GB147734A - Hollow supporting surface for flying machines - Google Patents

Hollow supporting surface for flying machines

Info

Publication number
GB147734A
GB147734A GB19737/20A GB1973720A GB147734A GB 147734 A GB147734 A GB 147734A GB 19737/20 A GB19737/20 A GB 19737/20A GB 1973720 A GB1973720 A GB 1973720A GB 147734 A GB147734 A GB 147734A
Authority
GB
United Kingdom
Prior art keywords
tubes
corrugations
spars
corrugated
plane
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
GB19737/20A
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
Publication of GB147734A publication Critical patent/GB147734A/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)
  • Tents Or Canopies (AREA)

Abstract

147,734. Junkers, H. Dec. 22, 1916, [Convention date]. Planes, construction of. - Planes for flying-machines are formed with lattice girder spans rigidly connected to a corrugated sheet-metal envelope without the. use of ribs or external bracing, the corrugations extending in the direction of flight. Figs 1 and 2 show longitudinal and transverse sections of a wing in which spars comprising upper and lower tubes 1, 2 united by vertical and inclined tubes 3, 4 are riveted directly to a corrugated metal envelope 6. Adjacent spars are connected together by diagonal braces 5. A modification is described in which the upper and lower booms are in staggered relation and braced only by diagonal members forming approximately equilateral triangles. The tubes taper in diameter or thickness of wall towards the wing tips. The leading edge of the plane where the curvature is sharp may be formed as a separate piece corrugated as shown in Fig. 17 so that the corrugations on the upper and lower surfaces of the plane are offset in order that they nest together at the rear edges of the plane, where they are secured over a wood filling-piece 28 as shown in Fig. 13. Alternatively, the leading edge may be made straight at the extreme front with gradually deeper corrugations towards its junction with the main surfaces, or it may be of trough form with straight edges joined to the main coverings, the corrugations of which diminish in depth towards the junction. The covering may be riveted directly to the tubes 1, 2 of the spars or to reinforcing-pieces 16 or 21, Figs. 8 and 10, clamped to the tubes. The covering may have an extra deep corrugation 9, Fig. 6, at intervals, or additional strengthening-pieces 10, corrugated at 11, may be applied to the surface either continuously on the outside or between adjacent spars on the inside. Rudders, fins, &e. may also be formed in this manner.
GB19737/20A 1916-12-22 1920-07-08 Hollow supporting surface for flying machines Expired GB147734A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE147734X 1916-12-22

Publications (1)

Publication Number Publication Date
GB147734A true GB147734A (en) 1921-09-01

Family

ID=5672193

Family Applications (1)

Application Number Title Priority Date Filing Date
GB19737/20A Expired GB147734A (en) 1916-12-22 1920-07-08 Hollow supporting surface for flying machines

Country Status (1)

Country Link
GB (1) GB147734A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2020059489A (en) * 2018-09-14 2020-04-16 ザ・ボーイング・カンパニーThe Boeing Company Monolithic spar for wing
WO2020120931A1 (en) * 2018-12-10 2020-06-18 Airbus Operations Limited Method of manufacturing an aerodynamic structure

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2020059489A (en) * 2018-09-14 2020-04-16 ザ・ボーイング・カンパニーThe Boeing Company Monolithic spar for wing
WO2020120931A1 (en) * 2018-12-10 2020-06-18 Airbus Operations Limited Method of manufacturing an aerodynamic structure
US12116123B2 (en) 2018-12-10 2024-10-15 Airbus Operations Limited Method of manufacturing an aerodynamic structure

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