Photodynamic aircraft

A technology of aircraft and light power, which is applied in the direction of aircraft, aerospace vehicles, power supply systems of aerospace vehicles, etc., and can solve problems such as unsuitable for vehicles and low photoelectric conversion efficiency

Inactive Publication Date: 2016-05-25
刘南林
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  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Existing solar energy utilization technology, such as photovoltaic power generation technology, due to the low photoelectric conversion efficiency, usually only about 15%, therefore requires the use of large-area photovoltaic panels to provide electrical energy, which is not yet suitable as a vehicle energy source

Method used

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Embodiment approach

[0009] A light-powered aircraft is composed of four parts: a light-to-heat conversion system, a composite power system, a spherical hull, and an automatic control system. It can be used for both unmanned and manned navigation. The specific optimized implementation methods are as follows:

[0010] The light-to-heat conversion system consists of a number of quartz glass concentrating lens sheets (1) embedded on the surface of the spherical hull with a high-temperature-resistant diamond-like film deposited on the surface, and a high-temperature ball made of metal molybdenum located in the focal point range of the light beam of the concentrating lens sheet (1). (2), the liquid metal lithium stored in the high temperature ball (2) is used as a high heat capacity carrier (3), and the hollow vaporization made of metal titanium that is located in the center of the high temperature ball (2) and the high temperature ball (2) has a common spherical center The ball (4), the spherical stora...

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Abstract

The invention provides a photodynamic aircraft. By a sunlight focusing method, light energy is converted into heat energy and is stored into a carrier with high heat capacity as a spherical launch vehicle of power energy, so that the dead-weight and the size can be reduced, the cruising ability and the effective load are improved, and amphibious operation in an outer space and an atmosphere space can be achieved. The photodynamic aircraft is characterized by comprising four parts, namely a photothermal conversion system, a composite power system, a spherical hull and an automatic control system. The technology belongs to the field of a launch vehicle. On one hand, the spherical hull of the aircraft is beneficial to collection of sunlight at different angles; and on the other hand, the spherical hull has motion stability and steering flexibility. A power bin is in a vacuum state internally, is beneficial to thermal insulation and is used for mounting the photothermal conversion system and the composite power system to reduce the heat loss of the carrier with high heat capacity. A work bin is used for mounting an operation room and launching equipment. The photodynamic aircraft is capable of carrying out unmanned automatic aviation and manned aviation, and can be taken as a spacecraft, an aircraft and a recoverable satellite.

Description

1. Technical field [0001] A photodynamic aircraft is a spherical vehicle that uses the method of focusing sunlight to convert light energy into heat and store it in a carrier with high heat capacity as a power source. It can not only reduce its weight and volume, increase its endurance and payload, but also Amphibious operations in space and atmospheric space can be realized. It is characterized by four parts: a light-to-heat conversion system, a composite power system, a spherical hull, and an automatic control system. The aircraft adopts isolation boards to divide the spherical hull into a power cabin and a working cabin; the power cabin is in a vacuum state, which is conducive to heat insulation, and is used to install the light-to-heat conversion system and the composite power system to reduce the heat loss of high heat capacity carriers; the working cabin Used to house the operator's cabin and carry equipment. On the one hand, the spherical hull is conducive to collecti...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64G1/44B64G1/42
CPCB64G1/446B64G1/42B64G1/427
Inventor 刘南林
Owner 刘南林
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