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Hybrid power system for fixed-wing unmanned aerial vehicle and propelling method

A hybrid power system, unmanned aerial vehicle technology, used in rotorcraft, motor vehicles, unmanned aerial vehicles, etc.

Active Publication Date: 2021-04-27
NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

At present, there are many hybrid power systems suitable for vehicles, but there are few researches on hybrid power systems based on fixed-wing unmanned aerial vehicles, and because the driving forms of automobiles and aircrafts are different, the structure of vehicle-mounted hybrid power systems cannot be copied. The hybrid power system structure and propulsion mode of a fixed-wing unmanned aerial vehicle are very important

Method used

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  • Hybrid power system for fixed-wing unmanned aerial vehicle and propelling method

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Embodiment Construction

[0032] In order to facilitate the understanding of those skilled in the art, the present invention will be further described below in conjunction with the embodiments and accompanying drawings, and the contents mentioned in the embodiments are not intended to limit the present invention.

[0033] refer to figure 1As shown, a hybrid power system for a fixed-wing unmanned aerial vehicle of the present invention includes: a first propulsion motor 1, a first propeller 2, a first ISG motor 3, a first ISG motor clutch 4, a second propeller 5, a power Controller 6, battery pack 7, transmission shaft 8, third propeller 9, second ISG motor clutch 10, second ISG motor 11, fourth propeller 12, second propulsion motor 13, first small bevel gear set 14, transmission Shaft bevel gear set 15, second pinion bevel gear set 16, main propeller 17, main propeller clutch 18, fuel engine 19, transmission shaft clutch 20;

[0034] The first propulsion motor 1 and the second propulsion motor 13 are ...

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Abstract

The invention discloses a hybrid power system for a fixed-wing unmanned aerial vehicle and a propelling method. The system comprises a first propulsion motor, a first propeller, a first ISG motor, a first ISG motor clutch, a second propeller, a power controller, a battery pack, a transmission shaft, a third propeller, a second ISG motor clutch, a second ISG motor, a fourth propeller, a second propulsion motor, a first bevel pinion set, a transmission shaft bevel gear set, a second bevel pinion set, a main propeller, a main propeller clutch, a fuel engine and a transmission shaft clutch. The hybrid power system combines the advantages of fuel propulsion and pure electric propulsion, has multiple hybrid propulsion modes, and can effectively improve the whole voyage of the fixed-wing unmanned aerial vehicle.

Description

technical field [0001] The invention belongs to the technical field of hybrid power systems, and specifically refers to a hybrid power system and a propulsion method for a fixed-wing unmanned aerial vehicle. Background technique [0002] With the continuous development of new energy technology, more forms of power based on new energy have emerged, such as pure electric drive systems using electrochemical batteries, hybrid drive systems using internal combustion Fuel cell drive systems in the form of energy storage, among which the hybrid drive system is the most mature, which is further divided into series hybrid, parallel hybrid and hybrid hybrid. The above-mentioned new energy drive forms have been widely used and developed in vehicles in the past ten years, but as aircraft, especially fixed-wing unmanned aerial vehicles, internal combustion engine propulsion is still the main drive form, so new energy power is used as the propulsion form The fixed-wing unmanned aerial ve...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64D27/02B64D35/04B64D35/08B64C27/28
CPCB64D27/02B64D35/04B64D35/08B64C27/28B64U10/00B64U50/11B64U50/19B64D27/026
Inventor 昌诚程赵万忠周小川齐前锦黄馨谊孙林林薛子宽
Owner NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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