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WO2017114370A1 - Hydrogen ion gas-filled aircraft - Google Patents

Hydrogen ion gas-filled aircraft Download PDF

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Publication number
WO2017114370A1
WO2017114370A1 PCT/CN2016/112218 CN2016112218W WO2017114370A1 WO 2017114370 A1 WO2017114370 A1 WO 2017114370A1 CN 2016112218 W CN2016112218 W CN 2016112218W WO 2017114370 A1 WO2017114370 A1 WO 2017114370A1
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Prior art keywords
telescopic cylinder
stage telescopic
hydrogen
aircraft
cylinder
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PCT/CN2016/112218
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French (fr)
Chinese (zh)
Inventor
龚炳新
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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64BLIGHTER-THAN AIR AIRCRAFT
    • B64B1/00Lighter-than-air aircraft
    • B64B1/58Arrangements or construction of gas-bags; Filling arrangements
    • B64B1/62Controlling gas pressure, heating, cooling, or discharging gas

Definitions

  • This type of aircraft consists of a multi-stage telescopic cylinder, a sealed container, a light source, an electric field and a propeller.
  • the multi-stage telescopic cylinder is made of plastic, and the multi-stage telescopic cylinder is connected with the sealed container through the valve; when lifting, the valve of the sealed container is opened, the hydrogen ions enter the multi-stage telescopic cylinder, and the multi-stage telescopic cylinder expands, when the hydrogen in the multi-stage telescopic cylinder
  • the aircraft obtains lift; the multi-stage telescopic cylinder is equipped with a light source, and when landing, the hydrogen ion is irradiated by the light source to make the hydrogen ions in the multi-stage telescopic cylinder attractive, and the multi-stage telescopic cylinder
  • the internal pressure is reduced, the external atmospheric pressure oppresses the piston of the multi-stage telescopic cylinder,
  • the invention provides a hydrogen-filled ion gas aircraft, which is composed of a multi-stage telescopic cylinder, a sealed container, a light source, an electric field and a propeller.
  • Multi-stage telescopic cylinders are made of plastic, such as nylon or Kevlar.
  • the multi-stage telescopic cylinder is connected to the sealed container through the valve; when lifting, the valve of the sealed container is opened, the hydrogen ions enter the multi-stage telescopic cylinder, and the multi-stage telescopic cylinder expands. After the expansion, the internal pressure of the multi-stage telescopic cylinder is greater than or equal to the external of the multi-stage telescopic cylinder.
  • Atmospheric pressure when the hydrogen ion density in the multi-stage telescopic cylinder is less than the external air density of the multi-stage telescopic cylinder, the aircraft obtains lift and lifts off; the multi-stage telescopic cylinder is equipped with a light source, and when landing, the light source is used to illuminate the hydrogen ion at the incident light. Under irradiation, hydrogen ions will be forced to vibrate. When the direction of the electric field strength of the incident light and the electric moment of the two oscillating hydrogen ions are on the same radial line and in the same direction, the attraction between the oscillating hydrogen ions is attractive.
  • the average kinetic energy of the irregular thermal motion of the hydrogen ions is reduced, and the pressure in the multi-stage telescopic cylinder is reduced.
  • the external atmospheric pressure is greater than the pressure in the multi-stage telescopic cylinder, the external atmospheric pressure presses the piston of the multi-stage telescopic cylinder to make the multi-stage telescopic cylinder
  • the volume is reduced, and the hydrogen ion density in the multi-stage telescopic cylinder is increased.
  • Such an aircraft can also be charged with other ionic gases, such as nitrogen ion gas or oxygen ion gas.
  • other ionic gases such as nitrogen ion gas or oxygen ion gas.
  • Hydrogen ions are positively charged. Under the illumination of incident light, the hydrogen ions will be forced to vibrate, similar to an oscillating electric dipole, and will emit secondary electromagnetic waves.
  • High-speed accelerating charge is usually only found in electron accelerators and other high-energy particle accelerators or in space. Ordinary laboratory sources, such as ultraviolet light, can be thought of as being generated by low-speed accelerating charges. Low-speed accelerating charges can be considered as oscillating electric dipoles. .
  • the incident light be generated by the low-speed accelerating charge, and set the low-speed acceleration charge to be Q, the amplitude is a, and the frequency is ⁇ , then the radiant electric field of the oscillating electric dipole is
  • ⁇ 0 is the vacuum dielectric constant
  • c is the vacuum speed of light
  • R is the distance from the observation point to the center of the oscillating electric dipole.
  • the hydrogen ion will be forced to vibrate, similar to an oscillating electric dipole whose oscillation frequency is equal to the frequency ⁇ of the incident light and emits secondary electromagnetic waves.
  • r is the distance from the observation point to the center of the oscillating hydrogen ion 1, r>>l 1 , r ⁇ , ⁇ is the wavelength of the incident light.
  • ⁇ 0 is the natural frequency of the oscillating hydrogen ion 2
  • is the damping coefficient
  • the oscillating hydrogen ion 2 can be considered as an oscillating electric dipole, the electric dipole moment of the oscillating hydrogen ion 2 is defined as And along Direction, then
  • the Coulomb repulsion F C can be decomposed into F Cx , F Cy , F Cz in Cartesian coordinates :
  • the pressure P has the following relationship:
  • n is the hydrogen ion number density
  • I the average of the squares of the velocity components
  • m e is the mass of the hydrogen ions
  • k B is the Boltzmann constant
  • T is the absolute temperature.
  • the attraction between the oscillating hydrogen ions can be controlled by controlling the frequency of the incident light, the charge amount and amplitude of the acceleration charge generating the incident light, and the distance between the light source and the oscillating hydrogen ions, thereby controlling the landing of the aircraft. speed.
  • the hydrogen ion is accelerated by the electric field force to increase the hydrogen ion velocity, so that the multi-stage telescopic cylinder expands and the multi-stage telescopic cylinder pressure is greater than or equal to Multi-stage telescopic cylinder external atmospheric pressure.
  • the multi-stage telescopic cylinder and the sealed container should be vacuumed to make the pressure inside the multi-stage telescopic cylinder and the sealed container. Less than 1P a . After vacuuming, the hydrogen ion gas is injected. In order to make the oscillating hydrogen ions in the near field of each other, the average distance between the hydrogen ions in the multistage telescopic cylinder and the sealed container should be much smaller than the wavelength of the incident light, r ⁇ . Because the average distance r between hydrogen ions and the hydrogen ion number density n have the following relationship:
  • the hydrogen ion number density n and the incident light wavelength ⁇ have the following relationship:
  • the cube of the hydrogen ion number density is much larger than the incident light wavelength.
  • the required number of hydrogen ions is known from the wavelength of the incident light.
  • the hydrogen ion gas pressure is reduced, the multi-stage telescopic cylinder is reduced in volume, the hydrogen ion density in the multi-stage telescopic cylinder is increased, and the multi-stage telescopic cylinder is made of plastic, such as nylon or Kevlar.
  • the sealed container is filled with hydrogen ion gas
  • the sealed container is made of glass or plastic, and the sealing tube is wrapped with heat insulating material to prevent the pressure of hydrogen ion gas from increasing after heat absorption.
  • the multi-stage telescopic cylinder is equipped with a light source.
  • the light source When landing, the light source is used to illuminate the hydrogen ions, so that the attraction between the oscillating hydrogen ions is generated.
  • the attraction force reduces the average kinetic energy of the irregular thermal motion of the hydrogen ions, and the pressure in the multi-stage telescopic cylinder is reduced.
  • the external atmospheric pressure When the external atmospheric pressure is greater than the pressure in the multi-stage telescopic cylinder, the external atmospheric pressure presses the piston of the multi-stage telescopic cylinder, so that the volume of the multi-stage telescopic cylinder is reduced, and the hydrogen ion density in the multi-stage telescopic cylinder is increased, when the multi-stage telescopic cylinder is inside.
  • the hydrogen ion density is greater than the external air density of the multi-stage telescopic cylinder, the aircraft descends.
  • the buoyancy of the aircraft is controlled by the use of light and the movement of the multi-stage telescopic cylinder piston.

