Aircraft and flying method thereof

A technology for aircrafts and rotors, which is applied to aircrafts, rotorcraft, power plants, etc., and can solve problems such as small flight range, small take-off load, and slow level flight speed

Inactive Publication Date: 2017-04-26
杜兴
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Such UAVs have disadvantages such as small take-off load, small flight range, and slow level flight speed.

Method used

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  • Aircraft and flying method thereof
  • Aircraft and flying method thereof
  • Aircraft and flying method thereof

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Embodiment Construction

[0039] The present invention will now be described in detail with reference to exemplary embodiments of the invention. However, the present invention is not limited to the embodiments described here, but it can be embodied in many different forms. The described embodiments are only intended to make this disclosure thorough and complete, and fully convey the concept of the present invention to those skilled in the art.

[0040] figure 1 is a schematic structural diagram of an aircraft 100 according to an embodiment of the present invention. The aircraft 100 may be, for example, an unmanned aerial vehicle, or a manned aircraft. exist figure 1 In the illustrated embodiment, aircraft 100 includes six powerplants, two of which are fuel powered and four of which are electric. The two fuel power devices are composed of maneuvering rotors 102a and 102b and fuel engines 103a and 103b driving the maneuvering rotors 102a and 102b respectively. The four electric power devices are res...

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Abstract

The invention provides an aircraft and a flying method thereof. The aircraft is provided with a plurality of power devices. The plurality of power devices comprise fuel power devices and electric power devices; the fuel power devices are driven by a fuel engine; the electric power devices comprise electric rotors driven by an electric motor; and the propelling directions of the fuel power devices are substantially vertical to rotation planes of the electric rotors so that the aircraft can vertically fly through simultaneous working of the fuel power devices and the electric power devices. As the aircraft simultaneously includes the fuel power devices and the electric rotors, the aircraft can bear heavy objects and can easily and accurately control the balance and posture of the aircraft. Optionally, the aircraft further comprises a fixed wing and the fixed wing is substantially parallel to the propelling directions of the plurality of power devices; therefore, at least partial power devices, including the fuel power devices, of the plurality of power devices can be matched with the fixed wing to realize flat flight of the aircraft.

Description

technical field [0001] The invention relates to an aircraft and a flying method thereof. Background technique [0002] Current drones usually use rotors for vertical takeoff and level flight, and usually use electric motors to drive the rotors, and the power is provided by batteries. Such unmanned aerial vehicles have the disadvantages of small take-off load, short flight range, and slow level flight speed. Contents of the invention [0003] In view of the above problems, the present invention provides an aircraft (for example, a drone or a small manned aircraft) driven by a fuel engine and an electric motor. Further, the present invention also provides an aircraft including rotors and fixed wings. This aircraft can not only take off and land vertically like a common helicopter, but also can fly level-off like a common fixed-wing aircraft. Specifically, embodiments of the present invention provide the following technical solutions. [0004] According to one aspect of th...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C27/08B64C27/26B64D27/02
CPCB64C27/08B64C27/26B64D27/02B64D2027/026
Inventor 杜兴
Owner 杜兴
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