CN104608940A - Method for driving engine by means of gravitational field curvature - Google Patents
Method for driving engine by means of gravitational field curvature Download PDFInfo
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- CN104608940A CN104608940A CN201410804269.5A CN201410804269A CN104608940A CN 104608940 A CN104608940 A CN 104608940A CN 201410804269 A CN201410804269 A CN 201410804269A CN 104608940 A CN104608940 A CN 104608940A
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- gravitational field
- curvature
- field curvature
- rotating ring
- annulus
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Abstract
The invention relates to the technical field of aerospace engines, in particular to a method for driving an engine, namely an anti-gravity engine, by means of the gravitational field curvature. The method comprises the steps that the circular motion replaces the linear motion, and anti-gravity is provided when gravitational force cannot provide the centripetal acceleration relative to the center of the gravitational force. According to the method, the circular motion is used for replacing the linear motion, and the anti-gravity is provided when the gravitational force cannot provide centripetal acceleration relative to the center of the gravitational force, so that the effect of driving the engine by means of the gravitational field curvature is achieved. By the adoption of the mode that the linear speed of a rotating object overcomes the gravitational force, the method can be used inside the atmosphere and the outer space; no extra working media are needed, thrust is provided, and the effective load is greatly and significantly improved; the method is applicable to gravitational fields with the curvatures larger than zero, such as an engine, an aircraft and an energy storing device.
Description
Technical field
The present invention relates to a kind of Aeronautics and Astronautics technical field of engines, particularly relate to a kind of method of gravitational field Curvature-driven engine, i.e. antigravity engine.
Background technology
Traditional aerospace driving engine leans on the anti-propelling thrust of working medium to run.Air can be utilized in endoatmosphere as working medium, and working medium can only be carried at the outer space and come.It is little that this shortcoming causes capacity weight, because which limit the work efficiency of driving engine.
Summary of the invention
For the deficiencies in the prior art part, the invention provides a kind of method of gravitational field Curvature-driven engine.Object is to provide a kind of engine technology not needing working medium, and the principle utilizing gravitational field to be curved surface is as promotion aircraft flight power.When gravitation cannot provide the centripetal acceleration of particle, the direction less to gravitation line curvature such as gravitational fields is moved by object.
In order to realize foregoing invention object, the present invention is achieved by the following technical solutions:
The method of gravitational field Curvature-driven engine replaces straight-line motion by circular movement, when gravitation cannot provide the centripetal acceleration relative to center of attraction, provides antigravity.
Described with circular movement replacement straight-line motion is: the curvature of earth surface is about k=1/6.4*10
6rice
-1, the object of moving linearly, curvature k=0, the object moved in a circle on ground level thus is also 0 relative to the curvature in the earth's core; The terrestrial attraction be subject to when the particle of a circular movement on that plane is thus mg, so when the speed of this particle is greater than
namely during the first cosmic velocity, centnifugal force is greater than this particle of terrestrial attraction and starts to provide lift; When all particles relative to the centnifugal force in the earth's core make a concerted effort the total force being greater than aircraft time, aircraft leaves ground; In above-mentioned formula: v
0represent minimum line speed; G represents the acceleration due to gravity of earth surface; K represents gravitational field curvature.
The gravitation face of waiting of described earth surface is an approximate ball, and gravitational field Curvature-driven current reference is the annulus of a High Rotation Speed tangent with waiting gravitation face, and the linear velocity of the rotating ring distributed when prevailing quality is greater than v
0time, gravitational field Curvature-driven engine starts to play antigravity effect; Utilize plane of rotation curvature to be approximately zero curved surface being less than gravitational field curved surface as the rotative speed v of annulus and be greater than v
0externally lift is exported time (critical value of the maximum centripetal acceleration provided of position gravitation); F=kmv
2-mg; In above formula: F for the lift m externally provided be the quality of annulus, v is the linear velocity of annulus, and k is the gravitational field curvature of position, and g is the gravitational acceleration of position; Changed the rotative speed 1 of annulus by external force, need external force to keep the axis L of rotating ring to point to the center of circle and the earth's core O of gravitational field radius of curvature simultaneously, aircraft just can be made to move between different gravitational field curved surfaces.
The material of the rotating ring of described prevailing quality distribution is macroscopic material or the microcosmic particle with rest mass.
The described microcosmic particle with rest mass comprises proton or electronics.