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Particle Accelerators (AREA)
  • Lasers (AREA)

Abstract

Provided is a hydrogen ion gas-filled aircraft composed of a multi-stage telescopic cylinder, a sealed container, a light source, an electric field and a propeller. The cylinder is made of plastic, and is connected to the sealed container through a valve; during lift-off, a valve of the sealed container is opened, hydrogen ions enter the cylinder, and the cylinder expands; when the density of the hydrogen ions in the cylinder is lower than the density of air outside the cylinder, the aircraft is provided with a lift force; a light source is mounted inside the cylinder; during landing, the light source is used to irradiate the hydrogen ions so as to generate an attractive force between the hydrogen ions, the pressure in the cylinder is lowered, and the external atmospheric pressure compresses a piston of the cylinder so that the volume of the cylinder is reduced and the density of the hydrogen ions in the cylinder is increased; and when the density of the hydrogen ions in the cylinder is higher than the density of the air outside the cylinder, the aircraft lands; and the hydrogen ions enter the sealed container under the action of the electric field force, the valve is closed, and the cylinder is retracted. The flight speed and direction of the aircraft are controlled by controlling the propeller. The aircraft is low in cost and not easy to explode, and is suitable for use as a personal aircraft.

Description

充氢离子气的飞行器Hydrogen-charged ion vehicle 技术领域Technical field

这种飞行器由多级伸缩气缸、密封容器、光源、电场和推进器构成。多级伸缩气缸由塑料制成,多级伸缩气缸通过阀门与密封容器连接;升空时,打开密封容器阀门,氢离子进入多级伸缩气缸,多级伸缩气缸膨胀,当多级伸缩气缸内氢离子密度小于多级伸缩气缸外部空气密度时,飞行器获得升力;多级伸缩气缸内安装有光源,降落时,利用光源照射氢离子,使多级伸缩气缸内氢离子产生吸引力,多级伸缩气缸内压力降低,外部大气压力压迫多级伸缩气缸的活塞,使多级伸缩气缸体积减少,多级伸缩气缸内氢离子密度增大,当多级伸缩气缸内氢离子密度大于多级伸缩气缸外部空气密度时,飞行器降落,飞行器降落后,在电场力作用下使氢离子进入密封容器,关闭阀门,收起多级伸缩气缸。通过控制推进器来控制飞行器的飞行速度与方向。This type of aircraft consists of a multi-stage telescopic cylinder, a sealed container, a light source, an electric field and a propeller. The multi-stage telescopic cylinder is made of plastic, and the multi-stage telescopic cylinder is connected with the sealed container through the valve; when lifting, the valve of the sealed container is opened, the hydrogen ions enter the multi-stage telescopic cylinder, and the multi-stage telescopic cylinder expands, when the hydrogen in the multi-stage telescopic cylinder When the ion density is less than the external air density of the multi-stage telescopic cylinder, the aircraft obtains lift; the multi-stage telescopic cylinder is equipped with a light source, and when landing, the hydrogen ion is irradiated by the light source to make the hydrogen ions in the multi-stage telescopic cylinder attractive, and the multi-stage telescopic cylinder The internal pressure is reduced, the external atmospheric pressure oppresses the piston of the multi-stage telescopic cylinder, the volume of the multi-stage telescopic cylinder is reduced, and the hydrogen ion density in the multi-stage telescopic cylinder is increased. When the hydrogen ion density in the multi-stage telescopic cylinder is greater than the external air of the multi-stage telescopic cylinder At the time of density, the aircraft landed and the aircraft descended. Under the action of the electric field force, hydrogen ions were introduced into the sealed container, the valve was closed, and the multi-stage telescopic cylinder was closed. Control the speed and direction of the aircraft by controlling the propeller.

