DE437671C - Airplane with motorcycle - Google Patents
Airplane with motorcycleInfo
- Publication number
- DE437671C DE437671C DEW69900D DEW0069900D DE437671C DE 437671 C DE437671 C DE 437671C DE W69900 D DEW69900 D DE W69900D DE W0069900 D DEW0069900 D DE W0069900D DE 437671 C DE437671 C DE 437671C
- Authority
- DE
- Germany
- Prior art keywords
- motorcycle
- airplane
- wings
- folded
- aircraft
- 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
- 239000000725 suspension Substances 0.000 claims 1
- 238000004804 winding Methods 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/38—Adjustment of complete wings or parts thereof
- B64C3/56—Folding or collapsing to reduce overall dimensions of aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Motorcycle And Bicycle Frame (AREA)
Description
Flugzeug mit Motorrad. Der Gegenstand der Erfindung ist ein in Abb. i dargestelltes Flugzeug mit Motorrad, das mit Tragflächen a, Propellerantrieb, V erwindungsklappen b, Höhen- und Seitensteuer und den sonstigen bekannten Einrichtungen ausgerüstet ist.Airplane with motorcycle. The subject of the invention is a fig. i illustrated aircraft with motorcycle, which with wings a, propeller drive, V winding flaps b, elevation and rudder control and the other known devices is equipped.
Das in Abb. i dargestellte Flugzeug weist beiderseits die Tragflächen a auf, die mitsamt den Verwindungseinrichtungen b zum Transport um in der Flugrichtung liegende Achsen c nach oben geklappt sind. Aus Abb. z ist ersichtlich, daß mittels der Federzüge d; durch welche der Flugzeugkörper mit den Tragflächen a verbunden ist, die letzteren beiderseits nach oben geklappt werden. Zum Flug lassen sich. die Tragflächen a, wie aus Abb. 3 hervorgeht, durch die mittels, Pedals fi zu bewegende Windevorrichtung g in die Gebrauchslage herabklappen. Zu diesem Behuf laufen an der Außenseite der Tragflächen, die in hochgeklappter Stellung einen rechten Winkel nicht erreichen sollen, Drahtseile e oder Gliederketten über in der Drehungsachse e liegende Rollenführungen f mit Kugellager zu der möglichst tief verankerten Windeeinrichtung g, die mittels Pedal k und Übersetzung! betätigt wird. Dieser Mechanismus ist jedoch ebenso für einen anderes an sich bekannten motorischen Antrieb einrichtbar, der selbsttätig oder willkürlich bedient wird.The aircraft shown in Fig. I has the wings on both sides a, which together with the twisting devices b for transport around in the direction of flight lying axes c are folded up. From Fig. Z it can be seen that by means of the pen balancer d; through which the aircraft body is connected to the wings a the latter can be folded up on both sides. To the flight can be. the wings a, as out Fig. 3 shows through the means, Fold down pedals fi to be moved winch g into the position of use. to this Behuf run on the outside of the wings, which are in the folded-up position should not reach a right angle, wire ropes or link chains over in the rotation axis e lying roller guides f with ball bearings to the possible deeply anchored winch device g, which by means of pedal k and translation! actuated will. However, this mechanism is also for another known motor Drive can be set up, which is operated automatically or arbitrarily.
Durch die Erfindung soll die schnell und leicht herbeizuführende Transportfähigkeit des Flugzeugs auf Wegen von beliebigem Querschnitt sowie die Unabhängigkeit von besonderer Start- und Landungsfläche erzielt werden.The invention is intended to be able to be transported quickly and easily of the aircraft on paths of any cross-section and independence from special take-off and landing areas can be achieved.
Claims (1)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DEW69900D DE437671C (en) | 1925-01-15 | 1925-01-15 | Airplane with motorcycle |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DEW69900D DE437671C (en) | 1925-01-15 | 1925-01-15 | Airplane with motorcycle |
Publications (1)
Publication Number | Publication Date |
---|---|
DE437671C true DE437671C (en) | 1926-11-24 |
Family
ID=7608501
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DEW69900D Expired DE437671C (en) | 1925-01-15 | 1925-01-15 | Airplane with motorcycle |
Country Status (1)
Country | Link |
---|---|
DE (1) | DE437671C (en) |
-
1925
- 1925-01-15 DE DEW69900D patent/DE437671C/en not_active Expired
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