AU2458584A - Variable trim-engagement system - Google Patents

Variable trim-engagement system

Info

Publication number
AU2458584A
AU2458584A AU24585/84A AU2458584A AU2458584A AU 2458584 A AU2458584 A AU 2458584A AU 24585/84 A AU24585/84 A AU 24585/84A AU 2458584 A AU2458584 A AU 2458584A AU 2458584 A AU2458584 A AU 2458584A
Authority
AU
Australia
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.)
Granted
Application number
AU24585/84A
Other versions
AU558086B2 (en
Inventor
Kenneth Charles Arifian
Douglas Harold Clelford
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 AU2458584A publication Critical patent/AU2458584A/en
Application granted granted Critical
Publication of AU558086B2 publication Critical patent/AU558086B2/en
Anticipated expiration legal-status Critical
Ceased 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 or altitude of land, water, air, or space vehicles, e.g. automatic pilot
    • G05D1/0055—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot with safety arrangements
    • G05D1/0061—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot with safety arrangements for transition from automatic pilot to manual pilot and vice versa
AU24585/84A 1983-02-28 1984-02-14 Variable trim-engagement system Ceased AU558086B2 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US47040183A 1983-02-28 1983-02-28
US470401 1983-02-28

Publications (2)

Publication Number Publication Date
AU2458584A true AU2458584A (en) 1984-09-06
AU558086B2 AU558086B2 (en) 1987-01-15

Family

ID=23867487

Family Applications (1)

Application Number Title Priority Date Filing Date
AU24585/84A Ceased AU558086B2 (en) 1983-02-28 1984-02-14 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
SE8400998D0 (en) 1984-02-23
DE3407223A1 (en) 1984-08-30
JPH046600B2 (en) 1992-02-06
NO158455B (en) 1988-06-06
AU558086B2 (en) 1987-01-15
NO840682L (en) 1984-08-29
DK104284D0 (en) 1984-02-27
JPS59171794A (en) 1984-09-28
DE3407223C2 (en) 1994-06-30
GB2135796A (en) 1984-09-05
GB8402941D0 (en) 1984-03-07
DK104284A (en) 1984-08-29
NO158455C (en) 1988-09-14
SE451827B (en) 1987-11-02
GB2135796B (en) 1986-07-09
ES530062A0 (en) 1985-02-01
SE8400998L (en) 1984-08-29
ES8502931A1 (en) 1985-02-01

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