背景技术Background technique

我们知道,充氢气的飞行器容易爆炸,充氦气的飞行器成本太高,而且充氢气和充氦气的飞行器降落后还占据大量空间,不适宜作个人飞行器。We know that hydrogen-filled aircraft are easy to explode, and the cost of a gas-filled aircraft is too high, and that the hydrogen-filled and helium-filled aircraft still take up a lot of space after landing, which is not suitable for personal aircraft.

发明内容Summary of the invention

本发明提供一种充氢离子气的飞行器,这种飞行器由多级伸缩气缸、密封容器、光源、电场和推进器构成。多级伸缩气缸由塑料制成,例如尼龙或凯夫拉。多级伸缩气缸通过阀门与密封容器连接;升空时,打开密封容器阀门,氢离子进入多级伸缩气缸,多级伸缩气缸膨胀,膨胀后多级伸缩气缸内压力大于或等于多级伸缩气缸外部大气压力,当多级伸缩气缸内氢离子密度小于多级伸缩气缸外部空气密度时,飞行器获得升力并升空;多级伸缩气缸内安装有光源,降落时,利用光源照射氢离子,在入射光照射下,氢离子将会作受迫振动,当入射光的电场强度方向和两个振荡氢离子的电矩在同一径向直线上且同向时,振荡氢离子之间是吸引力,吸引力使氢离子无规则的热运动平均动能减少,多级伸缩气缸内压力从而降低,当外部大气压力大于多级伸缩气缸内压力时,外部大气压力压迫多级伸缩气缸的活塞,使多级伸缩气缸体积减少,多级伸缩气缸内氢离子密度增大,当多级伸缩气缸内氢离子密度大于多级伸缩气缸外部空气密度时,飞行器降落;密封容器由玻璃或塑料制成,密封容器内有电场,飞行器降落后,在电场力作用下使氢离子进入密封容器,关闭阀门,收起多级伸缩气缸。通过控制推进器来控制飞行器的飞行速度与方向。The invention provides a hydrogen-filled ion gas aircraft, which is composed of a multi-stage telescopic cylinder, a sealed container, a light source, an electric field and a propeller. Multi-stage telescopic cylinders are made of plastic, such as nylon or Kevlar. The multi-stage telescopic cylinder is connected to the sealed container through the valve; when lifting, the valve of the sealed container is opened, the hydrogen ions enter the multi-stage telescopic cylinder, and the multi-stage telescopic cylinder expands. After the expansion, the internal pressure of the multi-stage telescopic cylinder is greater than or equal to the external of the multi-stage telescopic cylinder. Atmospheric pressure, when the hydrogen ion density in the multi-stage telescopic cylinder is less than the external air density of the multi-stage telescopic cylinder, the aircraft obtains lift and lifts off; the multi-stage telescopic cylinder is equipped with a light source, and when landing, the light source is used to illuminate the hydrogen ion at the incident light. Under irradiation, hydrogen ions will be forced to vibrate. When the direction of the electric field strength of the incident light and the electric moment of the two oscillating hydrogen ions are on the same radial line and in the same direction, the attraction between the oscillating hydrogen ions is attractive. The average kinetic energy of the irregular thermal motion of the hydrogen ions is reduced, and the pressure in the multi-stage telescopic cylinder is reduced. When the external atmospheric pressure is greater than the pressure in the multi-stage telescopic cylinder, the external atmospheric pressure presses the piston of the multi-stage telescopic cylinder to make the multi-stage telescopic cylinder The volume is reduced, and the hydrogen ion density in the multi-stage telescopic cylinder is increased. When the density of hydrogen ions in the multi-stage telescopic cylinder is greater than that of the multi-stage extension Outside the cylinder air density, aircraft landing; hermetically sealed container made of glass or plastic, an electric field in a sealed vessel, after the landing of the aircraft, hydrogen ions into the sealed vessel, closing the valve, a multi-stage telescopic cylinder stowed under the electrostatic force. Control the speed and direction of the aircraft by controlling the propeller.

这种飞行器也可以充其它的离子气,例如氮离子气或氧离子气。Such an aircraft can also be charged with other ionic gases, such as nitrogen ion gas or oxygen ion gas.

