DE69900471D1 - Integriertes feuer- und flugsteuerungssystem mit automatischer motordrehmomentbeschränkung - Google Patents

Integriertes feuer- und flugsteuerungssystem mit automatischer motordrehmomentbeschränkung

Info

Publication number
DE69900471D1
DE69900471D1 DE69900471T DE69900471T DE69900471D1 DE 69900471 D1 DE69900471 D1 DE 69900471D1 DE 69900471 T DE69900471 T DE 69900471T DE 69900471 T DE69900471 T DE 69900471T DE 69900471 D1 DE69900471 D1 DE 69900471D1
Authority
DE
Germany
Prior art keywords
control system
engine torque
flight control
automatic engine
torque limitation
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 - Lifetime
Application number
DE69900471T
Other languages
English (en)
Other versions
DE69900471T2 (de
Inventor
J Gold
Fogler, Jr
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.)
Sikorsky Aircraft Corp
Original Assignee
Sikorsky Aircraft 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 Sikorsky Aircraft Corp filed Critical Sikorsky Aircraft Corp
Publication of DE69900471D1 publication Critical patent/DE69900471D1/de
Application granted granted Critical
Publication of DE69900471T2 publication Critical patent/DE69900471T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime 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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/04—Helicopters

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Automation & Control Theory (AREA)
  • Feedback Control In General (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
DE69900471T 1998-03-31 1999-03-09 Integriertes feuer- und flugsteuerungssystem mit automatischer motordrehmomentbeschränkung Expired - Lifetime DE69900471T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US09/052,628 US6012676A (en) 1998-03-31 1998-03-31 Integrated fire and flight control system with automatic engine torque limiting
PCT/US1999/005020 WO1999050729A1 (en) 1998-03-31 1999-03-09 Integrated fire and flight control system with automatic engine torque limiting

Publications (2)

Publication Number Publication Date
DE69900471D1 true DE69900471D1 (de) 2001-12-20
DE69900471T2 DE69900471T2 (de) 2002-08-22

Family

ID=21978851

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69900471T Expired - Lifetime DE69900471T2 (de) 1998-03-31 1999-03-09 Integriertes feuer- und flugsteuerungssystem mit automatischer motordrehmomentbeschränkung

Country Status (6)

Country Link
US (1) US6012676A (de)
EP (1) EP1068564B1 (de)
JP (1) JP2002509844A (de)
CA (1) CA2321586A1 (de)
DE (1) DE69900471T2 (de)
WO (1) WO1999050729A1 (de)

Families Citing this family (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6879885B2 (en) * 2001-11-16 2005-04-12 Goodrich Pump & Engine Control Systems, Inc. Rotor torque predictor
US6648269B2 (en) * 2001-12-10 2003-11-18 Sikorsky Aircraft Corporation Trim augmentation system for a rotary wing aircraft
IL153291A (en) * 2002-12-05 2010-05-31 Nir Padan System and method for situation assessment and dynamic guidance to aerial vehicles for the optimal conduct of close-in maneuvering air combat
US7970498B2 (en) * 2007-06-01 2011-06-28 Sikorsky Aircraft Corporation Model based sensor system for loads aware control laws
US8271151B2 (en) 2008-03-31 2012-09-18 Sikorsky Aircraft Corporation Flight control system for rotary wing aircraft
EP2329203A2 (de) * 2008-10-02 2011-06-08 Carrier Corporation Kühlsystem mit adaptiver heissgasneuerhitzung
EP2296064B1 (de) * 2009-09-10 2019-04-24 Sikorsky Aircraft Corporation Leben verbesserndes Flugsteuerungssystem
US8265815B2 (en) * 2009-11-25 2012-09-11 GM Global Technology Operations LLC Method for controlling output torque in powertrains
US8777803B2 (en) 2011-05-25 2014-07-15 GM Global Technology Operations LLC Method of prioritizing output torque and off-going clutch torque constraints during a torque phase
RU2486108C1 (ru) * 2011-11-18 2013-06-27 Открытое Акционерное Общество "Московский Вертолётный Завод Им. М.Л. Миля" Система контроля оборотов несущего винта вертолета
US9051055B2 (en) * 2013-03-07 2015-06-09 Bell Helicopter Textron Inc. System and method of adaptively governing rotor speed for optimal performance
US9856017B2 (en) 2013-06-11 2018-01-02 Bell Helicopter Textron Inc. Torque based method of limiting vertical axis augmentation
US10508887B2 (en) * 2016-06-02 2019-12-17 Sikorsky Aircraft Corporation Attitude-coupled targeting system for rotary wing aircraft
US10633104B2 (en) 2017-05-17 2020-04-28 General Electric Company Hybrid-electric propulsion system for an aircraft
US10800536B2 (en) 2017-06-09 2020-10-13 General Electric Company Propulsion system for an aircraft
US10006375B1 (en) 2017-07-11 2018-06-26 General Electric Company Propulsion system for an aircraft
US10479491B2 (en) * 2017-08-17 2019-11-19 Textron Innovations Inc. System and method for rotorcraft collective power hold

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
BR8701672A (pt) * 1986-08-04 1988-01-05 United Technologies Corp Processo para detectar uma folha de motor em uma aeronave de motor multiplo
US4998202A (en) * 1989-05-19 1991-03-05 United Technologies Corporation Helicopter, high rotor load speed enhancement
US5178307A (en) * 1991-08-28 1993-01-12 United Technologies Corporation High speed yaw control system for rotary wing aircraft
US5238203A (en) * 1991-08-28 1993-08-24 United Technologies Corporation High speed turn coordination for rotary wing aircraft
ES2099832T3 (es) * 1991-08-28 1997-06-01 United Technologies Corp Sistema de control vertical para helicoptero.
US5331881A (en) * 1992-05-19 1994-07-26 United Technologies Corporation Helicopter integrated fire and flight control having azimuth and pitch control
US5263662A (en) * 1992-05-19 1993-11-23 United Technologies Corporation Helicopter integrated fire and flight control system having turn coordination control
US5310136A (en) * 1992-05-19 1994-05-10 United Technologies Corporation Helicopter integrated fire and flight control having constraint limiting control
US5310135A (en) * 1992-10-28 1994-05-10 United Technologies Corporation Helicopter integrated fire and flight control having coordinated area bombing control
US5465212A (en) * 1993-12-23 1995-11-07 United Technologies Corporation Helicopter integrated fire and flight control having a pre-launch and post-launch maneuver director
US5850615A (en) * 1995-12-06 1998-12-15 Mcdonnell Douglas Helicopter Co. Rotor blade swashplate-axis rotation and gyroscopic moments componsator

Also Published As

Publication number Publication date
WO1999050729A1 (en) 1999-10-07
JP2002509844A (ja) 2002-04-02
EP1068564A1 (de) 2001-01-17
EP1068564B1 (de) 2001-11-14
DE69900471T2 (de) 2002-08-22
CA2321586A1 (en) 1999-10-07
US6012676A (en) 2000-01-11

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Legal Events

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8364 No opposition during term of opposition