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Power supply system and aircraft

A technology of power supply system and electrical appliances, which is applied in the direction of collectors, DC power supply parallel operation, photovoltaic power generation, etc., can solve the problems of being easily affected by the environment, difficult to maintain long-term flight, and reducing the flight stability of aircraft, so as to achieve the expansion of application Environment, improved battery life, and economical usage effects

Pending Publication Date: 2018-11-27
DONGHAN SOLAR UAV TECH CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

However, when relying solely on the solar power supply system to power the aircraft, the flight of the aircraft is easily affected by the environment. This improves the flight stability of the aircraft; while relying solely on the battery power supply system to power the aircraft, due to the limited energy storage of the aircraft's onboard batteries, it is difficult to maintain long-term flight

Method used

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  • Power supply system and aircraft
  • Power supply system and aircraft
  • Power supply system and aircraft

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Embodiment Construction

[0041] Example embodiments will now be described more fully with reference to the accompanying drawings. Example embodiments may, however, be embodied in many forms and should not be construed as limited to the embodiments set forth herein; rather, these embodiments are provided so that this disclosure will be thorough and complete, and will fully convey the concept of example embodiments to those skilled in the art. The same reference numerals in the drawings denote the same or similar structures, and thus their detailed descriptions will be omitted.

[0042] Although relative terms such as "upper" and "lower" are used in this specification to describe the relative relationship of one component of an icon to another component, these terms are used in this specification only for convenience, for example, according to the description in the accompanying drawings directions for the example described above. It will be appreciated that if the illustrated device is turned over so...

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Abstract

The application relates to the technical field of new energy, and in particular to a power supply system and an aircraft. The power supply system comprises a solar power supply device, a fuel cell power supply device, and an electric energy control mechanism; and the electric energy control mechanism, which is connected to the solar power supply device and the fuel cell power supply device, is soarranged as to control the electric on-state between each of the solar power supply device and the fuel cell power supply device and an electricity-consuming device. The technical solution not only can enable the aircraft to stably fly under different light environments, but also can increase the endurance of the aircraft.

Description

technical field [0001] The present application relates to the field of new energy technology, in particular, to a power supply system and an aircraft. Background technique [0002] At present, most drones and other aircraft use a single power supply system to power them to realize their own flight. For example, a solar power supply system or a battery power supply system alone are used to power the aircraft. However, when relying solely on the solar power supply system to power the aircraft, the flight of the aircraft is easily affected by the environment. This improves the flight stability of the aircraft; and when relying solely on the battery power supply system to power the aircraft, it is difficult to maintain long-term flight due to the limited energy storage of the onboard battery of the aircraft. [0003] It should be noted that the information disclosed in the above background technology section is only used to enhance the understanding of the background of the ap...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): H02J1/10H02J7/35H02J9/06H02S10/10
CPCH02J1/10H02J7/35H02J9/06H02S10/10H02J2300/30Y02E10/50Y02B10/70Y02B90/10
Inventor 冯昆
Owner DONGHAN SOLAR UAV TECH CO LTD