Novel fuel cell and hydrogen and oxygen producing device and aircraft loaded with fuel cell

A fuel cell and aircraft technology, applied in the direction of fuel cell additives, etc., can solve the problems of unreachable, low energy conversion efficiency, and inability to output high-power or ultra-high-power electrical energy.

Inactive Publication Date: 2016-02-24
任立峰
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0005] (1) The obvious disadvantage of this technology is that the absorbing and dispersing solar energy device still continues the original dispersion, does not effectively gather solar energy, and does not have the physical and chemical effects of the concentrated state
The solar energy itself radiates to the earth with low density, dispersion, and time constraints such as day and night, and is affected by spatial location such as regional altitude and climate, and cannot provide basic energy in a timely, stable and intensive manner.
[0006] (2) Althoug

Method used

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  • Novel fuel cell and hydrogen and oxygen producing device and aircraft loaded with fuel cell
  • Novel fuel cell and hydrogen and oxygen producing device and aircraft loaded with fuel cell
  • Novel fuel cell and hydrogen and oxygen producing device and aircraft loaded with fuel cell

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Effect test

Embodiment 1

[0060] like figure 1 As shown, the fuel cell described in this application includes four independent unit working cylinders in series, and the working medium 1 is housed in the unit working cylinders, and a pair of double-layer plate platinum electrodes 3 and a gas supply device 5 are provided to supply gas The device 5 can be fixed on the structure of the double-layer plate platinum electrode 3 by means of adhesion or the like. At the same time, the double-layer plate platinum electrode 3 and the gas supply device 5 are immersed below the liquid level of the working medium 1, and the gas supply device 5 is connected with the external gas storage and supply device, and the negative electrode and the positive electrode of the platinum electrode are respectively supplied to the platinum electrode through the gas supply device 5. Provide fuel hydrogen and oxygen. Adjacent unit working cylinders are connected in series through adjacent positive and negative platinum electrodes in...

Embodiment 2

[0065] In the concentration thermochemical production of hydrogen and oxygen of the present application, a solar energy heat collection device is also provided, and the solar energy device includes a concave heat collector, the inner wall of which is coated with a fluorescent alloy material layer. Preferably, the material used for the fluorescent metal material layer is any one of zinc sulfide and cadmium sulfide. The two fluorescent materials have a very good effect of collecting heat. Preferably, the inner wall of the concave heat collector is densely covered with small concave bodies. Preferably, the concave heat collector is a double-layer vacuum structure. The double-layer vacuum structure is a structure made of two layers of material with a vacuum in the middle, which improves the thermal insulation performance. This heat energy of strong accumulation and heat preservation can continuously act on the heat collector. Preferably, the concave heat collector is provided w...

Embodiment 3

[0087] In the aircraft described in the invention of the present application, the exterior of the fuel cell is further connected to the electrolysis device, and can supply power to the electrolysis device. After the electrolysis device is powered on, hydrogen and oxygen can be prepared by electrolyzing water and provided to the fuel cell. At the same time, the fuel cell can further provide power for the motor of the aircraft and the hydrogen fluoride laser of the LED resonant cavity.

[0088] The details of the aircraft loaded with the fuel cell as the main energy source in this application are as follows: ① The aircraft in the invention of this application uses the fuel cell described in this application to provide power for a light-body electric motor air pump. Specifically, after the electric motor is powered by the fuel cell, the light metal rotor or electromagnetic induction coil rotor in the center of the electric motor will be energized, and the electric device that fix...

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Abstract

The invention provides a novel fuel cell, a heat-aggregation chemical hydrogen and oxygen producing device containing the fuel cell and an aircraft containing the fuel cell. Magnetic induction coils are arranged in insulating layers of double-layer magnetic-material working cylinders of the protected fuel cell, when the fuel cell works, three magnetic currents exist in a system, and therefore the power of the fuel cell is improved. Meanwhile, the fuel cell can be loaded on the heat-aggregation chemical hydrogen and oxygen producing device, and the device which can produce hydrogen and oxygen in illumination time and non-illumination time is provided. Furthermore, the fuel cell can be further used for the aircraft and serve as a main source of energy to provide energy and power.

Description

technical field [0001] The invention relates to the field of fuel cells, in particular to a fuel cell containing a strong electromagnetic induction coil, a device for producing hydrogen and oxygen carrying the fuel cell, and an aircraft carrying the fuel cell. Background technique [0002] A fuel cell (FuelCell) is a power generation device that directly converts the chemical energy present in fuel and oxidant into electrical energy. Fuel and air are sent separately to the fuel cell to generate electricity. [0003] The solar photovoltaic hydrogen production energy storage fuel cell power generation system is a battery technology that uses solar photovoltaic production of hydrogen and oxygen, and then uses hydrogen and oxygen as the raw fuel to generate electricity in reverse. Photovoltaic cells have developed greatly up to now, mainly in the change and development of battery materials. The development of semiconductors (crystalline silicon) in the 1980s brought down the p...

Claims

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Application Information

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IPC IPC(8): H01M8/04
CPCH01M8/04Y02E60/50
Inventor 任立峰
Owner 任立峰
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