DE572758C - Airplane for lift and plan flight with separate control surfaces for both types of flight - Google Patents

Airplane for lift and plan flight with separate control surfaces for both types of flight

Info

Publication number
DE572758C
DE572758C DEN31326D DEN0031326D DE572758C DE 572758 C DE572758 C DE 572758C DE N31326 D DEN31326 D DE N31326D DE N0031326 D DEN0031326 D DE N0031326D DE 572758 C DE572758 C DE 572758C
Authority
DE
Germany
Prior art keywords
flight
control surfaces
lift
types
airplane
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
Application number
DEN31326D
Other languages
German (de)
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
JACOB EMIL NOEGGERATH DR ING
Original Assignee
JACOB EMIL NOEGGERATH DR ING
Publication date
Priority to DEN31326D priority Critical patent/DE572758C/en
Application granted granted Critical
Publication of DE572758C publication Critical patent/DE572758C/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers

Landscapes

  • Engineering & Computer Science (AREA)
  • Automation & Control Theory (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Toys (AREA)

Description

Flugzeuge für Hub- und Planflug, bei denen für den Antrieb beider Flugarten verschieden angeordnete Propeller oder in verschiedene Lagen einstellbare Propeller vorgesehen sind und die Steuerung des Flugzeuges im Hub- und* Planfhig durch gesonderte Steuerflächen erfolgt, sind bekannt. Um nun bei dieser Anordnung die Bedienung der Steuerung möglichst zu vereinfachen, werden gemäß der vorliegenden Erfindung die einander in ihrer Wirkung entsprechenden Steuerflächen für den Hub- und Planflug, also einerseits die beiden Höhensteuer und anderseits die beiden Seitents Steuer, durch denselben Steuerhebel betätigt. In den Abbildungen ist ein Ausführungsbeispiel. der Erfindung dargestellt.Airplanes for lift and plan flight, which are different for the propulsion of both types of flight arranged propellers or propellers adjustable in different positions are provided are and the control of the aircraft in the lifting and * plan capable by separate Control surfaces done are known. In order to simplify the operation of the control as much as possible with this arrangement, according to the present invention, the mutually corresponding in their effect Control surfaces for the vertical and planar flight, so on the one hand the two elevation controls and on the other hand the two side panels Steering wheel operated by the same joystick. In the figures is an exemplary embodiment. of the invention shown.

Abb. ι zeigt die Anordnung und Betätigung der Steuerflächen für die Höhensteuerung, Fig. Ι shows the arrangement and operation of the control surfaces for the height control,

Abb. 2 diejenige für die Seitensteuerung. Beim Planflug wirkt das Höhensteuer 1 und das Seitensteuer 2, beim Hubflug das Höhensteuer 3 und das Seitensteuer 4. Die Steuerflächen 1 und 2 sind in der üblichen Weise am Schwanzende des Flugzeuges angebracht. Die Steuerfläche 3 befindet sich an der Seite des Rumpfes und die Steuerfläche 4 unterhalb des Rumpfes. Außer diesen Steuerflächen ist noch eine Stabilisierungsfläche 5 am vorderen Ende des Flugzeuges vorgesehen. Bei der dargestellten Anordnung sind die Höhensteuer und die Seitensteuer durch den Steuerhebel 6 in derselben Weise betätigt. .Fig. 2 the one for the side controls. Elevation control 1 is effective during plan flight and the rudder 2, the elevator 3 and the rudder 4 during lift flight Control surfaces 1 and 2 are attached to the tail end of the aircraft in the usual manner. The control surface 3 is on the side of the fuselage and the control surface 4 is below the fuselage. Except for these Control surfaces is also a stabilization surface 5 at the front end of the aircraft intended. In the arrangement shown, the elevator rudder and the rudder rudder are the rudder operated by the control lever 6 in the same way. .

Claims (1)

Patentanspruch:Claim: Flugzeug für Hub- und Planflug mit gesonderten Steuerflächen für beide Flugarten, dadurch gekennzeichnet, daß die einander in ihrer Wirkung entsprechenden Steuerflächen für den Hub- und Planflug durch denselben Steuerhebel betätigt werden.Airplane for lift and plan flight with separate control surfaces for both types of flight, characterized in that the control surfaces corresponding to one another in their effect for the lifting and planing flight operated by the same control lever. Hierzu ι Blatt ZeichnungenFor this purpose ι sheet of drawings
DEN31326D Airplane for lift and plan flight with separate control surfaces for both types of flight Expired DE572758C (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
DEN31326D DE572758C (en) Airplane for lift and plan flight with separate control surfaces for both types of flight

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DEN31326D DE572758C (en) Airplane for lift and plan flight with separate control surfaces for both types of flight

Publications (1)

Publication Number Publication Date
DE572758C true DE572758C (en) 1933-04-05

Family

ID=7345932

Family Applications (1)

Application Number Title Priority Date Filing Date
DEN31326D Expired DE572758C (en) Airplane for lift and plan flight with separate control surfaces for both types of flight

Country Status (1)

Country Link
DE (1) DE572758C (en)

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