振荡氢离子之间产生吸引力及多级伸缩气缸内压力降低基于以下的原理:The attraction between the oscillating hydrogen ions and the multi-stage telescopic cylinder pressure reduction are based on the following principles:

氢离子带正电荷,在入射光照射下,氢离子将会作受迫振动,类似于一个振荡电偶极子,并将发射次级电磁波。Hydrogen ions are positively charged. Under the illumination of incident light, the hydrogen ions will be forced to vibrate, similar to an oscillating electric dipole, and will emit secondary electromagnetic waves.

当入射光的电场强度方向和两个振荡电偶极子的电矩在同一径向直线上且同向时,两振荡电偶极子之间是相互吸引的径向作用力,也就是说,两个振荡氢离子之间是相互吸引的径向作用力。 When the direction of the electric field intensity of the incident light and the electric moment of the two oscillating electric dipoles are on the same radial straight line and in the same direction, the two oscillating electric dipoles are mutually attracted radial forces, that is, The two oscillating hydrogen ions are mutually attracted radial forces.

根据光的电磁理论,光是由加速电荷产生。高速加速电荷通常只存在于电子加速器和其它高能粒子加速器或宇宙空间中,普通的实验室光源,例如紫外光,可以认为是由低速加速电荷产生的,低速加速电荷可以考虑为振荡电偶极子。According to the electromagnetic theory of light, light is generated by accelerating charge. High-speed accelerating charge is usually only found in electron accelerators and other high-energy particle accelerators or in space. Ordinary laboratory sources, such as ultraviolet light, can be thought of as being generated by low-speed accelerating charges. Low-speed accelerating charges can be considered as oscillating electric dipoles. .

设入射光由低速加速电荷产生,设低速加速电荷带电量为Q,振幅为a,频率为ω,则这个振荡电偶极子的辐射电场为

Figure PCTCN2016112218-appb-000001
Let the incident light be generated by the low-speed accelerating charge, and set the low-speed acceleration charge to be Q, the amplitude is a, and the frequency is ω, then the radiant electric field of the oscillating electric dipole is
Figure PCTCN2016112218-appb-000001

Figure PCTCN2016112218-appb-000002
Figure PCTCN2016112218-appb-000002

式中ε0是真空介电常数,c是真空光速,R是观察点到振荡电偶极子中心的距离。Where ε 0 is the vacuum dielectric constant, c is the vacuum speed of light, and R is the distance from the observation point to the center of the oscillating electric dipole.

make

Figure PCTCN2016112218-appb-000003
Figure PCTCN2016112218-appb-000003

则公式(1)变为Then the formula (1) becomes

Figure PCTCN2016112218-appb-000004
Figure PCTCN2016112218-appb-000004

电场强度

Figure PCTCN2016112218-appb-000005
将会使氢离子作受迫振动,类似于一个振荡电偶极子,它的振荡频率等于入射光的频率ω,并发射次级电磁波。Electric field strength
Figure PCTCN2016112218-appb-000005
The hydrogen ion will be forced to vibrate, similar to an oscillating electric dipole whose oscillation frequency is equal to the frequency ω of the incident light and emits secondary electromagnetic waves.

设氢离子1的带电量为qe,振幅为l1,在球坐标中,振荡氢离子1的近区电场强度和磁场强度分别为:Let the charge of hydrogen ion 1 be q e and the amplitude be l 1 . In the spherical coordinates, the electric field strength and magnetic field strength of the near-field of the oscillating hydrogen ion 1 are:

Figure PCTCN2016112218-appb-000006
Figure PCTCN2016112218-appb-000006

Figure PCTCN2016112218-appb-000007
Figure PCTCN2016112218-appb-000007

Figure PCTCN2016112218-appb-000008
Figure PCTCN2016112218-appb-000008

式中r是观察点到振荡氢离子1中心的距离,r>>l1,r<<λ,λ是入射光的波长。Where r is the distance from the observation point to the center of the oscillating hydrogen ion 1, r>>l 1 , r<<λ, λ is the wavelength of the incident light.

设振荡氢离子2在观察点,因此振荡氢离子1和振荡氢离子2的距离是r。当电场强度

Figure PCTCN2016112218-appb-000009
沿
Figure PCTCN2016112218-appb-000010
方向时,θ=0,公式(4)、(5)和(6)变为Let the oscillating hydrogen ion 2 be at the observation point, so the distance between the oscillating hydrogen ion 1 and the oscillating hydrogen ion 2 is r. Electric field strength
Figure PCTCN2016112218-appb-000009
along
Figure PCTCN2016112218-appb-000010
In the direction, θ = 0, and equations (4), (5), and (6) become

Figure PCTCN2016112218-appb-000011
Figure PCTCN2016112218-appb-000011

Figure PCTCN2016112218-appb-000012
Figure PCTCN2016112218-appb-000012

Figure PCTCN2016112218-appb-000013
Figure PCTCN2016112218-appb-000013

振荡氢离子2在电场强度

Figure PCTCN2016112218-appb-000014
Figure PCTCN2016112218-appb-000015
作用下作简谐受迫振动,其振荡频率等于入射光的频率ω,并将发射次级电磁波。设其质量为me,带电量为qe,振幅为l2,则振荡氢离子2在
Figure PCTCN2016112218-appb-000016
方向上的运动方程为:Oscillating hydrogen ion 2 at electric field strength
Figure PCTCN2016112218-appb-000014
with
Figure PCTCN2016112218-appb-000015
Under the action, the harmonic vibration is forced, the oscillation frequency is equal to the frequency ω of the incident light, and the secondary electromagnetic wave will be emitted. Which is set mass m e, charge amount q e, amplitude l 2, 2 hydrogen ions in the oscillation
Figure PCTCN2016112218-appb-000016
The equation of motion in the direction is:

Figure PCTCN2016112218-appb-000017
Figure PCTCN2016112218-appb-000017

式中ω0是振荡氢离子2的固有频率,γ是阻尼系数,Where ω 0 is the natural frequency of the oscillating hydrogen ion 2, and γ is the damping coefficient.

