GB2135796B - Variable trim-engagement system - Google Patents

Variable trim-engagement system

Info

Publication number
GB2135796B
GB2135796B GB08402941A GB8402941A GB2135796B GB 2135796 B GB2135796 B GB 2135796B GB 08402941 A GB08402941 A GB 08402941A GB 8402941 A GB8402941 A GB 8402941A GB 2135796 B GB2135796 B GB 2135796B
Authority
GB
United Kingdom
Prior art keywords
engagement system
variable trim
trim
variable
engagement
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
GB08402941A
Other versions
GB8402941D0 (en
GB2135796A (en
Inventor
Douglas Harold Clelford
Kenneth Charles Arifian
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 GB8402941D0 publication Critical patent/GB8402941D0/en
Publication of GB2135796A publication Critical patent/GB2135796A/en
Application granted granted Critical
Publication of GB2135796B publication Critical patent/GB2135796B/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
    • B64C13/02—Initiating means
    • B64C13/16—Initiating means actuated automatically, e.g. responsive to gust detectors
    • B64C13/18—Initiating means actuated automatically, e.g. responsive to gust detectors using automatic pilot
    • 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
    • G05D1/0055—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots with safety arrangements
    • G05D1/0061—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots with safety arrangements for transition from automatic pilot to manual pilot and vice versa

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Automation & Control Theory (AREA)
  • Remote Sensing (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Numerical Control (AREA)
  • Hydraulic Clutches, Magnetic Clutches, Fluid Clutches, And Fluid Joints (AREA)
  • Catching Or Destruction (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Communication Control (AREA)
  • Mechanical Control Devices (AREA)
  • Position Input By Displaying (AREA)
GB08402941A 1983-02-28 1984-02-03 Variable trim-engagement system Expired GB2135796B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US47040183A 1983-02-28 1983-02-28

Publications (3)

Publication Number Publication Date
GB8402941D0 GB8402941D0 (en) 1984-03-07
GB2135796A GB2135796A (en) 1984-09-05
GB2135796B true GB2135796B (en) 1986-07-09

Family

ID=23867487

Family Applications (1)

Application Number Title Priority Date Filing Date
GB08402941A Expired GB2135796B (en) 1983-02-28 1984-02-03 Variable trim-engagement system

Country Status (8)

Country Link
JP (1) JPS59171794A (en)
AU (1) AU558086B2 (en)
DE (1) DE3407223C2 (en)
DK (1) DK104284A (en)
ES (1) ES530062A0 (en)
GB (1) GB2135796B (en)
NO (1) NO158455C (en)
SE (1) SE451827B (en)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3431583A1 (en) * 1984-08-28 1986-03-13 Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn DEVICE FOR THE AUTOMATIC ELIMINATION OF TAX FORCE ERRORS IN AIRCRAFT, IN PARTICULAR HELICOPTERS
GB2339614B (en) * 1998-07-14 2000-06-21 Infrared Integrated Syst Ltd Detector-array sensor with mask warning
US6325331B1 (en) * 1998-12-11 2001-12-04 Bell Helicopter Textron Inc. Trim actuator
JP3091743B1 (en) 1999-03-30 2000-09-25 株式会社コミュータヘリコプタ先進技術研究所 Pilot device
US6311930B1 (en) * 1999-07-16 2001-11-06 Swales Aerospace Anti-friction release device

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4387432A (en) * 1981-03-30 1983-06-07 United Technologies Corporation Pulsed aircraft actuator

Also Published As

Publication number Publication date
NO158455B (en) 1988-06-06
GB8402941D0 (en) 1984-03-07
SE8400998D0 (en) 1984-02-23
SE451827B (en) 1987-11-02
DE3407223C2 (en) 1994-06-30
AU558086B2 (en) 1987-01-15
NO840682L (en) 1984-08-29
DK104284A (en) 1984-08-29
DK104284D0 (en) 1984-02-27
AU2458584A (en) 1984-09-06
NO158455C (en) 1988-09-14
JPH046600B2 (en) 1992-02-06
GB2135796A (en) 1984-09-05
ES8502931A1 (en) 1985-02-01
ES530062A0 (en) 1985-02-01
JPS59171794A (en) 1984-09-28
SE8400998L (en) 1984-08-29
DE3407223A1 (en) 1984-08-30

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Legal Events

Date Code Title Description
PCNP Patent ceased through non-payment of renewal fee