IL72461A - Increases helicopter load factor - Google Patents

Increases helicopter load factor

Info

Publication number
IL72461A
IL72461A IL7246184A IL7246184A IL72461A IL 72461 A IL72461 A IL 72461A IL 7246184 A IL7246184 A IL 7246184A IL 7246184 A IL7246184 A IL 7246184A IL 72461 A IL72461 A IL 72461A
Authority
IL
Israel
Prior art keywords
rotor
rotor speed
signal
load
load factor
Prior art date
Application number
IL7246184A
Other languages
English (en)
Hebrew (he)
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 IL72461A publication Critical patent/IL72461A/en

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)
  • Fuel-Injection Apparatus (AREA)
  • Controls For Constant Speed Travelling (AREA)
  • Control Of The Air-Fuel Ratio Of Carburetors (AREA)
  • Control Of Vehicle Engines Or Engines For Specific Uses (AREA)
IL7246184A 1983-08-01 1984-07-20 Increases helicopter load factor IL72461A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US51933283A 1983-08-01 1983-08-01

Publications (1)

Publication Number Publication Date
IL72461A true IL72461A (en) 1996-10-16

Family

ID=24067852

Family Applications (1)

Application Number Title Priority Date Filing Date
IL7246184A IL72461A (en) 1983-08-01 1984-07-20 Increases helicopter load factor

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
US5314147A (en) * 1991-08-27 1994-05-24 United Technologies Corporation Helicopter engine speed enhancement during heavy rotor load and rapid descent rate maneuvering
US5265825A (en) * 1991-08-27 1993-11-30 United Technologies Corporation Helicopter engine control having yaw input anticipation
US5265826A (en) * 1991-08-27 1993-11-30 United Technologies Corporation Helicopter engine control having lateral cyclic pitch anticipation
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
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

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
DE3428224A1 (de) 1985-02-14
FR2550161A1 (fr) 1985-02-08
DE3428224C2 (de) 2000-02-10
FR2550161B1 (fr) 1988-06-10
JPS6038297A (ja) 1985-02-27
JPH0733159B2 (ja) 1995-04-12
GB2144244A (en) 1985-02-27
CA1246717A (en) 1988-12-13
GB2144244B (en) 1986-11-12
GB8417638D0 (en) 1984-08-15
IT8422117A0 (it) 1984-07-30
IT1174616B (it) 1987-07-01

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Legal Events

Date Code Title Description
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KB Patent renewed
KB Patent renewed
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