GB256743A - Improvements in aeroplanes having folding wings - Google Patents

Improvements in aeroplanes having folding wings

Info

Publication number
GB256743A
GB256743A GB15518/25A GB1551825A GB256743A GB 256743 A GB256743 A GB 256743A GB 15518/25 A GB15518/25 A GB 15518/25A GB 1551825 A GB1551825 A GB 1551825A GB 256743 A GB256743 A GB 256743A
Authority
GB
United Kingdom
Prior art keywords
wings
rings
turret
fuselage
ring
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
GB15518/25A
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 GB15518/25A priority Critical patent/GB256743A/en
Publication of GB256743A publication Critical patent/GB256743A/en
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64UUNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U20/00Constructional aspects of UAVs
    • B64U20/50Foldable or collapsible UAVs

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Remote Sensing (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Pivots And Pivotal Connections (AREA)

Abstract

256,743. Saunders, S. E. June 15, 1925. Planes, arrangement and construction of. -The wings of an aeorplane are hinged about a common axis so that they can fold towards each other into line with the fuselage, provision being made for moving the wings out of their common level, as they fold, into positions one above the other. In the case of a biplane, the upper wings fold above and the lower wings below the fuselage, the interplane struts being hinged to one plane of each pair. The two lower wings b, c of a biplane are secured to rings e, f surrounding a turret d secured to the fuselage, the engaging edges g, h of the rings being inclined to ensure that the wing 'b is raised out of the plane of the wing c as the wings are folded. The upper edge of the ring e and the lower edge of a sleeve w surrounding the turret dare curved as shown at e<1> so as to engage one another in both the upper and lower positions of :the ring e. Toothed quadrants k, v engaged by pinions l, u are provided on the rings f, e, the quadrant v being curved to permit therising movement of the ring e. The pinions l, u are turned by chain gearing from a hand-wheel n. Spring-pressed locking-bolts x in the turret d, operated by Bowden cables from a lever z, lock the rings e, f in their two positions. According to the Provisional Specification, the wings .may be of metal or of sewn plywood such as that known under the Trade Mark " Consuta.''
GB15518/25A 1925-06-15 1925-06-15 Improvements in aeroplanes having folding wings Expired GB256743A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB15518/25A GB256743A (en) 1925-06-15 1925-06-15 Improvements in aeroplanes having folding wings

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB15518/25A GB256743A (en) 1925-06-15 1925-06-15 Improvements in aeroplanes having folding wings

Publications (1)

Publication Number Publication Date
GB256743A true GB256743A (en) 1926-08-19

Family

ID=10060533

Family Applications (1)

Application Number Title Priority Date Filing Date
GB15518/25A Expired GB256743A (en) 1925-06-15 1925-06-15 Improvements in aeroplanes having folding wings

Country Status (1)

Country Link
GB (1) GB256743A (en)

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2573271A (en) * 1947-06-30 1951-10-30 Adolph R Perl Roadable aircraft
US2707084A (en) * 1954-07-01 1955-04-26 Jr Edward K Mills Land, sea, and air vehicle
US2812911A (en) * 1953-07-30 1957-11-12 Jean Leland De Folding wing airplane
US3415467A (en) * 1967-01-30 1968-12-10 Joseph A. Barringer Retrievable rocket with folded wings
CN102390229A (en) * 2011-10-10 2012-03-28 南昌航空大学 Airfoil transformation mechanism of submarine aircraft
CN109367760A (en) * 2018-09-21 2019-02-22 北京大翔航空科技有限公司 A kind of light-duty unmanned plane wing-folding unfolding mechanism
RU2731138C1 (en) * 2019-12-30 2020-08-31 Российская Федерация, от имени которой выступает Государственная корпорация по атомной энергии "Росатом" (Госкорпорация "Росатом") Device for fixation of aircraft outer wings in folded state

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2573271A (en) * 1947-06-30 1951-10-30 Adolph R Perl Roadable aircraft
US2812911A (en) * 1953-07-30 1957-11-12 Jean Leland De Folding wing airplane
US2707084A (en) * 1954-07-01 1955-04-26 Jr Edward K Mills Land, sea, and air vehicle
US3415467A (en) * 1967-01-30 1968-12-10 Joseph A. Barringer Retrievable rocket with folded wings
CN102390229A (en) * 2011-10-10 2012-03-28 南昌航空大学 Airfoil transformation mechanism of submarine aircraft
CN109367760A (en) * 2018-09-21 2019-02-22 北京大翔航空科技有限公司 A kind of light-duty unmanned plane wing-folding unfolding mechanism
RU2731138C1 (en) * 2019-12-30 2020-08-31 Российская Федерация, от имени которой выступает Государственная корпорация по атомной энергии "Росатом" (Госкорпорация "Росатом") Device for fixation of aircraft outer wings in folded state

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