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Wingless aircraft

An instrument and wing technology, which is applied in the field of flight instruments without wings, can solve problems such as limited availability, infeasible panoramic images, and inappropriateness.

Active Publication Date: 2018-10-23
思飞锐有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] For this reason, the flying instruments known from the prior art are not suitable for taking and producing panoramas, for example, when flying close to buildings, when flying over buildings or, for example, also flying over trees or the like , since the object to be imaged is often outside the field of view of the camera in this type of recording, so that the object can only be partially imaged accordingly, and at each point in time of the flyby The generation of a complete panoramic picture of the surroundings of the above-mentioned flight instruments is not feasible or is only feasible to a limited extent

Method used

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Embodiment Construction

[0040] exist Figure 1a and 1b A wingless aircraft 1 with four lift rotors 3 driven by electric motors and rotating about different rotor axes 2 is schematically shown in FIG. The aircraft 1 has two camera units 4 for capturing panoramic images.

[0041] The camera unit 4 and the lift rotor 3 are arranged and oriented relative to each other such that the smallest, spherical rotor envelope 5 enclosing all lift rotors 3 has a larger ratio than the smallest spherical camera envelope Line 6 has a large volume, the camera envelope enclosing all camera lens 7 of camera mechanism 4 . The camera unit 4 expands a field of view, wherein the field of view surrounds the entire aircraft 1 in order to be able to detect the entire surroundings of the aircraft 1 . The lift rotor 3 is outside the viewing space. Furthermore, the distance 8 between the lenses of the two camera units 4 is smaller than the distance 9 between the two lift rotors 3 arranged opposite one another. In the flight i...

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Abstract

The invention relates to a wingless aircraft (1) having a plurality of lifting rotors (3) which are driven by electric motor and rotate about various rotor axes (2). The aircraft (1) has at least oneenergy store (21) for making available the electrical energy necessary to operate the lifting rotors (3), at least one control device (22) for actuating the lifting rotors (3) and for communication with a ground station and at least two camera devices (4) for detecting a panorama image. An extremely small, spherical rotor envelope (5) which encloses all the lifting rotors (3) has a larger volume than an extremely small spherical camera envelope (6) which encloses camera lenses (7) of all the camera devices (4). The camera devices (4) extend over a field of vision, wherein the field of vision surrounds the entire aircraft (1), and wherein the lifting rotors (3) lie outside the field of vision.

Description

technical field [0001] The invention relates to a wingless aircraft having a plurality of lift rotors driven by electric motors and rotating about different rotor axes, wherein the aircraft has at least one energy store For supplying the electrical energy necessary for operating the lift rotor, at least one control device for actuating the lift rotor and for communicating with a ground station, and at least two camera devices for detecting panoramic images. Background technique [0002] Such an unmanned and remotely controlled aerial vehicle from the ground station, such as a quadcopter, is used to generate an aerial image panorama. For this purpose, in known aircraft devices, a plurality of camera units are usually arranged on the frame of the aircraft device, wherein the camera units are arranged as far as possible such that the field of view of the camera units is relative to all The flying devices are spaced one above the other so that the entire surroundings of the fly...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C39/02H04N23/90
CPCG03B15/006H04N23/698H04N23/90B64U10/13B64U30/20B64U50/19B64U2101/30B64U20/87
Inventor J.黑塞尔巴特N.奇巴克
Owner 思飞锐有限公司
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