Figure PCTCN2016112218-appb-000018
Figure PCTCN2016112218-appb-000018

因为γ<<ω,所以Because γ<<ω, so

Figure PCTCN2016112218-appb-000019
Figure PCTCN2016112218-appb-000019

Figure PCTCN2016112218-appb-000020
Figure PCTCN2016112218-appb-000020

因为振荡氢离子2可以考虑为振荡电偶极子,定义振荡氢离子2的电偶极矩为

Figure PCTCN2016112218-appb-000021
并沿
Figure PCTCN2016112218-appb-000022
方向,则Since the oscillating hydrogen ion 2 can be considered as an oscillating electric dipole, the electric dipole moment of the oscillating hydrogen ion 2 is defined as
Figure PCTCN2016112218-appb-000021
And along
Figure PCTCN2016112218-appb-000022
Direction, then

Figure PCTCN2016112218-appb-000023
Figure PCTCN2016112218-appb-000023

电场强度

Figure PCTCN2016112218-appb-000024
和距离r没有关系,因此不会给振荡氢离子2
Figure PCTCN2016112218-appb-000025
方向的力。Electric field strength
Figure PCTCN2016112218-appb-000024
Has nothing to do with distance r, so it will not give oscillating hydrogen ions 2
Figure PCTCN2016112218-appb-000025
Direction of force.

振荡氢离子1的近区电场强度

Figure PCTCN2016112218-appb-000026
将会给振荡氢离子2
Figure PCTCN2016112218-appb-000027
方向的力FN,电场强度
Figure PCTCN2016112218-appb-000028
振荡氢离子1和振荡氢离子2的电矩沿
Figure PCTCN2016112218-appb-000029
连线且同向,Near-field electric field strength of oscillating hydrogen ion 1
Figure PCTCN2016112218-appb-000026
Will give oscillating hydrogen ions 2
Figure PCTCN2016112218-appb-000027
Directional force F N , electric field strength
Figure PCTCN2016112218-appb-000028
The electric moment along the oscillating hydrogen ion 1 and the oscillating hydrogen ion 2
Figure PCTCN2016112218-appb-000029
Connected and in the same direction,

Figure PCTCN2016112218-appb-000030
Figure PCTCN2016112218-appb-000030

式中

Figure PCTCN2016112218-appb-000031
In the middle
Figure PCTCN2016112218-appb-000031

Figure PCTCN2016112218-appb-000032
Figure PCTCN2016112218-appb-000032

由公式(16)可知,在近区,振荡氢离子1和振荡氢离子2之间有

Figure PCTCN2016112218-appb-000033
方向上的吸引力。It can be seen from the formula (16) that in the near region, there is a relationship between the oscillating hydrogen ion 1 and the oscillating hydrogen ion 2
Figure PCTCN2016112218-appb-000033
The attraction in the direction.

这个

Figure PCTCN2016112218-appb-000034
方向上的吸引力FN可在直角坐标上分解为FNx、FNy和FNz:This one
Figure PCTCN2016112218-appb-000034
The attractive force F N in the direction can be decomposed into F Nx , F Ny and F Nz on the Cartesian coordinates:

Figure PCTCN2016112218-appb-000035
Figure PCTCN2016112218-appb-000035

Figure PCTCN2016112218-appb-000036
Figure PCTCN2016112218-appb-000036

Figure PCTCN2016112218-appb-000037
Figure PCTCN2016112218-appb-000037

氢离子1和氢离子2之间有库仑斥力FCThere is a Coulomb repulsion F C between hydrogen ion 1 and hydrogen ion 2:

Figure PCTCN2016112218-appb-000038
Figure PCTCN2016112218-appb-000038

库仑斥力FC可在直角坐标上分解为FCx,FCy,FCzThe Coulomb repulsion F C can be decomposed into F Cx , F Cy , F Cz in Cartesian coordinates :

Figure PCTCN2016112218-appb-000039
Figure PCTCN2016112218-appb-000039

Figure PCTCN2016112218-appb-000040
Figure PCTCN2016112218-appb-000040

Figure PCTCN2016112218-appb-000041
Figure PCTCN2016112218-appb-000041

因为氢离子的体积很少,氢离子可当作质点,除碰撞瞬间外,氢离子间的相互作用可忽略不计,碰撞前后氢离子动能守恒,因此压强P有如下关系:Because the volume of hydrogen ions is very small, hydrogen ions can be regarded as mass points. Except for the collision moment, the interaction between hydrogen ions is negligible. The hydrogen kinetic energy is conserved before and after the collision. Therefore, the pressure P has the following relationship:

Figure PCTCN2016112218-appb-000042
Figure PCTCN2016112218-appb-000042

Figure PCTCN2016112218-appb-000043
Figure PCTCN2016112218-appb-000043

式中n是氢离子数密度,

Figure PCTCN2016112218-appb-000044
Figure PCTCN2016112218-appb-000045
是各速度分量的平方的平均值,me是氢离子质量,kB是玻尔兹曼常数,T是绝对温度。Where n is the hydrogen ion number density,
Figure PCTCN2016112218-appb-000044
with
Figure PCTCN2016112218-appb-000045
Is the average of the squares of the velocity components, m e is the mass of the hydrogen ions, k B is the Boltzmann constant, and T is the absolute temperature.

