DE474719C - Airplane with cylinders rotating around transverse axes - Google Patents
Airplane with cylinders rotating around transverse axesInfo
- Publication number
- DE474719C DE474719C DEW72446D DEW0072446D DE474719C DE 474719 C DE474719 C DE 474719C DE W72446 D DEW72446 D DE W72446D DE W0072446 D DEW0072446 D DE W0072446D DE 474719 C DE474719 C DE 474719C
- Authority
- DE
- Germany
- Prior art keywords
- airplane
- rotating around
- transverse axes
- around transverse
- cylinders rotating
- 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
- B64C39/00—Aircraft not otherwise provided for
- B64C39/003—Aircraft not otherwise provided for with wings, paddle wheels, bladed wheels, moving or rotating in relation to the fuselage
- B64C39/005—Aircraft not otherwise provided for with wings, paddle wheels, bladed wheels, moving or rotating in relation to the fuselage about a horizontal transversal axis
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Wind Motors (AREA)
- Toys (AREA)
Description
Flugzeug mit um Querachsen rotierenden Zylindern Es sind bereits Einrichtungen bekannt geworden, Flugzeuge zeit quer zur Flugrichtung angeordneten, rotierenden Zylindern zu versehen. Die Anordnungen erzeugen Wirkungen nach Art des bekannten Magnuseffektes und äußern sich bei Flugzeugen derart, daß ein leichterer und steilerer Auftrieb sowie auch ein Vortrieb erzielt wird.Airplane with cylinders rotating around transverse axes There are already facilities It has become known that aircraft are rotating at right angles to the direction of flight To provide cylinders. The arrangements produce effects of the known type Magnus effect and manifest themselves in aircraft in such a way that a lighter and steeper Buoyancy as well as propulsion is achieved.
Der Gegenstand der Erfindung betrifft nun ein Flugzeug, bei dem die Rotoren auch als Tragflächen in Tätigkeit treten. können. Zu diesem Zwecke sind erfndUngsgeniäß die Zylindermantelflächen in kleine Flächen unterteilt, die durch eine beliebige Einstellvorrichtung vom Führerstande aus um Achsen quer zur Flugrichtung umgelegt werden können.The object of the invention now relates to an aircraft in which the Rotors also act as wings. can. For this purpose are In accordance with the invention, the cylinder jacket surfaces are divided into small surfaces that run through any adjustment device from the driver's cab around axes transverse to the direction of flight can be turned over.
In der Zeichnung ist der Erfindungsgegenstand schematisch in Seitenansicht dargestellt. Mit a ist eine Tragfläche bezeichnet, unter der ein Rotor b angeordnet ist. Der Mantel des Rotors besteht aus einzelnen drehbaren kleinen Flächen, die in irgendeiner Weise in wagerechte Lage und parallel zueinander eingestellt werden können, sobald der Rotor zum Stillstand gebracht worden ist. In der Zeichnung ist die Einstellungsart dieser Flächen c punktiert angedeutet; ;es ist verständlich, daß die Flächen c in dieser Stellung eine Art Tragflächen bilden, da, die Luftströmungen zwischen den Flächen hindurchstreichen können, wobei aus -der Summe der sämtlichen kleinen Flächen eine große Tragfläche gebildet wird.In the drawing, the subject matter of the invention is shown schematically in a side view shown. With a wing is referred to, under which a rotor b is arranged is. The casing of the rotor consists of individual rotatable small surfaces, which be adjusted in any way in a horizontal position and parallel to each other as soon as the rotor has been brought to a standstill. In the drawing is the type of setting of these surfaces c indicated by dotted lines; ;it's understandable, that the surfaces c in this position form a kind of airfoil, da, the air currents can pass through between the surfaces, whereby from -the sum of all small areas a large wing is formed.
Die Einrichtung gemäß der Erfindung kann bei allen Flugzeugarten, auch bei solchen zeit mehreren Propellern, Verwendung finden.The device according to the invention can be used in all types of aircraft, even with such a time several propellers are used.
Claims (1)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DEW72446D DE474719C (en) | Airplane with cylinders rotating around transverse axes |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DEW72446D DE474719C (en) | Airplane with cylinders rotating around transverse axes |
Publications (1)
Publication Number | Publication Date |
---|---|
DE474719C true DE474719C (en) | 1929-04-06 |
Family
ID=7609148
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DEW72446D Expired DE474719C (en) | Airplane with cylinders rotating around transverse axes |
Country Status (1)
Country | Link |
---|---|
DE (1) | DE474719C (en) |
-
0
- DE DEW72446D patent/DE474719C/en not_active Expired
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