GB486749A - Improvements relating to the operation of control surfaces of aircraft - Google Patents

Improvements relating to the operation of control surfaces of aircraft

Info

Publication number
GB486749A
GB486749A GB960838A GB960838A GB486749A GB 486749 A GB486749 A GB 486749A GB 960838 A GB960838 A GB 960838A GB 960838 A GB960838 A GB 960838A GB 486749 A GB486749 A GB 486749A
Authority
GB
United Kingdom
Prior art keywords
axis
axes
spindle
pivot joint
control surfaces
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
GB960838A
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to GB960838A priority Critical patent/GB486749A/en
Publication of GB486749A publication Critical patent/GB486749A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/02—Mounting or supporting thereof

Abstract

486,749. Operating aircraft control surfaces. HUDSON, R. J. H. Dec. 8, 1936, No. 9608/38. Divided out of 487,049. [Class 4] Control mechanism for hinged control surfaces of aircraft comprises an element rotatable about a first axis and carrying a pivot joint with its (a second) axis substantially perpendicular to the first axis, these two axes intersecting the hinge axis of the surface at a point, the pivot joint connecting the said element with a further element rotatably borne in the surface about an (fourth) axis which also intersects at the said point and which is inclined to the first and third axes, whereby rotation of the said first element produces angular movement of the surface. As applied to an aileron 42, Fig. 1, hinged to a wing 43, about axis B, a control spindle 41B is rotatably carried about axis A in wing 43 and carries a fork 41C constituting with a similar fork 44 carried by a spindle 44A rotatably mounted in the aileron, a pivot joint of which the axis C is perpendicular to axis A. Axis D of spindle 44A is inclined to axes A and C, and all four axes are concurrent at F. The mechanism may be arranged to give differential action to the controls.
GB960838A 1936-12-08 1936-12-08 Improvements relating to the operation of control surfaces of aircraft Expired GB486749A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB960838A GB486749A (en) 1936-12-08 1936-12-08 Improvements relating to the operation of control surfaces of aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB960838A GB486749A (en) 1936-12-08 1936-12-08 Improvements relating to the operation of control surfaces of aircraft

Publications (1)

Publication Number Publication Date
GB486749A true GB486749A (en) 1938-06-08

Family

ID=9875253

Family Applications (1)

Application Number Title Priority Date Filing Date
GB960838A Expired GB486749A (en) 1936-12-08 1936-12-08 Improvements relating to the operation of control surfaces of aircraft

Country Status (1)

Country Link
GB (1) GB486749A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4531417A (en) * 1980-09-29 1985-07-30 Hollman Nils David Hinge-type angle setting device

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4531417A (en) * 1980-09-29 1985-07-30 Hollman Nils David Hinge-type angle setting device

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