DE400727C - Wing with corrugated iron covering - Google Patents
Wing with corrugated iron coveringInfo
- Publication number
- DE400727C DE400727C DEE26064D DEE0026064D DE400727C DE 400727 C DE400727 C DE 400727C DE E26064 D DEE26064 D DE E26064D DE E0026064 D DEE0026064 D DE E0026064D DE 400727 C DE400727 C DE 400727C
- Authority
- DE
- Germany
- Prior art keywords
- wing
- covering
- corrugated iron
- iron covering
- waves
- 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
- B64C3/26—Construction, shape, or attachment of separate skins, e.g. panels
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Laminated Bodies (AREA)
Description
Tragfläche mit Wellblechbespannung. Es ist bekannt, Tragflächen von Flugzeugen mit Wellblech zu bekleiden, dessen; Wellen quer zur Flugrichtung liegen. Hierbei ist jedoch nur .der mittlere Teil der Tragfläche mit Wellblech bespannt, und es ist für diesen Teil eine besondere Versteifung vorgesehen.Wing with corrugated sheet metal covering. It is known to have wings of To clad aircraft with corrugated iron, of; Waves are perpendicular to the direction of flight. However, only the middle part of the wing is covered with corrugated iron. and a special stiffener is provided for this part.
Nach der Erfindung reicht die Bespannung mit quer zur Flugrichtung verlaufenden Wellen über das ganze Flügelprofil, .abgesehen von der vorderen Rundung, wo die Bespannung ohne Wellen ausgeführt ist; hierbei dienen in ihrer eigenen Ebene versteifte, mit den benachbarten Spanten durch Diagonalstreben verbundene Spanten zur Verstrebung des Ganzen, so daß die Holme entbehrlich werden.According to the invention, the covering is sufficient with transverse to the direction of flight running waves over the whole wing profile, apart from the front curve, where the covering is made without waves; here serve in their own level stiffened ribs connected to the neighboring ribs by diagonal struts to brace the whole thing, so that the spars are dispensable.
Die Zeichnung veranschaulicht den Gegenstand der Erfindung an einem Ausführungsbeispiel, und zwar zeigt Abb. i einen Querschnitt durch die Tragfläche, Abb. z einen Längsschnitt und Abb. g eine Oberansicht dazu.The drawing illustrates the subject matter of the invention on a Embodiment, namely Fig. I shows a cross section through the wing, Fig. Z is a longitudinal section and Fig. G is a top view.
Mit a und b ist diel Bespannung der Ober-und Unterseite in der zur Flugrichtung quer verlaufenden Wellung bezeichnet. Diese Be. spannung ist auf den Spant c aufgeschraubt oder genietet. Der. Spant c ist in sich durch Streben oder Stege d versteift. A and b denote the covering of the upper and lower sides in the corrugation running transversely to the direction of flight. This Be. tension is screwed or riveted onto frame c. Of the. Frame c is stiffened by struts or webs d.
Wie die Abb. a zeigt,, ist die Bespannung durch -mehrere solcher Spanten c, d verbunden, welche unterein-nder durch Streben e, versteift-. sind. Diese Streben können auch als Bänder ausgebildet sein, welche gleichzeitig mit der Bespannung und den Spanten verbunden sind.As Fig. A shows, the covering is made up of several such frames c, d connected, which are stiffened by struts e, stiffened. are. This pursuit can also be designed as bands, which are concurrent with the covering and the frames are connected.
Die Abbildungen zeigen, daß die Bauart für die ganze Tragfläche einheitlich durchgeführt ist. Die Holme sind vermieden, und die Bespannung, die Ober- und Untergurte und die Spanten und Streben bilden das Fachwerk.The figures show that the design is the same for the entire wing is carried out. The spars are avoided, and the covering, the upper and lower straps and the frames and struts form the framework.
Claims (1)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DEE26064D DE400727C (en) | 1920-12-31 | 1920-12-31 | Wing with corrugated iron covering |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DEE26064D DE400727C (en) | 1920-12-31 | 1920-12-31 | Wing with corrugated iron covering |
Publications (1)
Publication Number | Publication Date |
---|---|
DE400727C true DE400727C (en) | 1924-08-23 |
Family
ID=7071962
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DEE26064D Expired DE400727C (en) | 1920-12-31 | 1920-12-31 | Wing with corrugated iron covering |
Country Status (1)
Country | Link |
---|---|
DE (1) | DE400727C (en) |
-
1920
- 1920-12-31 DE DEE26064D patent/DE400727C/en not_active Expired
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