因为 Because

Figure PCTCN2016112218-appb-000046
Figure PCTCN2016112218-appb-000046

Figure PCTCN2016112218-appb-000047
Figure PCTCN2016112218-appb-000047

Figure PCTCN2016112218-appb-000048
Figure PCTCN2016112218-appb-000048

Figure PCTCN2016112218-appb-000049
Figure PCTCN2016112218-appb-000049

由于A可以控制,所以Since A can be controlled,

Figure PCTCN2016112218-appb-000050
Figure PCTCN2016112218-appb-000050

当ω>>ω0时,When ω>>ω 0 ,

Figure PCTCN2016112218-appb-000051
Figure PCTCN2016112218-appb-000051

Figure PCTCN2016112218-appb-000052
Figure PCTCN2016112218-appb-000052

Figure PCTCN2016112218-appb-000053
Figure PCTCN2016112218-appb-000053

由于due to

Figure PCTCN2016112218-appb-000054
Figure PCTCN2016112218-appb-000054

积分式(32)和(33)可得,Integral (32) and (33) are available,

Figure PCTCN2016112218-appb-000055
Figure PCTCN2016112218-appb-000055

Figure PCTCN2016112218-appb-000056
Figure PCTCN2016112218-appb-000056

由于A、l1和r都可以控制,当Since A, l 1 and r can be controlled, when

Figure PCTCN2016112218-appb-000057
Figure PCTCN2016112218-appb-000057

时,Time,

Vx1-Vx0<0      (38)V x1 -V x0 <0 (38)

P1-P0<0      (39)P 1 -P 0 <0 (39)

when

Figure PCTCN2016112218-appb-000058
Figure PCTCN2016112218-appb-000058

时,Time,

Vx1=0,P1=0     (41)V x1 =0, P 1 =0 (41)

因为because

Figure PCTCN2016112218-appb-000059
Figure PCTCN2016112218-appb-000059

所以and so

Vx=0     (43)V x = 0 (43)

同理可得The same reason

Vy=0,Vz=0      (44)V y =0, V z =0 (44)

从以上原理可知,在入射光照射下,振荡氢离子之间产生吸引力,多级伸缩气缸内压力降低到零。但是,由于杂质的存在,多级伸缩气缸内压力不能真正降低到零。It can be seen from the above principle that under the irradiation of incident light, an attractive force is generated between the oscillating hydrogen ions, and the pressure in the multi-stage telescopic cylinder is reduced to zero. However, due to the presence of impurities, the pressure in the multi-stage telescopic cylinder cannot be truly reduced to zero.

从以上原理可知,可以通过控制入射光的频率、产生入射光的加速电荷的带电量和振幅以及光源与振荡氢离子之间的距离来控制振荡氢离子之间的吸引力,从而控制飞行器的降落速度。It can be known from the above principle that the attraction between the oscillating hydrogen ions can be controlled by controlling the frequency of the incident light, the charge amount and amplitude of the acceleration charge generating the incident light, and the distance between the light source and the oscillating hydrogen ions, thereby controlling the landing of the aircraft. speed.

由于多级伸缩气缸内氢离子密度越小,获得的升力越大,但多级伸缩气缸膨胀后多级伸缩气缸内压力应大于或等于多级伸缩气缸外部大气压力,因此通过光照以及控制氢离子密度和多级伸缩气缸活塞的行程来控制获得的升力,飞行器升空时,通过电场力加速氢离子,使氢离子速度增大,使多级伸缩气缸膨胀后多级伸缩气缸内压力大于或等于多级伸缩气缸外部大气压力。The smaller the hydrogen ion density in the multi-stage telescopic cylinder, the greater the lift obtained, but the multi-stage telescopic cylinder after expansion should be greater than or equal to the external atmospheric pressure of the multi-stage telescopic cylinder, so through the illumination and control of hydrogen ions Density and the stroke of the multi-stage telescopic cylinder piston to control the lift obtained. When the aircraft is lifted off, the hydrogen ion is accelerated by the electric field force to increase the hydrogen ion velocity, so that the multi-stage telescopic cylinder expands and the multi-stage telescopic cylinder pressure is greater than or equal to Multi-stage telescopic cylinder external atmospheric pressure.

具体实施方式detailed description

下面介绍一具体实施例,具体实施方式不局限于此例。A specific embodiment is described below, and the specific embodiment is not limited to this example.

