DE197062C - - Google Patents
Info
- Publication number
- DE197062C DE197062C DENDAT197062D DE197062DA DE197062C DE 197062 C DE197062 C DE 197062C DE NDAT197062 D DENDAT197062 D DE NDAT197062D DE 197062D A DE197062D A DE 197062DA DE 197062 C DE197062 C DE 197062C
- Authority
- DE
- Germany
- Prior art keywords
- bicycle
- front wheel
- air
- wings
- attached
- 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.)
- Active
Links
- 210000001503 Joints Anatomy 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C31/00—Aircraft intended to be sustained without power plant; Powered hang-glider-type aircraft; Microlight-type aircraft
- B64C31/04—Man-powered aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Motorcycle And Bicycle Frame (AREA)
Description
KAISERLICHESIMPERIAL
PATENTAMT.PATENT OFFICE.
Die Erfindung bezieht sich auf eine Flugmaschine mit Fahrrad und besteht darin, daß das Vorderrad des Fahrrades als Steuersegel ausgebildet ist.The invention relates to a flying machine with a bicycle and consists in that the front wheel of the bicycle is designed as a control sail.
Auf der beiliegenden Zeichnung ist die Flugmaschine mit dem Fahrrad in Fig. ι in Seitenansicht und in Fig. 2 in Vorderansicht dargestellt.On the accompanying drawing, the flying machine is shown with the bicycle in Fig. Ι in Side view and shown in Fig. 2 in front view.
Das Gestell des Zweirades trägt die Ständer α und b, mit welchen die Flügel c (Fig. 2) durch die Schenkel d und durch Gelenke verbunden sind. Die Bewegung der Flügel erfolgt von dem als Schwungrad dienenden Hinterrade aus, an dessen nach beiden Seiten verlängerter Achse Kurbeln h (Fig. 2) angebracht sind. An diese sind mittels Zapfen ι die Pleuelstangen k angelenkt, welche mit den Flügeln gelenkig verbunden sind.The frame of the two-wheeler carries the stands α and b, with which the wings c (Fig. 2) are connected by the legs d and by joints. The wings are moved from the rear wheel, which acts as a flywheel, on whose axis, which is extended on both sides, cranks h (FIG. 2) are attached. These connecting rods are articulated by means of pins k ι, which are articulated to the wings.
Das Vorderrad ist nun als Steuersegel ausgebildet und zu diesem Zwecke mit luftdichtem Stoff ρ, (Fig. 1) bespannt. Durch eine an der geraden Lenkstange angebrachte, in eine Nut r einer am Fahrrad angebrachten Scheibe s eingreifende federnde Klinke (Fig. 2) kann das Vorderrad während der Fahrt in der Luft festgestellt werden.The front wheel is now designed as a control sail and for this purpose covered with airtight material ρ, (Fig. 1). By means of a resilient pawl (FIG. 2) which is attached to the straight handlebar and engages in a groove r of a disk s attached to the bicycle, the front wheel can be fixed in the air while driving.
Um sich mit dem Fahrzeug in die Luft zu erheben, wird es mit möglichst großer Geschwindigkeit vorwärts bewegt, und bei hinreichender Geschwindigkeit wird es, durch den unter der schräg gestellten Schwebefläche entstehenden Luftdruck unterstützt, durch die Flügelbewegung sich vom Erdboden erheben. Sowohl bei der Fahrt auf dem Erdboden als auch bei der Fortbewegung in der Luft soll das Vorderrad zur Steuerung dienen.In order to get the vehicle into the air, it will be as large as possible Speed moves forward, and with sufficient speed it will move through supports the air pressure under the inclined floating surface, through which Wing movement rise from the ground. Both when driving on the ground as well as when moving in the air, the front wheel should be used for steering.
Claims (1)
Publications (1)
Publication Number | Publication Date |
---|---|
DE197062C true DE197062C (en) |
Family
ID=459984
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DENDAT197062D Active DE197062C (en) |
Country Status (1)
Country | Link |
---|---|
DE (1) | DE197062C (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE3731210A1 (en) * | 1987-09-17 | 1989-04-06 | Heinrich Sandrock | Flapping-wing aircraft having struts and ribs made of a material whose modulus of elasticity reduces in the longitudinal direction |
DE102009035147A1 (en) * | 2009-07-29 | 2011-03-03 | Sepp Schiller | Transmission flutter for generation and transmission of movements by wings, fins or rudders, in liquid or gas, has fully articulated and supported carrying beam |
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0
- DE DENDAT197062D patent/DE197062C/de active Active
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE3731210A1 (en) * | 1987-09-17 | 1989-04-06 | Heinrich Sandrock | Flapping-wing aircraft having struts and ribs made of a material whose modulus of elasticity reduces in the longitudinal direction |
DE102009035147A1 (en) * | 2009-07-29 | 2011-03-03 | Sepp Schiller | Transmission flutter for generation and transmission of movements by wings, fins or rudders, in liquid or gas, has fully articulated and supported carrying beam |
DE102009035147A8 (en) * | 2009-07-29 | 2011-06-01 | Sepp Schiller | Flatter gear |
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