GB8402941D0 - Variable trim-engagement - Google Patents

Variable trim-engagement

Info

Publication number
GB8402941D0
GB8402941D0 GB848402941A GB8402941A GB8402941D0 GB 8402941 D0 GB8402941 D0 GB 8402941D0 GB 848402941 A GB848402941 A GB 848402941A GB 8402941 A GB8402941 A GB 8402941A GB 8402941 D0 GB8402941 D0 GB 8402941D0
Authority
GB
United Kingdom
Prior art keywords
engagement
variable trim
trim
variable
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
GB848402941A
Other versions
GB2135796B (en
GB2135796A (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.)
RTX 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

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C13/00Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
    • B64C13/02Initiating means
    • B64C13/16Initiating means actuated automatically, e.g. responsive to gust detectors
    • B64C13/18Initiating means actuated automatically, e.g. responsive to gust detectors using automatic pilot
    • 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
    • G05D1/0055Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots with safety arrangements
    • G05D1/0061Control 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)
  • Catching Or Destruction (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Communication Control (AREA)
  • Hydraulic Clutches, Magnetic Clutches, Fluid Clutches, And Fluid Joints (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 true GB8402941D0 (en) 1984-03-07
GB2135796A GB2135796A (en) 1984-09-05
GB2135796B 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) ES8502931A1 (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
SE8400998L (en) 1984-08-29
NO158455C (en) 1988-09-14
ES530062A0 (en) 1985-02-01
JPH046600B2 (en) 1992-02-06
NO840682L (en) 1984-08-29
JPS59171794A (en) 1984-09-28
DK104284A (en) 1984-08-29
SE8400998D0 (en) 1984-02-23
ES8502931A1 (en) 1985-02-01
DE3407223A1 (en) 1984-08-30
DE3407223C2 (en) 1994-06-30
GB2135796B (en) 1986-07-09
GB2135796A (en) 1984-09-05
AU2458584A (en) 1984-09-06
NO158455B (en) 1988-06-06
AU558086B2 (en) 1987-01-15
DK104284D0 (en) 1984-02-27
SE451827B (en) 1987-11-02

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Legal Events

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