如果多级伸缩气缸和密封容器内有空气,空气分子的热动能将会影响氢离子气压力降低,所以要先将多级伸缩气缸和密封容器抽真空,使多级伸缩气缸和密封容器内压强低于1Pa。抽真空后,再将氢离子气注入,为使振荡氢离子处于彼此的近区场,多级伸缩气缸和密封容器内氢离子间的平均距离应远小于入射光的波长,r<<λ。因为氢离子间的平均距离r和氢离子数密度n有如下关系: If there is air in the multi-stage telescopic cylinder and the sealed container, the thermal kinetic energy of the air molecules will affect the pressure of the hydrogen ion gas. Therefore, the multi-stage telescopic cylinder and the sealed container should be vacuumed to make the pressure inside the multi-stage telescopic cylinder and the sealed container. Less than 1P a . After vacuuming, the hydrogen ion gas is injected. In order to make the oscillating hydrogen ions in the near field of each other, the average distance between the hydrogen ions in the multistage telescopic cylinder and the sealed container should be much smaller than the wavelength of the incident light, r<<λ. Because the average distance r between hydrogen ions and the hydrogen ion number density n have the following relationship:

Figure PCTCN2016112218-appb-000060
Figure PCTCN2016112218-appb-000060

因此氢离子数密度n和入射光的波长λ有如下关系:Therefore, the hydrogen ion number density n and the incident light wavelength λ have the following relationship:

Figure PCTCN2016112218-appb-000061
Figure PCTCN2016112218-appb-000061

也就是氢离子数密度的三次方远远大于入射光波长。从入射光波长可知需要的氢离子数密度。That is, the cube of the hydrogen ion number density is much larger than the incident light wavelength. The required number of hydrogen ions is known from the wavelength of the incident light.

因为氢离子是从气体电离产生的,氢分子有2个氢离子,每摩尔氢气有6.023×1023个氢分子,从入射光波长可知需要电离的氢气摩尔数。Since hydrogen ions are generated from gas ionization, the hydrogen molecules have two hydrogen ions, and there are 6.023 × 10 23 hydrogen molecules per mole of hydrogen. From the wavelength of the incident light, the number of moles of hydrogen that needs to be ionized is known.

因光照会导致氢离子气压力降低,多级伸缩气缸体积减少,多级伸缩气缸内氢离子密度增大,多级伸缩气缸由塑料制成,例如尼龙或凯夫拉。Due to the illumination, the hydrogen ion gas pressure is reduced, the multi-stage telescopic cylinder is reduced in volume, the hydrogen ion density in the multi-stage telescopic cylinder is increased, and the multi-stage telescopic cylinder is made of plastic, such as nylon or Kevlar.

因密封容器内充满氢离子气,密封容器由玻璃或塑料制成,密封管外包裹隔热材料,防止氢离子气吸热后压力升高。Because the sealed container is filled with hydrogen ion gas, the sealed container is made of glass or plastic, and the sealing tube is wrapped with heat insulating material to prevent the pressure of hydrogen ion gas from increasing after heat absorption.

升空时,打开密封容器阀门,氢离子进入多级伸缩气缸,多级伸缩气缸膨胀,膨胀后多级伸缩气缸内压力大于或等于多级伸缩气缸外部大气压力,当多级伸缩气缸内氢离子密度小于多级伸缩气缸外部空气密度时,飞行器获得升力并升空。When lifting off, open the sealed container valve, hydrogen ions enter the multi-stage telescopic cylinder, multi-stage telescopic cylinder expands, after expansion, the multi-stage telescopic cylinder pressure is greater than or equal to the external atmospheric pressure of the multi-stage telescopic cylinder, when the hydrogen ion in the multi-stage telescopic cylinder When the density is less than the external air density of the multi-stage telescopic cylinder, the aircraft gains lift and lifts off.

通过控制推进器来控制飞行器的飞行速度与方向。Control the speed and direction of the aircraft by controlling the propeller.

多级伸缩气缸内安装有光源,降落时,利用光源照射氢离子,使振荡氢离子之间产生吸引力,吸引力使氢离子无规则的热运动平均动能减少,多级伸缩气缸内压力从而降低,当外部大气压力大于多级伸缩气缸内压力时,外部大气压力压迫多级伸缩气缸的活塞,使多级伸缩气缸体积减少,多级伸缩气缸内氢离子密度增大,当多级伸缩气缸内氢离子密度大于多级伸缩气缸外部空气密度时,飞行器降落。The multi-stage telescopic cylinder is equipped with a light source. When landing, the light source is used to illuminate the hydrogen ions, so that the attraction between the oscillating hydrogen ions is generated. The attraction force reduces the average kinetic energy of the irregular thermal motion of the hydrogen ions, and the pressure in the multi-stage telescopic cylinder is reduced. When the external atmospheric pressure is greater than the pressure in the multi-stage telescopic cylinder, the external atmospheric pressure presses the piston of the multi-stage telescopic cylinder, so that the volume of the multi-stage telescopic cylinder is reduced, and the hydrogen ion density in the multi-stage telescopic cylinder is increased, when the multi-stage telescopic cylinder is inside. When the hydrogen ion density is greater than the external air density of the multi-stage telescopic cylinder, the aircraft descends.

通过用光照以及多级伸缩气缸活塞的运动来控制飞行器的浮力。The buoyancy of the aircraft is controlled by the use of light and the movement of the multi-stage telescopic cylinder piston.

密封容器内有电场,飞行器降落后,在电场力作用下使氢离子进入密封容器,关闭阀门,收起多级伸缩气缸。There is an electric field in the sealed container. After the aircraft descends, the hydrogen ions enter the sealed container under the action of the electric field force, the valve is closed, and the multi-stage telescopic cylinder is collected.

参考文献:references:

1,1,

BingXin Gong,2013,The light controlled fusion,Annals of Nuclear Energy,62(2013),57–60. BingXin Gong, 2013, The light controlled fusion, Annals of Nuclear Energy, 62 (2013), 57–60.

