GB730010A - Improvements in and relating to flying controls for aircraft - Google Patents

Improvements in and relating to flying controls for aircraft

Info

Publication number
GB730010A
GB730010A GB263452A GB263452A GB730010A GB 730010 A GB730010 A GB 730010A GB 263452 A GB263452 A GB 263452A GB 263452 A GB263452 A GB 263452A GB 730010 A GB730010 A GB 730010A
Authority
GB
United Kingdom
Prior art keywords
cylinder
inclination
links
ratio
link
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
GB263452A
Inventor
John William Morrall
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.)
Boulton Paul Aircraft Ltd
Original Assignee
Boulton Paul Aircraft Ltd
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 Boulton Paul Aircraft Ltd filed Critical Boulton Paul Aircraft Ltd
Priority to GB263452A priority Critical patent/GB730010A/en
Publication of GB730010A publication Critical patent/GB730010A/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
    • B64C13/24—Transmitting means
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05G—CONTROL DEVICES OR SYSTEMS INSOFAR AS CHARACTERISED BY MECHANICAL FEATURES ONLY
    • G05G1/00—Controlling members, e.g. knobs or handles; Assemblies or arrangements thereof; Indicating position of controlling members
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05G—CONTROL DEVICES OR SYSTEMS INSOFAR AS CHARACTERISED BY MECHANICAL FEATURES ONLY
    • G05G2700/00—Control mechanisms or elements therefor applying a mechanical movement
    • G05G2700/02—Means for regulating or adjusting control mechanisms, e.g. devices for automatic adjustment

Landscapes

  • Engineering & Computer Science (AREA)
  • Automation & Control Theory (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Transmission Devices (AREA)

Abstract

730,010. Linkwork. BOULTON PAUL AIRCRAFT, Ltd. Feb. 2, 1953 [Jan. 31, 1952], No. 2634/52. Class 80 (3). [Also in Group XXXIII] The ratio of longitudinalmovement of two links 4, 5 is varied by varying the inclination of a surface 2 along which is movable a pivot connection between the two links. In the embodiment of Fig. 1, the part tubular member 2 is pivotable about an axis 40 by means of link 18 joined to lug 20. The casing 22 contains an internally-threaded cylinder mounted in thrust ball bearings. A pulley is fast to the cylinder, and is rotated by cables driven by a reversible electric motor or manually. The cylinder contains a threaded block attached to lug 20, so that rotation of the cylinder causes the leg to rise or fall, tilting member 2. A pivoted connection between links 4 and 5 slides in member 2, so that the ratio of the longitudinal movements of the reds depends on the inclination of member 2. As in Fig. 3, member 2 consists of angle irons 1 secured to rod, rotatable by link 18. The pivotal connection 6 between rods 4 and 5, of which the latter is forked, is slidable in angle irons 1 by means of rollers 8 or phosphor-bronze slippers. The member 2 may be of any desired shape to cause the ratio of link movement to vary with the inclination of member 2 in any way.
GB263452A 1952-01-31 1952-01-31 Improvements in and relating to flying controls for aircraft Expired GB730010A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB263452A GB730010A (en) 1952-01-31 1952-01-31 Improvements in and relating to flying controls for aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB263452A GB730010A (en) 1952-01-31 1952-01-31 Improvements in and relating to flying controls for aircraft

Publications (1)

Publication Number Publication Date
GB730010A true GB730010A (en) 1955-05-18

Family

ID=9743011

Family Applications (1)

Application Number Title Priority Date Filing Date
GB263452A Expired GB730010A (en) 1952-01-31 1952-01-31 Improvements in and relating to flying controls for aircraft

Country Status (1)

Country Link
GB (1) GB730010A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2476013A1 (en) * 1980-02-19 1981-08-21 Messerschmitt Boelkow Blohm CONTROL DEVICE FOR AIRCRAFT WITH DIFFERENT CHARACTERISTICS IN SLIGHT VOLUME AND IN FAST FLIGHT

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2476013A1 (en) * 1980-02-19 1981-08-21 Messerschmitt Boelkow Blohm CONTROL DEVICE FOR AIRCRAFT WITH DIFFERENT CHARACTERISTICS IN SLIGHT VOLUME AND IN FAST FLIGHT
US4385741A (en) * 1980-02-19 1983-05-31 Messerschmitt-Boelkow-Blohm Gmbh Aircraft steering mechanism

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