GB305675A - Improvements in and relating to supporting wings or planes for aircraft - Google Patents

Improvements in and relating to supporting wings or planes for aircraft

Info

Publication number
GB305675A
GB305675A GB4387/29A GB438729A GB305675A GB 305675 A GB305675 A GB 305675A GB 4387/29 A GB4387/29 A GB 4387/29A GB 438729 A GB438729 A GB 438729A GB 305675 A GB305675 A GB 305675A
Authority
GB
United Kingdom
Prior art keywords
wing
booms
partitions
aeroplane
fuselage
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
GB4387/29A
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.)
AVIONS BERNARD SOC D
Original Assignee
AVIONS BERNARD SOC D
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 AVIONS BERNARD SOC D filed Critical AVIONS BERNARD SOC D
Publication of GB305675A publication Critical patent/GB305675A/en
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C3/00Wings

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Toys (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

305,675. Soc. des Avions Bernard. Feb. 9, 1928, [Convention date]. Aeroplanes; cabins; planes, construction of. - A multicellular wing for an aeroplane has a resisting portion consisting of a number of laterally juxtaposed longitudinal cells constituted by booms of fibrous material such as wood whose outer surface corresponds to the outer surface of the wing and by vertical partitions each extending from one face of the wing to the other between consecutive booms. A series of vertical partitions a<1>, Fig. 7, which may be made up of inclined strips are glued or otherwise secured between booms b<1> conforming to the surface of the wing, the partitions being stayed by horizontal strips c<1>. The wing may be made roughly to shape as shown to the right of the Figure and subsequently trimmed. The wing has a central enlarged portion which acts as a section of the fuselage and has an axial opening in the enlarged section. Certain of the partitions a<1> near the transverse axis of the wing may be shortened to produce a bifurcated framework towards the wing tips. As shown in Fig. 3, the aeroplane is made up of separate interchangeable sections comprising a propelling element a, the wing structure b, an alighting element c and the fuselage and balancing unit d. The sections may be coupled up after assembly by bolts, eyelets &c.
GB4387/29A 1928-02-09 1929-02-09 Improvements in and relating to supporting wings or planes for aircraft Expired GB305675A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
BE305675X 1928-02-09

Publications (1)

Publication Number Publication Date
GB305675A true GB305675A (en) 1930-05-09

Family

ID=3867475

Family Applications (1)

Application Number Title Priority Date Filing Date
GB4387/29A Expired GB305675A (en) 1928-02-09 1929-02-09 Improvements in and relating to supporting wings or planes for aircraft

Country Status (1)

Country Link
GB (1) GB305675A (en)

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