Claims (4)

充氢离子气的飞行器,其特征在于:这种充氢离子气的飞行器由多级伸缩气缸、密封容器、光源、电场和推进器构成;多级伸缩气缸由塑料制成,多级伸缩气缸通过阀门与密封容器连接;升空时,打开密封容器阀门,氢离子进入多级伸缩气缸,多级伸缩气缸膨胀,膨胀后多级伸缩气缸内压力大于或等于多级伸缩气缸外部大气压力,当多级伸缩气缸内氢离子密度小于多级伸缩气缸外部空气密度时,飞行器获得升力并升空;多级伸缩气缸内安装有光源,降落时,利用光源照射氢离子,在入射光照射下,氢离子将会作受迫振动,当入射光的电场强度方向和两个振荡氢离子的电矩在同一径向直线上且同向时,振荡氢离子之间是吸引力,吸引力使氢离子无规则的热运动平均动能减少,多级伸缩气缸内压力从而降低,当外部大气压力大于多级伸缩气缸内压力时,外部大气压力压迫多级伸缩气缸的活塞,使多级伸缩气缸体积减少,多级伸缩气缸内氢离子密度增大,当多级伸缩气缸内氢离子密度大于多级伸缩气缸外部空气密度时,飞行器降落;密封容器由玻璃或塑料制成,密封容器内有电场,飞行器降落后,在电场力作用下使氢离子进入密封容器,关闭阀门,收起多级伸缩气缸;通过控制推进器来控制飞行器的飞行速度与方向。An apparatus for charging hydrogen ion gas, characterized in that: the hydrogen-charged ion gas aircraft is composed of a multi-stage telescopic cylinder, a sealed container, a light source, an electric field and a propeller; the multi-stage telescopic cylinder is made of plastic, and the multi-stage telescopic cylinder passes The valve is connected with the sealed container; when lifting, the valve of the sealed container is opened, the hydrogen ions enter the multi-stage telescopic cylinder, and the multi-stage telescopic cylinder expands. After the expansion, the pressure in the multi-stage telescopic cylinder is greater than or equal to the external atmospheric pressure of the multi-stage telescopic cylinder. When the hydrogen ion density in the stage telescopic cylinder is less than the external air density of the multi-stage telescopic cylinder, the aircraft obtains lift and lifts off; the multi-stage telescopic cylinder is equipped with a light source. When landing, the light source is used to irradiate hydrogen ions, and under the irradiation of incident light, hydrogen ions Forced vibration will occur. When the direction of the electric field strength of the incident light and the electric moment of the two oscillating hydrogen ions are on the same radial line and in the same direction, the attraction between the oscillating hydrogen ions is attractive, and the attraction force makes the hydrogen ions irregular. The average kinetic energy of the thermal motion is reduced, and the pressure in the multi-stage telescopic cylinder is reduced, when the external atmospheric pressure is greater than the pressure in the multi-stage telescopic cylinder The external atmospheric pressure oppresses the piston of the multi-stage telescopic cylinder, which reduces the volume of the multi-stage telescopic cylinder, and increases the hydrogen ion density in the multi-stage telescopic cylinder. When the hydrogen ion density in the multi-stage telescopic cylinder is greater than the external air density of the multi-stage telescopic cylinder, the aircraft The sealed container is made of glass or plastic. The sealed container has an electric field. After the aircraft descends, the hydrogen ions enter the sealed container under the action of the electric field force, close the valve, and close the multi-stage telescopic cylinder; control the aircraft by controlling the propeller. Flight speed and direction. 根据权利要求1所述的充氢离子气的飞行器,其特征在于:这种充氢离子气的飞行器也可以充氮离子气或氧离子气或其它的离子气。The hydrogen-charged ion-gas aircraft according to claim 1, characterized in that the hydrogen-charged ion-gas aircraft can also be filled with nitrogen ion gas or oxygen ion gas or other ion gas. 根据权利要求1所述的充氢离子气的飞行器,其特征在于:通过控制入射光的频率、产生入射光的加速电荷的带电量和振幅以及光源与振荡氢离子之间的距离来控制振荡氢离子之间的吸引力,从而控制飞行器的降落速度。The hydrogen-filled ion gas-based aircraft according to claim 1, wherein the oscillating hydrogen is controlled by controlling a frequency of incident light, a charge amount and amplitude of an acceleration charge for generating incident light, and a distance between the light source and the oscillating hydrogen ion. The attraction between the ions to control the landing speed of the aircraft. 根据权利要求1所述的充氢离子气的飞行器,其特征在于:通过光照以及控制氢离子密度和多级伸缩气缸活塞的行程来控制获得的升力,飞行器升空时,通过电场力加速氢离子,使氢离子速度增大,使多级伸缩气缸膨胀后多级伸缩气缸内压力大于或等于多级伸缩气缸外部大气压力。 The apparatus for charging hydrogen ion gas according to claim 1, wherein the obtained lift is controlled by illumination and controlling the hydrogen ion density and the stroke of the multistage telescopic cylinder piston, and the hydrogen ion is accelerated by the electric field force when the aircraft is lifted off. The hydrogen ion velocity is increased, and the pressure in the multi-stage telescopic cylinder after the expansion of the multi-stage telescopic cylinder is greater than or equal to the external atmospheric pressure of the multi-stage telescopic cylinder.
PCT/CN2016/112218 2015-12-30 2016-12-26 Hydrogen ion gas-filled aircraft Ceased WO2017114370A1 (en)

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