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AT49705B - Airplane. - Google Patents

Airplane.

Info

Publication number
AT49705B
AT49705B AT49705DA AT49705B AT 49705 B AT49705 B AT 49705B AT 49705D A AT49705D A AT 49705DA AT 49705 B AT49705 B AT 49705B
Authority
AT
Austria
Prior art keywords
wing
airplane
desc
strips
fan
Prior art date
Application number
Other languages
German (de)
Inventor
Ludwig Schmidl
Original Assignee
Ludwig Schmidl
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 Ludwig Schmidl filed Critical Ludwig Schmidl
Application granted granted Critical
Publication of AT49705B publication Critical patent/AT49705B/en

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/38—Adjustment of complete wings or parts thereof
    • B64C3/54—Varying in area

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Supports For Plants (AREA)
  • On-Site Construction Work That Accompanies The Preparation And Application Of Concrete (AREA)
  • Toys (AREA)

Description

  

   <Desc/Clms Page number 1> 
 



    A e r 0 p I a n.   



   Vorliegende Erfindungbetrifft einen Aeroplan, bei welchem die   Trag-bezw. Steuerflächen   zwecks Lenkung bezw. Steuerung an den Aussenseiten mit fächerförmig einzieh- und ausstreck- 
 EMI1.1 
 miteinander durch   Geienkstangen derart   verbunden sind, dass sie sich bei   Betätigung des Flügels     paraHe ! zueinander   in der richtung ihrer Ebene verschieben und beim Einziehen desselben 
 EMI1.2 
   fächerartig auseinander schiebbaren Streifen bestehen, der Vorteil erreicht, dass der iStirnwiderstand   sowohl im ausgebreiteten, als auch im eingezogenen Zustande des Flügels wesentlich vermindert   wird.

   Ferners wird   der Einfallswinkel des der Wölbung der Tragfläche angepassten Flügels bei 
 EMI1.3 
 ziehen eine Änderung ihrer Lage in bezug auf die   Tragfläche   erfahren. 



   In der Zeichnung sind zwei Ausführungsbeispiele   dieser Faltflügel   an einem   Eindecken   veranschaulicht. Nach der in Fig. 1, 3 und 4 dargestellten Ausführungsform des Flügels sind die Flächen- 
 EMI1.4 
 Schmalseite der Tragfläche jede für sich um 19, 20, 21 in der Ebene desselben drehbar gelagert. Diese Streifen sind durch eine Anzahl Querstangen 2 gelenkig miteinander verbunden, so dass 
 EMI1.5 
 
 EMI1.6 
 

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



   <Desc / Clms Page number 1>
 



    A e r 0 p I a n.



   The present invention relates to an airplane, in which the support respectively. Control surfaces for the purpose of steering respectively. Control on the outside with fan-shaped pull-in and stretch-out
 EMI1.1
 are connected to each other by pivot rods in such a way that they are paraHe! move to each other in the direction of their plane and when pulling the same
 EMI1.2
   There are strips that can be pushed apart like a fan, the advantage that the frontal resistance is significantly reduced both in the expanded and in the retracted state of the wing.

   Furthermore, the angle of incidence of the wing adapted to the curvature of the wing is at
 EMI1.3
 draw a change in their position in relation to the wing.



   In the drawing, two exemplary embodiments of these folding wings are illustrated on a covering. According to the embodiment of the wing shown in Fig. 1, 3 and 4, the surface
 EMI1.4
 The narrow side of the wing is mounted rotatably by 19, 20, 21 in the plane of the same. These strips are articulated to one another by a number of cross bars 2 so that
 EMI1.5
 
 EMI1.6
 

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

Claims (1)

**WARNUNG** Ende CLMS Feld Kannt Anfang DESC uberlappen**. ** WARNING ** End of CLMS field may overlap beginning of DESC **.
AT49705D 1910-04-09 1910-04-09 Airplane. AT49705B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
AT49705T 1910-04-09

Publications (1)

Publication Number Publication Date
AT49705B true AT49705B (en) 1911-09-11

Family

ID=3570468

Family Applications (1)

Application Number Title Priority Date Filing Date
AT49705D AT49705B (en) 1910-04-09 1910-04-09 Airplane.

Country Status (2)

Country Link
AT (1) AT49705B (en)
GB (1) GB191108911A (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111959746B (en) * 2020-08-31 2022-10-11 哈尔滨工业大学 Parallel connecting rod type deformation wing framework

Also Published As

Publication number Publication date
GB191108911A (en) 1911-05-25

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