GB278020A - Monoplane with wings attached to the sides of the fuselage - Google Patents
Monoplane with wings attached to the sides of the fuselageInfo
- Publication number
- GB278020A GB278020A GB25500/27A GB2550027A GB278020A GB 278020 A GB278020 A GB 278020A GB 25500/27 A GB25500/27 A GB 25500/27A GB 2550027 A GB2550027 A GB 2550027A GB 278020 A GB278020 A GB 278020A
- Authority
- GB
- United Kingdom
- Prior art keywords
- fuselage
- points
- wing
- struts
- spars
- 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)
- Toys (AREA)
Abstract
278,020. Rohrba-ch, A. Sept. 27, 1926, [Convention date]. Planes, connecting to machine.-A monoplane has its wings jointed to the fuselage sides, each wing spar, or some of the wing spars, being connected thereto by a direct joint and by a short inclined strut connected at one end to the fuselage and at the other to the wing spar a short distance along the span. A wing is shown having the upper girders of its spars connected to the fuselage at two points c and the lower girders of the spars connected at points d to short struts f which are connected to the fuselage at two points g or at points h or i. Struts n connect the points c, d. The root of the wing may terminate along the line m to avoid obstruction of the view from the windows, or a transparent section r may continue the contour of the wing. Modifications are described in which the struts f on each side of the machine converge to single points on the lower edge or to a common point in the base of the fuselage. In another modification, the points d of each wing are connected by a horizontal member supported at its centre by a short inclined strut connected to the fuselage. The wings may have their direct connections at the bottom of the fuselage and their strut connections at the top.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE278020X | 1926-09-27 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB278020A true GB278020A (en) | 1928-01-19 |
Family
ID=6028452
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB25500/27A Expired GB278020A (en) | 1926-09-27 | 1927-09-27 | Monoplane with wings attached to the sides of the fuselage |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB278020A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| RU2448866C1 (en) * | 2010-11-08 | 2012-04-27 | Открытое акционерное общество "Авиационный комплекс им. С.В. Ильюшина" | Device for jointing aircraft wing to fuselage |
-
1927
- 1927-09-27 GB GB25500/27A patent/GB278020A/en not_active Expired
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| RU2448866C1 (en) * | 2010-11-08 | 2012-04-27 | Открытое акционерное общество "Авиационный комплекс им. С.В. Ильюшина" | Device for jointing aircraft wing to fuselage |
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