GB147734A - Hollow supporting surface for flying machines - Google Patents
Hollow supporting surface for flying machinesInfo
- 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
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
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.
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)
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 |
-
1920
- 1920-07-08 GB GB19737/20A patent/GB147734A/en not_active Expired
Cited By (3)
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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