AT86828B - Rigid airship with several side wing cells in a row. - Google Patents
Rigid airship with several side wing cells in a row.Info
- Publication number
- AT86828B AT86828B AT86828DA AT86828B AT 86828 B AT86828 B AT 86828B AT 86828D A AT86828D A AT 86828DA AT 86828 B AT86828 B AT 86828B
- Authority
- AT
- Austria
- Prior art keywords
- row
- wing cells
- side wing
- several side
- rigid airship
- Prior art date
Links
Description
<Desc/Clms Page number 1>
Starrluftschiff mit mehreren seitlichen Tragfläehenzellen hintereinander.
EMI1.1
darin, dass neben der üblichen als Boot dienenden Mittelgondel noch mit den Tragflächenzellen verbundene ungefähr in der Höhe der Mittelgondel befindliche Seitenschwimmer vorgesehen sind.
Die Erfindung ist in der Zeichnung beispielsweise dargestellt, und zwar zeigt -Fig. i eine Seitenansicht eines Luftfahrzeuges gemäss vorliegender Erfindung.
Fig. 2 ist eine Draufsicht.
Fig. 3 ist eine Endansicht.
Das dargestellte Seeluftfahrzeug besteht aus einem einheitlichen mittleren Gasbehälter a mit drei Paaren seitlicher Flächensätze b, c, d, die jede aus drei Decken zusammengesetzt sind. Ausser dem Bootskörper e sind besondere Hilfsschwimmer f und g angeordnet, die unter jedem Tragflächensatz liegen und mit den Tragflächen starr verbunden sind. Das Luftfahrzeug besitzt Propeller h und wie üblich Höhen- und Seitensteuer i und k.
Die Anzahl der Flächen, ihre Ausbildung und ihre Anordnung am Rumpf können nach den jeweiligen Erfordernissen gewählt werden. Gegebenenfalls kann eine Mehrzahl Gasbehälter Anwendung finden. Zusammen mit den üblichen Zug-oder Druckpropellern können
Hubschrauben benutzt werden.
**WARNUNG** Ende DESC Feld kannt Anfang CLMS uberlappen**.
<Desc / Clms Page number 1>
Rigid airship with several side wing cells in a row.
EMI1.1
in that, in addition to the usual central pod, which is used as a boat, there are side floats connected to the wing cells approximately at the height of the central pod.
The invention is shown in the drawing, for example, namely shows -Fig. i a side view of an aircraft according to the present invention.
Fig. 2 is a plan view.
Figure 3 is an end view.
The sea aircraft shown consists of a uniform central gas container a with three pairs of lateral sets of surfaces b, c, d, each composed of three blankets. In addition to the hull e, special auxiliary floats f and g are arranged, which lie under each wing set and are rigidly connected to the wings. The aircraft has propellers h and, as usual, elevator and rudder controls i and k.
The number of surfaces, their training and their arrangement on the fuselage can be selected according to the respective requirements. If necessary, a plurality of gas containers can be used. Together with the usual push or pull propellers
Lifting screws are used.
** WARNING ** End of DESC field may overlap beginning of CLMS **.
Claims (1)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB86828X | 1919-04-04 |
Publications (1)
Publication Number | Publication Date |
---|---|
AT86828B true AT86828B (en) | 1921-12-27 |
Family
ID=9857210
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
AT86828D AT86828B (en) | 1919-04-04 | 1920-04-10 | Rigid airship with several side wing cells in a row. |
Country Status (1)
Country | Link |
---|---|
AT (1) | AT86828B (en) |
-
1920
- 1920-04-10 AT AT86828D patent/AT86828B/en active
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