GB8417638D0 - Rotorcraft load factor enhancer - Google Patents

Rotorcraft load factor enhancer

Info

Publication number
GB8417638D0
GB8417638D0 GB848417638A GB8417638A GB8417638D0 GB 8417638 D0 GB8417638 D0 GB 8417638D0 GB 848417638 A GB848417638 A GB 848417638A GB 8417638 A GB8417638 A GB 8417638A GB 8417638 D0 GB8417638 D0 GB 8417638D0
Authority
GB
United Kingdom
Prior art keywords
rotorcraft
load factor
factor enhancer
enhancer
load
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
GB848417638A
Other versions
GB2144244B (en
GB2144244A (en
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 GB8417638D0 publication Critical patent/GB8417638D0/en
Publication of GB2144244A publication Critical patent/GB2144244A/en
Application granted granted Critical
Publication of GB2144244B publication Critical patent/GB2144244B/en
Expired legal-status Critical Current

Links

Classifications

    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
    • G05D1/08—Control of attitude, i.e. control of roll, pitch, or yaw
    • G05D1/0808—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft
    • G05D1/0858—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft specially adapted for vertical take-off of aircraft
    • 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
    • H02P23/00—Arrangements or methods for the control of AC motors characterised by a control method other than vector control
    • H02P23/16—Controlling the angular speed of one shaft

Landscapes

  • Engineering & Computer Science (AREA)
  • General Physics & Mathematics (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Physics & Mathematics (AREA)
  • Power Engineering (AREA)
  • Automation & Control Theory (AREA)
  • Control Of Turbines (AREA)
  • Control Of Vehicle Engines Or Engines For Specific Uses (AREA)
  • Controls For Constant Speed Travelling (AREA)
  • Control Of The Air-Fuel Ratio Of Carburetors (AREA)
  • Fuel-Injection Apparatus (AREA)
GB08417638A 1983-08-01 1984-07-11 Rotorcraft load factor enhancer Expired GB2144244B (en)

Applications Claiming Priority (1)

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

Publications (3)

Publication Number Publication Date
GB8417638D0 true GB8417638D0 (en) 1984-08-15
GB2144244A GB2144244A (en) 1985-02-27
GB2144244B GB2144244B (en) 1986-11-12

Family

ID=24067852

Family Applications (1)

Application Number Title Priority Date Filing Date
GB08417638A Expired GB2144244B (en) 1983-08-01 1984-07-11 Rotorcraft load factor enhancer

Country Status (7)

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

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
US5265826A (en) * 1991-08-27 1993-11-30 United Technologies Corporation Helicopter engine control having lateral cyclic pitch 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
US5265825A (en) * 1991-08-27 1993-11-30 United Technologies Corporation Helicopter engine control having yaw input anticipation
FR3000466B1 (en) 2012-12-27 2015-02-13 Eurocopter France METHOD FOR ROTATING A ROTOR OF A ROTOR BY FORECKING ANTICIPATION OF TORQUE REQUIREMENTS BETWEEN TWO ROTATOR ROTATION SPEED INSTRUCTIONS
FR3000465B1 (en) 2012-12-27 2015-02-13 Eurocopter France METHOD FOR ROTATING A MAIN ROTOR OF ROTOR OF ROTOR, ACCORDING TO A VARIABLE VALUE ROTATION SPEED SET

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 (en) * 1953-05-18 1956-11-15 Bendix Aviat Corp Automatic control equipment for aircraft
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 (en) * 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 (en) 1985-02-14
DE3428224C2 (en) 2000-02-10
JPH0733159B2 (en) 1995-04-12
FR2550161B1 (en) 1988-06-10
GB2144244B (en) 1986-11-12
IT8422117A0 (en) 1984-07-30
JPS6038297A (en) 1985-02-27
FR2550161A1 (en) 1985-02-08
IL72461A (en) 1996-10-16
CA1246717A (en) 1988-12-13
GB2144244A (en) 1985-02-27
IT1174616B (en) 1987-07-01

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Legal Events

Date Code Title Description
PE20 Patent expired after termination of 20 years

Effective date: 20040710