AT49705B - Airplane. - Google Patents
Airplane.Info
- Publication number
- AT49705B AT49705B AT49705DA AT49705B AT 49705 B AT49705 B AT 49705B AT 49705D A AT49705D A AT 49705DA AT 49705 B AT49705 B AT 49705B
- Authority
- AT
- Austria
- Prior art keywords
- wing
- airplane
- desc
- strips
- fan
- Prior art date
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/38—Adjustment of complete wings or parts thereof
- B64C3/54—Varying in area
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Toys (AREA)
- On-Site Construction Work That Accompanies The Preparation And Application Of Concrete (AREA)
- Supports For Plants (AREA)
Description
<Desc/Clms Page number 1>
A e r 0 p I a n.
Vorliegende Erfindungbetrifft einen Aeroplan, bei welchem die Trag-bezw. Steuerflächen zwecks Lenkung bezw. Steuerung an den Aussenseiten mit fächerförmig einzieh- und ausstreck-
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miteinander durch Geienkstangen derart verbunden sind, dass sie sich bei Betätigung des Flügels paraHe ! zueinander in der richtung ihrer Ebene verschieben und beim Einziehen desselben
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fächerartig auseinander schiebbaren Streifen bestehen, der Vorteil erreicht, dass der iStirnwiderstand sowohl im ausgebreiteten, als auch im eingezogenen Zustande des Flügels wesentlich vermindert wird.
Ferners wird der Einfallswinkel des der Wölbung der Tragfläche angepassten Flügels bei
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ziehen eine Änderung ihrer Lage in bezug auf die Tragfläche erfahren.
In der Zeichnung sind zwei Ausführungsbeispiele dieser Faltflügel an einem Eindecken veranschaulicht. Nach der in Fig. 1, 3 und 4 dargestellten Ausführungsform des Flügels sind die Flächen-
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Schmalseite der Tragfläche jede für sich um 19, 20, 21 in der Ebene desselben drehbar gelagert. Diese Streifen sind durch eine Anzahl Querstangen 2 gelenkig miteinander verbunden, so dass
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**WARNUNG** Ende DESC Feld kannt Anfang CLMS uberlappen**.
<Desc / Clms Page number 1>
A e r 0 p I a n.
The present invention relates to an airplane, in which the support respectively. Control surfaces for the purpose of steering respectively. Control on the outside with fan-shaped pull-in and stretch-out
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are connected to each other by pivot rods in such a way that they are paraHe! move to each other in the direction of their plane and when pulling the same
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There are strips that can be pushed apart like a fan, the advantage that the frontal resistance is significantly reduced both in the expanded and in the retracted state of the wing.
Furthermore, the angle of incidence of the wing adapted to the curvature of the wing is at
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draw a change in their position in relation to the wing.
In the drawing, two exemplary embodiments of these folding wings are illustrated on a covering. According to the embodiment of the wing shown in Fig. 1, 3 and 4, the surface
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The narrow side of the wing is mounted rotatably by 19, 20, 21 in the plane of the same. These strips are articulated to one another by a number of cross bars 2 so that
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** WARNING ** End of DESC field may overlap beginning of CLMS **.
Claims (1)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| AT49705T | 1910-04-09 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| AT49705B true AT49705B (en) | 1911-09-11 |
Family
ID=3570468
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| AT49705D AT49705B (en) | 1910-04-09 | 1910-04-09 | Airplane. |
Country Status (2)
| Country | Link |
|---|---|
| AT (1) | AT49705B (en) |
| GB (1) | GB191108911A (en) |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111959746B (en) * | 2020-08-31 | 2022-10-11 | 哈尔滨工业大学 | Parallel connecting rod type deformation wing framework |
-
1910
- 1910-04-09 AT AT49705D patent/AT49705B/en active
-
1911
- 1911-04-10 GB GB191108911D patent/GB191108911A/en not_active Expired
Also Published As
| Publication number | Publication date |
|---|---|
| GB191108911A (en) | 1911-05-25 |
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