AT73964B - Plane. - Google Patents
Plane.Info
- Publication number
- AT73964B AT73964B AT73964DA AT73964B AT 73964 B AT73964 B AT 73964B AT 73964D A AT73964D A AT 73964DA AT 73964 B AT73964 B AT 73964B
- Authority
- AT
- Austria
- Prior art keywords
- control
- hollow
- plane
- propeller
- cords
- Prior art date
Links
Landscapes
- Seal Device For Vehicle (AREA)
Description
<Desc/Clms Page number 1>
Flugzeug.
Gegenstand vorliegender Erfindung bezieht sich auf ein Flugzeug, das sich von den bekannten, ähnlichen Einrichtungen dadurch wesentlich und vorteilhaft unterscheidet, dass das Steuer und der Propeller auf einer hohlen Stahlstange gelagert sind.
Die Steuerschnt1re liegen in dieser durchgehenden hohlen Propellerwelle und führen vom Steuer zum Sitz des Flugzeugführers. Die Durchführung der Steuerschnüre durch die Steuerwelle gewährt den erheblichen Vorteil, dass diese Schnüre vollständig geschützt liegen und eine verhältnismässig sehr einfache Anordnung derselben möglich ist. Es werden insbesondere die bei den sonstigen Steueranordnungen unbedingt notwendigen, verschiedenen Richtungsänderungen und dazu dienenden Rollenführungen der Steuerachntlre erspart.
Auf der Zeichnung ist eine schematische Darstellung eines Zweideckers nach vorliegender Erfindung gezeigt. Es bedeuten 1 und 2 die Tragflächen, 3 das Chassis, durch das eine hohle Achse 4 hindurchgeht. Auf dieser hohlen Achse sitzt der Propeller 5 und der Schwanz 6. Dieser letztere ist bei der dargestellten Ausführungsform auf einem Querrahmen befestigt und auf der hohlen Stahlachse 4 nicht drehbar. Der Schwanz 6 wird durch Schnüre 7, die durch die hohle Achse 4 hindurchgeführt sind, in seiner Lage gehalten und zur Steuerung entsprechend bewegt.
**WARNUNG** Ende DESC Feld kannt Anfang CLMS uberlappen**.
<Desc / Clms Page number 1>
Plane.
The subject of the present invention relates to an aircraft which differs from the known, similar devices essentially and advantageously in that the control and the propeller are mounted on a hollow steel rod.
The control doors lie in this continuous hollow propeller shaft and lead from the controls to the pilot's seat. The implementation of the control cords through the control shaft provides the considerable advantage that these cords are completely protected and a relatively very simple arrangement of the same is possible. In particular, the various changes of direction that are absolutely necessary for the other control arrangements and the roller guides for the rear control are saved.
The drawing shows a schematic representation of a two-decker according to the present invention. 1 and 2 mean the wings, 3 the chassis through which a hollow axle 4 passes. The propeller 5 and the tail 6 are seated on this hollow axis. In the embodiment shown, the latter is fastened to a transverse frame and cannot be rotated on the hollow steel axis 4. The tail 6 is held in its position by cords 7 which are passed through the hollow axle 4 and moved accordingly for control.
** WARNING ** End of DESC field may overlap beginning of CLMS **.
Claims (1)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE73964X | 1912-10-11 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| AT73964B true AT73964B (en) | 1917-11-10 |
Family
ID=5636619
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| AT73964D AT73964B (en) | 1912-10-11 | 1913-10-10 | Plane. |
Country Status (1)
| Country | Link |
|---|---|
| AT (1) | AT73964B (en) |
-
1913
- 1913-10-10 AT AT73964D patent/AT73964B/en active
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