter engine speed enhancement during heavy rotor load and rapid descent rate maneuvering
US5265826A (en) * 1991-08-27 1993-11-30 United Technologies Corporation Helicopter engine control having lateral cyclic pitch anticipation
FR3000465B1 (fr) 2012-12-27 2015-02-13 Eurocopter France Procede d'entrainement en rotation d'un rotor principal de giravion, selon une consigne de vitesse de rotation a valeur variable
FR3000466B1 (fr) 2012-12-27 2015-02-13 Eurocopter France Procede d'entrainement en rotation d'un rotor de giravion, par anticipation des besoins en couple entre deux consignes de vitesse de rotation du rotor

Family Cites Families (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2645293A (en) * 1946-09-14 1953-07-14 Gen Electric Apparatus for regulating propulsion power plants
DE952404C (de) * 1953-05-18 1956-11-15 Bendix Aviat Corp Selbsttaetige Steuerungsvorruchtung fuer Flugzeuge
US3174551A (en) * 1963-02-19 1965-03-23 United Aircraft Corp Power management control for helicopters
US3200886A (en) * 1964-05-28 1965-08-17 Joseph L Magri Droop compensated fuel control system
GB1120327A (en) * 1967-02-24 1968-07-17 Ltv Aerospace Corp Autothrottle
GB1244160A (en) * 1967-11-17 1971-08-25 Dowty Rotol Ltd Engine, propeller and rotor installations
US3930366A (en) * 1974-07-17 1976-01-06 General Motors Corporation Helicopter power plant control
JPS5112012A (ja) * 1974-07-18 1976-01-30 Mitsubishi Heavy Ind Ltd Gasutaabinnenshokino kaenkanshisochi
US4217754A (en) * 1977-01-22 1980-08-19 Bodenseewerk Geratetechnik Gmbh Apparatus for controlling the rotary speed in turbo-jet engines for aircraft
US4127245A (en) * 1977-04-27 1978-11-28 United Technologies Corporation Helicopter pitch rate feedback bias for pitch axis maneuvering stability and load feel
GB2052805B (en) * 1979-06-29 1983-03-09 Smiths Industries Ltd Gas-turbine engine control
ZA814691B (en) * 1980-08-08 1983-02-23 Ass Eng Ltd Automatic speed control systems
US4442667A (en) * 1981-01-14 1984-04-17 Aviation Electric Ltd. Acceleration limit reset
US4423593A (en) * 1982-04-16 1984-01-03 Chandler Evans Inc. Fuel control for controlling helicopter rotor/turbine acceleration

Also Published As

Publication number Publication date
FR2550161B1 (fr) 1988-06-10
FR2550161A1 (fr) 1985-02-08
IT8422117A0 (it) 1984-07-30
GB8417638D0 (en) 1984-08-15
JPH0733159B2 (ja) 1995-04-12
JPS6038297A (ja) 1985-02-27
DE3428224A1 (de) 1985-02-14
IL72461A (en) 1996-10-16
IT1174616B (it) 1987-07-01
GB2144244A (en) 1985-02-27
GB2144244B (en) 1986-11-12
DE3428224C2 (de) 2000-02-10

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Legal Events

Date Code Title Description
MKEX Expiry