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Aircraft, preferably unmanned

A technology of unmanned and aircraft, applied in the field of aircraft, can solve the problems of cumbersome take-off preparations, etc., and achieve the effect of increasing effective flight time, improving performance, maneuvering ability and maneuvering characteristics

Inactive Publication Date: 2015-02-18
QUANTUM SYST GMBH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

But preparation for takeoff is very cumbersome due to the necessary catapults or infrastructure in the form of a takeoff runway

Method used

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  • Aircraft, preferably unmanned
  • Aircraft, preferably unmanned
  • Aircraft, preferably unmanned

Examples

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Embodiment Construction

[0068] A preferred exemplary embodiment is described below with the aid of the drawings. Identical, similar or identically acting components are identified with the same reference numerals and in order to avoid redundant descriptions, a repeated description of these components will be partially omitted in the following description.

[0069] exist Figure 1 to Figure 3 An aircraft according to an embodiment of the present invention is schematically shown in top view, side view and front view. The aircraft 1 comprises an aerodynamic fixed wing 2 constructed in a known manner. The fixed wing 2 is a wing optimized for aerodynamic flight. Starting from a certain speed, for example, 50 km / h, the wing can provide the lift required for the dynamic forward flight of the entire aircraft 1 .

[0070] The wing 2 includes an outer wingtip 20 and a connection region 22 on the fuselage 3 of the aircraft 1 . Furthermore, the ailerons 24 serve to control the aircraft with respect to the rol...

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Abstract

The invention relates to an aircraft (1), preferably an unmanned aircraft (UAV), drone, or unmanned aerial system (UAS), comprising a rigid wing (2), which enables aerodynamic horizontal flight, and at least four rotors (4, 4'), which are driven by means of controllable electric motors (5) and which can be pivoted between a vertical starting position and a horizontal flight position by means of a pivoting mechanism (7), wherein all electric motors (5) and rotors (4) are arranged on the wing (2).

Description

technical field [0001] The present invention relates to an aircraft, preferably an unmanned aerial vehicle (UAV, Unmanned Aerial Vehicle), a drone and / or an unmanned aerial system (UAS, Unmanned Aerial System). Background technique [0002] In the field of unmanned aerial vehicles, drones and / or unmanned aerial systems different designs are known for take-off and landing of such aircraft. It is known, for example, that the drone is designed as a conventional flat plane with fixed wings and is launched by means of a catapult. Since the aircraft has high aerodynamic characteristics, the effective flight time that the aircraft can achieve is very long. However, preparation for take-off is very cumbersome due to the necessary infrastructure in the form of catapults or take-off runways. The landing of this aircraft also needs to be prepared, because it needs to land on the runway, or it needs to land in the receiving net or on the parachute. [0003] There is also known a dron...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C29/00B64C39/02B64D27/24
CPCB64C29/0033B64D27/24Y02T50/62B64C2201/042B64C39/024B64C2211/00Y02T50/60B64U50/19B64U30/10B64U30/297B64U10/20B64U10/25B64U50/13B64U30/293B64U2101/31
Inventor 弗洛里安·塞贝尔米夏埃尔·沃尔法特米夏埃尔·克里格尔
Owner QUANTUM SYST GMBH
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