[go: up one dir, main page]

GB320333A - Improvements in or relating to slotted wings for aircraft - Google Patents

Improvements in or relating to slotted wings for aircraft

Info

Publication number
GB320333A
GB320333A GB1304928A GB1304928A GB320333A GB 320333 A GB320333 A GB 320333A GB 1304928 A GB1304928 A GB 1304928A GB 1304928 A GB1304928 A GB 1304928A GB 320333 A GB320333 A GB 320333A
Authority
GB
United Kingdom
Prior art keywords
lever
rod
spindle
cam
slot
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
GB1304928A
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 GB1304928A priority Critical patent/GB320333A/en
Publication of GB320333A publication Critical patent/GB320333A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C23/00—Influencing air flow over aircraft surfaces, not otherwise provided for

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Transmission Devices (AREA)

Abstract

320,333. Fairey, C. R. May 3, 1928. Controlling. - In order to prevent excessive stresses from being produced at high speeds in wings having auxiliary planes or other " slot " forming means, the auxiliary planes or other means are acted upon to prevent the formation of or to close the slots when the load on a member transmitting stresses in the plane of the flying loads exceeds a predetermined value. The slot mechanism may be acted upon by certain of the main flying wires a at the front of the wing structure which act upon a bell-crank lever b, c. A spring d acting on this lever determines the stress at which the closing action commences. The arm c of this lever moves over a rod g provided with stops h linked to a cam member k mounted on a spindle m, a part j of the cam being concentric with the spindle. The cam k acts on a push rod n connected to one of the parallel links e or other mounting for the auxiliary plane f. A lever i on the spindle m is adapted to be engaged by stops on a rod o connected to a bell-crank lever r moved by a rod s to enable the pilot to close the slot or to prevent it from opening.
GB1304928A 1928-05-03 1928-05-03 Improvements in or relating to slotted wings for aircraft Expired GB320333A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB1304928A GB320333A (en) 1928-05-03 1928-05-03 Improvements in or relating to slotted wings for aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1304928A GB320333A (en) 1928-05-03 1928-05-03 Improvements in or relating to slotted wings for aircraft

Publications (1)

Publication Number Publication Date
GB320333A true GB320333A (en) 1929-10-03

Family

ID=10015853

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1304928A Expired GB320333A (en) 1928-05-03 1928-05-03 Improvements in or relating to slotted wings for aircraft

Country Status (1)

Country Link
GB (1) GB320333A (en)

Similar Documents

Publication Publication Date Title
US2406475A (en) Slotted airplane wing
GB320333A (en) Improvements in or relating to slotted wings for aircraft
US2974903A (en) Aircraft having wings provided with flaps and gas blowing means
GB524864A (en) Improvements relating to folding wing aircraft
US2231858A (en) Engine throttle control
GB558045A (en) Improvements relating to aircraft controls
US2276688A (en) Control device for ailerons and flaps
GB575471A (en) Improvements in tailless aircraft
GB548916A (en) Improvements in and relating to mechanism for releasably locking a pivoted member in one or more positions, particularly applicable to retractable undercarriages for aircraft
GB313415A (en) Improvements in or relating to the tail surfaces of aircraft
GB582206A (en) Improvements in tailless airplanes
GB502336A (en) Improvements in the controls of aircraft
GB176909A (en) Improvements in means for balancing and regulating the lift of aircraft
GB223292A (en) Improvements in the method of and means for controlling aeroplanes
GB581876A (en) Improvements in and relating to aerodynamic control devices for aircraft
US1773625A (en) Aeroplane
GB489392A (en) Improved method and means for operating trimming or balancing flaps on the control surfaces of aircraft
GB695025A (en) Improvements in or relating to high speed aircraft
GB581512A (en) Improvements in or relating to the control surfaces of aircraft
GB1010042A (en) Method and apparatus for controlling an aircraft
GB528808A (en) Improvements in or relating to lift increasing devices for aircraft
GB475163A (en) Aeroplane wing flaps
GB494579A (en) Improvements in the means for controlling the movements of ailerons, rudders, elevators or other moving surfaces of aircraft
GB456969A (en) Improvements in and relating to aircraft and particularly aeroplanes
GB417898A (en) Improvements in or relating to the controlling mechanism of aeroplanes