AT50887B - Stabilizing device for flying machines. - Google Patents

Stabilizing device for flying machines.

Info

Publication number
AT50887B
AT50887B AT50887DA AT50887B AT 50887 B AT50887 B AT 50887B AT 50887D A AT50887D A AT 50887DA AT 50887 B AT50887 B AT 50887B
Authority
AT
Austria
Prior art keywords
stabilizing device
flying machines
handlebar
seat
housing
Prior art date
Application number
Other languages
German (de)
Inventor
Jean Georges Ramel
Original Assignee
Jean Georges Ramel
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Jean Georges Ramel filed Critical Jean Georges Ramel
Application granted granted Critical
Publication of AT50887B publication Critical patent/AT50887B/en

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Description

  

   <Desc/Clms Page number 1> 
 



  StabillisierungsvorrichtungfürFlugmaschinen. 



   Die Erfindung hat eine   Stabilisiorungsvorrichtung   für Flugmaschinen mit pendelndem   Ijcnkorsitz   zum Gegenstände und besteht darin, dass der Lenkersitz innerhalb eines mit ihm fest verbundenen kugelförmigen Gehäuses angeordnet ist, das auf Rollen allseits vordrehbar gelagert ist. 



   Es wird hiedurch der Vorteil erzielt, dass der Lenkersitz aus seiner Gewichtslage gebracht, stets unmittelbar in dieselbe wieder zurückkehrt. Bei den bekannten Vorrichtungen   nimmt     der Lonkersitz   erst nach   Vollführung   mehrerer Schwingungen seine Gleichgewichtsstellung ein und war diese grosse Empfindlichkeit die Ursache, dass man bisher in der Praxis von der Verwendung pendelnder Lenkersitze absehen musste. 



   In den in Fig. 1 und 2 der Zeichnung ist der Erfindungsgegenstand in zwei Stellungen beispielsweise dargestellt. 



   Der Lenkersitz 1 ist innerhalb eines kugelförmigen, auf Rollen   15   oder dgl. gelagerten Gehäuseteiles 13 angeordnet, so dass der Lenkersitz stets in der vertikalen Achse Z-Z verbleibt. Zugleinen 9 sind an eine Öse 14 im oberen Teil des kugelförmigen Gehäuses angeschlossen und dienen zur Betätigung der Stabilisierungsflächen und   Ilöhen-   steuer, je   nachdem   der Apparat gegen die horizontale Achse Y-Y oder die vertikale Achse   Z-Z geneigt wird.   Um die Beobachtung von verschiedenen Punkten des   Gehäuses   aus   zn   ermöglichen, sind an geeigneten Stellen des Gehäuses 13 durch Glas, Glimmer, Zelluloid und dgl. verkleidete Öffnungen vorgesehen. 

**WARNUNG** Ende DESC Feld kannt Anfang CLMS uberlappen**.



   <Desc / Clms Page number 1>
 



  Stabilization device for aircraft.



   The invention has a stabilization device for flying machines with a pendulous Ijcnkorsitz for objects and consists in that the handlebar seat is arranged within a spherical housing firmly connected to it, which is mounted on rollers so that it can be rotated on all sides.



   This has the advantage that the handlebar seat is brought out of its weight position and always immediately returns to it. In the known devices, the Lonker seat only assumes its equilibrium position after several oscillations have been carried out, and this great sensitivity was the reason why it was previously necessary to refrain from using swinging handlebar seats in practice.



   In FIGS. 1 and 2 of the drawing, the subject of the invention is shown in two positions, for example.



   The handlebar seat 1 is arranged within a spherical housing part 13 mounted on rollers 15 or the like, so that the handlebar seat always remains in the vertical axis Z-Z. Tension lines 9 are connected to an eyelet 14 in the upper part of the spherical housing and are used to operate the stabilizing surfaces and height control, depending on whether the apparatus is inclined to the horizontal axis Y-Y or the vertical axis Z-Z. In order to enable observation from different points of the housing from zn, openings covered by glass, mica, celluloid and the like are provided at suitable locations on the housing 13.

** WARNING ** End of DESC field may overlap beginning of CLMS **.

 

Claims (1)

PATENT-ANSPRUCH : EMI1.1 EMI1.2 **WARNUNG** Ende CLMS Feld Kannt Anfang DESC uberlappen**. PATENT CLAIM: EMI1.1 EMI1.2 ** WARNING ** End of CLMS field may overlap beginning of DESC **.
AT50887D 1909-02-13 1910-02-09 Stabilizing device for flying machines. AT50887B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR50887X 1909-02-13

Publications (1)

Publication Number Publication Date
AT50887B true AT50887B (en) 1911-11-25

Family

ID=8685841

Family Applications (1)

Application Number Title Priority Date Filing Date
AT50887D AT50887B (en) 1909-02-13 1910-02-09 Stabilizing device for flying machines.

Country Status (1)

Country Link
AT (1) AT50887B (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1128300B (en) * 1959-01-17 1962-04-19 Franz Wirth Stabilizing device for aircraft, in particular gliders

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1128300B (en) * 1959-01-17 1962-04-19 Franz Wirth Stabilizing device for aircraft, in particular gliders

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