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GB191416924A - Improvements in Aeroplanes. - Google Patents

Improvements in Aeroplanes.

Info

Publication number
GB191416924A
GB191416924A GB191416924DA GB191416924A GB 191416924 A GB191416924 A GB 191416924A GB 191416924D A GB191416924D A GB 191416924DA GB 191416924 A GB191416924 A GB 191416924A
Authority
GB
United Kingdom
Prior art keywords
bolts
wings
locked
hinged
rack
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
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.)
J Samuel White and Co Ltd
Original Assignee
J Samuel White and Co 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 J Samuel White and Co Ltd filed Critical J Samuel White and Co Ltd
Application granted granted Critical
Publication of GB191416924A publication Critical patent/GB191416924A/en
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C3/00Wings
    • B64C3/38Adjustment of complete wings or parts thereof
    • B64C3/56Folding or collapsing to reduce overall dimensions of aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Hinges (AREA)

Abstract

16,924. White & Co., J. S., and Wright, H. T. July 16. Planes, arrangement and construction of; propelling. -Relates to aeroplanes in which the laterally extending portions of the wings are hinged to the central fixed part and are capable of being turned back to lie parallel with the fuselage for storage, and consists in providing sliding contact gearing, such as a rack and pinion, for moving the wings into and out of the flying position. Means are provided to prevent the motor from being started until the wings are locked in the flying position. The movable portion 3 of the wing is hinged at 5 to the fixed part 1 and is provided with a hinged rack-bar 13 slidable in a pivoted stirrup 17 and engaging a pinion 18 actuated by worm gear 19, 33. The worm shaft is provided with a handle 20 operable when the machine is at rest from the front of the machine. The wings are locked in the extended position by bolts 42 passing through a metal cap 38 on the spar 8 and a clip 39 secured to the spar 14. The bolts are locked in position by a pivoted catch 47 which engages the narrowed part 43 of the bolts. When the bolts are withdrawn, they are carried by a bracket 46 secured to the clip 39 and formed with holes for holding the cylindrical heads 44 of the bolts. In this position of the bolts, the catch 47 engages with a fixed contact-plate 50 connected with the magneto of the motor, so that the magneto is earthed. The rack-and-pinion gear is arranged on the lower wing of a biplane, and the upper foldable wings are provided with a spring locking- bolt to secure them to the central fixed portion.
GB191416924D 1914-07-16 1914-07-16 Improvements in Aeroplanes. Expired GB191416924A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB191416924T 1914-07-16

Publications (1)

Publication Number Publication Date
GB191416924A true GB191416924A (en) 1915-03-18

Family

ID=32585610

Family Applications (1)

Application Number Title Priority Date Filing Date
GB191416924D Expired GB191416924A (en) 1914-07-16 1914-07-16 Improvements in Aeroplanes.

Country Status (1)

Country Link
GB (1) GB191416924A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2015150817A1 (en) * 2014-04-04 2015-10-08 Airbus Operations Limited An aircraft wing with a wing tip device and a strut
GB2555854A (en) * 2016-11-14 2018-05-16 Airbus Operations Ltd Rack and pinion systems
CN109515684A (en) * 2018-12-07 2019-03-26 贵州华阳电工有限公司 Wing-folding manipulation device

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2015150817A1 (en) * 2014-04-04 2015-10-08 Airbus Operations Limited An aircraft wing with a wing tip device and a strut
GB2555854A (en) * 2016-11-14 2018-05-16 Airbus Operations Ltd Rack and pinion systems
CN109515684A (en) * 2018-12-07 2019-03-26 贵州华阳电工有限公司 Wing-folding manipulation device
CN109515684B (en) * 2018-12-07 2021-10-22 贵州华阳电工有限公司 Wing folding control device

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