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Umbrella-shaped boosting solar aircraft

A technology of aircraft and solar energy, which is applied in the direction of aircraft, current collectors, aircraft control, etc., can solve problems such as insufficient rigidity, bulky, and aircraft powerlessness, and achieve the effects of improving stiffness and stability, increasing initial launch velocity, and reducing launch area

Inactive Publication Date: 2019-11-22
西安长峰机电研究所
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] At present, the aircraft used for reconnaissance and observation mainly include helicopters, airships, etc., such as UAVs with conventional layouts, high-altitude balloons, airships, and conventional UAV systems. They have their own advantages, but most of these aircraft rely on fossil fuels As the main source of power, it is capable of performing short-distance, short-range and low-altitude missions with ease, but in the face of higher mission requirements, such as ultra-long air time, ultra-long flight distance, etc., due to the long-term stable and efficient energy supply conditions Constrained by traditional aircraft, it seems powerless
In order to solve the above problems, in the last century, many domestic and foreign scientists began to study solar aircraft, and related technologies have achieved remarkable results, such as the "Sun Challenger" and "Helios" aircraft developed by the United States, and the "Sun God" aircraft developed by the United Kingdom. "Western Wind 3" aircraft, etc. Domestic representatives include "Soarer" aircraft, "Green Pioneer" aircraft, etc., but limited by the conversion efficiency of photovoltaic cells, in order to obtain a larger lighting area, the existing solar aircraft still use large Aspect ratio structure, which directly leads to increased flexibility and insufficient rigidity of the aircraft structure, which seriously affects the flight safety of the aircraft
In order to fundamentally solve the problems of low structural rigidity, bulky volume, inconvenient storage, recovery and launch of solar-powered aircraft, as well as the low efficiency of response to emergencies and emergencies, there is an urgent need for a solar-powered aircraft that can meet the needs of Requirements such as rapidity and convenient recycling

Method used

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Embodiment Construction

[0023] The present invention will be further described below in conjunction with the accompanying drawings and embodiments, and the present invention includes but not limited to the following embodiments.

[0024] The aircraft of the present invention is mainly composed of a rocket engine, an aircraft body, a solar film, a coaxial double-rotor mechanism, an energy storage battery, a power management system, a load system and the like. Before launch, it looks like a rocket with dual rotors at the front end. The rocket engine pushes the aircraft to a certain height, releases the contraction and tightening mechanism of the umbrella-shaped solar aircraft, and the solar umbrella opens. Then, the rocket engine falls off, and the umbrella-shaped aircraft begins to use solar energy. Work.

[0025] The structure of the aircraft body is as figure 1 As shown, the working principle of the connecting rod is used to push the connecting rod to move through the spring to realize the folding ...

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Abstract

The invention provides an umbrella-shaped boosting solar aircraft. The aircraft comprises an aircraft body, a rocket engine, a solar film, a coaxial double-rotor mechanism, an energy storage battery and an umbrella-shaped retractable structure; the coaxial double-rotor mechanism is installed at the upper end of the aircraft body, the rocket engine is installed at the lower end of the aircraft body, the umbrella-shaped retractable structure is installed outside the middle section, and the energy storage battery is installed inside the aircraft body; the umbrella-shaped retractable structure isclung to the outer wall of the aircraft body when being folded, is conical when being unfolded and is coaxial with the aircraft body; and the solar film covers the upper surface of the umbrella-shapedretractable structure and supplies power to the energy storage battery. The launching initial speed can be increased, the initial loss energy is reduced, the variable structure design of the aircraftis realized, and the aircraft is more convenient to launch, recover and store.

Description

technical field [0001] The invention relates to a solar-powered aircraft and belongs to the technical field of testing and testing. . Background technique [0002] Solar aircraft technology has broad application prospects, such as aerial fixed-point observation, reconnaissance, early warning, interceptors, high-altitude radar stations, communication relays, border patrols, electronic warfare, battlefield monitoring, atmospheric satellites, environmental and disaster monitoring, and even anti- Guide and so on. [0003] At present, the aircraft used for reconnaissance and observation mainly include helicopters, airships, etc., such as UAVs with conventional layouts, high-altitude balloons, airships, and conventional UAV systems. They have their own advantages, but most of these aircraft rely on fossil fuels As the main source of power, it is capable of performing short-distance, short-range and low-altitude missions with ease, but in the face of higher mission requirements, ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C39/02B64C27/10B64C19/00B64D27/02B64D27/24B64F1/04H02J7/35H02S20/32
CPCB64C39/02B64C27/10B64C19/00B64D27/023B64D27/24B64F1/04H02S20/32B64D27/026Y02E10/50
Inventor 鲁静王宏涛王海峰
Owner 西安长峰机电研究所
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