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Unidirectional power generator

A generation device, one-way technology, which is applied in the directions of the propulsion system device of the spacecraft, the type of power plant, etc., can solve the problems of low energy utilization rate of the aircraft, increase the weight of the aircraft itself, and low air specific gravity, so as to improve the energy utilization efficiency. , the effect of reducing self quality and reducing damage

Inactive Publication Date: 2007-11-07
黄立新
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Because the conventional aircraft is powered by the consumption of recoil objects, due to the small air specific gravity and low utilization rate, it needs to carry more liquid hydrogen and liquid oxygen, which will increase the weight of the aircraft itself, and the recoil objects after burning will still To take away a certain amount of heat energy, so the energy utilization rate of conventional aircraft is not high
In addition, since the space is basically a vacuum, the flight of the aircraft is driven by the recoil working fluid formed by the fuel carried after combustion and injection, which will inevitably have many adverse effects on the flight speed and flight mileage of the aircraft.

Method used

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Embodiment Construction

[0016] As shown in Figure 1, the unidirectional power generating device is fixed with two motors 14, 16 with the same structure, power and rotating speed on the board surface of a rectangular base plate 15, the tails of the two motors are opposite, and the output shafts are on the same straight line The upper side protrudes in reverse, and the output shaft ends of the two motors are respectively connected with a one-way power conversion device. The controller 18 between the two motors controls the operation of the two motors, and provides the required power for the relevant mechanisms in the one-way power conversion device.

[0017] A kind of one-way power conversion device shown in Fig. 2 is to fix an upright circular retaining ring 9 by bracket 17 on the base plate 15, is provided with ejector 5 in the center of retaining ring, and ejector is fixed by strut 7 , the pole 7 is either in contact with the bracket 17 or in contact with the base plate 15 . One side of retaining r...

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PUM

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Abstract

The unidirectional power generator has the structure includes one base board, two motors and motor controllers in the same structure, power and rotation speed and fixed on the base board with opposite tails and output shafts extending out oppositely in the same line, and two unidirectional power converters connected separately to the output shafts of the motors. The present invention needs no kickback article, and this makes it possible for the flyer to decrease its dead weight. The present invention can provides space flyer with unidirectional power for high flying speed, long flying distance, increased flying time and increased amount of carried instrument.

Description

technical field [0001] The invention relates to a power device, in particular to a one-way power generating device. Background technique [0002] In the current aerodynamic technology, the aircraft relies on the combustion of liquid hydrogen, liquid oxygen, etc. and recoils the air to provide forward flight power. Because the air density is small, to further increase the specific impulse, the capital required is huge, but the effect seen is very small. Because the conventional aircraft is powered by the consumption of recoil objects, due to the small air specific gravity and low utilization rate, it needs to carry more liquid hydrogen and liquid oxygen, which will increase the weight of the aircraft itself, and the recoil objects after burning will still To take away a certain amount of thermal energy, so the energy utilization rate of conventional aircraft is not high. In addition, since the space is basically a vacuum, the flight of the aircraft is driven by the recoil w...

Claims

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Application Information

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IPC IPC(8): B64G1/40B64D27/02
Inventor 黄立新
Owner 黄立新
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