The rotating ring of described prevailing quality distribution is undertaken accelerating by the assistive drive coil in drive motor or supplementary module;
Wherein supplementary module comprises, assistive drive coil, energy regenerating coil and magnetic suspension, restraint device, stabilizing device, measurement and control setup, magnetic suspension in supplementary module, restraint device, stabilizing device, measurement and control setup make the annulus of High Rotation Speed stablize, in order to prevent annulus and windage from generating heat, the rotating ring of prevailing quality distribution is sealed in vacuum (-tight) housing; Energy regenerating coil when the rotating ring of prevailing quality distribution needs to slow down in supplementary module is used for reclaiming kinetic energy.
Described replaces straight-line motion with circular movement, when it is with time on board the aircraft, needs reverse dicyclo or driving engine more than two to offset the antagonistic force of rotating ring rotation and the deflecting force of earth rotation of prevailing quality distribution.This driving engine only provides lift and antigravity, also needs other forms of driving engine to keep flight attitude and heading on board the aircraft.
Advantageous effect of the present invention is:
The present invention seeks to replace straight-line motion with circular movement, when gravitation cannot provide the centripetal acceleration relative to center of attraction, provide antigravity, to reach the effect of gravitational field Curvature-driven engine.Adopt the linear velocity of rotating object to overcome the mode of gravitation, can use in endoatmosphere and outer space.The present invention does not need overwork medium, provides thrust, and capacity weight is improved greatly significantly.Be applicable to the gravitational field that any curvature is greater than zero, as driving engine, aircraft and closed-center system.
Below in conjunction with drawings and Examples, the present invention is further detailed explanation.
Accompanying drawing explanation
Fig. 1 is principle of the invention schematic diagram;
Fig. 2 is rotating part schematic diagram of the present invention;
Fig. 3 is practical application schematic diagram of the present invention.
In figure: the rotating ring 1 of prevailing quality distribution, the spoke 2 of support and fastening effect, the center 3 of rotation, main shaft 4, drive motor 5, supplementary module 6, vacuum (-tight) housing 7, the earth's core O, Deng gravitation curvature of a curve radius R, gravitational field Curvature-driven engine rotating part linear velocity is V, the axis L of rotating ring.
Detailed description of the invention
The present invention is a kind of method of gravitational field Curvature-driven engine.Be replace straight-line motion with circular movement, when gravitation cannot provide the centripetal acceleration relative to center of attraction, provide antigravity.
Gravitational field one word refers in particular to the gravitational field of the earth.Gravitational field is the field that description one particle is subject to gravitation in space.Any have the object of quality all can produce gravitational field.Intensity of a gravitational field is defined as:
Wherein, E intensity of a gravitational field is F is the gravitation that particle m is subject in field.Because space is continuous print, so wait gravitation line to be also continuous print.
Because the law of universal gravitation is mentioned:
Therefore can be write as again:
Here m be send the mass of object of gravitational field, r be from the distance of this object, G be universal gravitational constant.The unit of intensity of a gravitational field is N kg
-1.
As shown in Figure 1, Fig. 1 is principle of the invention schematic diagram.In FIG: comprise the earth's core O, wait gravitation curvature of a curve radius R, gravitational field Curvature-driven engine rotating part linear velocity V, the axis L of rotating ring, the rotating ring 1 of prevailing quality distribution.
For the earth, the curvature of earth surface is about k=1/6.4*10
6rice
-1, the object of moving linearly, curvature k=0, the object moved in a circle on ground level thus is also 0 relative to the curvature in the earth's core.The terrestrial attraction be subject to when the particle of a circular movement on that plane is thus mg, so when the speed of this particle is greater than
time (i.e. the first cosmic velocity), centnifugal force is greater than this particle of terrestrial attraction and starts to provide lift.When all particles relative to the centnifugal force in the earth's core make a concerted effort the total force being greater than aircraft time, aircraft just can leave ground.
In above-mentioned formula: v
0represent minimum line speed; G represents the acceleration due to gravity of earth surface; K represents gravitational field curvature.
The gravitation face of waiting of earth surface (other celestial bodies comparatively far away, affect less) is an approximate ball, and gravitational field Curvature-driven current reference is the annulus of a High Rotation Speed tangent with gravitation face such as grade, when the linear velocity of annulus is greater than v
0time, gravitational field Curvature-driven engine starts to play antigravity effect.
Utilize plane of rotation curvature to be approximately zero curved surface being less than gravitational field curved surface as the rotative speed v of the rotating ring 1 of prevailing quality distribution and be greater than v
0externally lift is exported time (critical value of the maximum centripetal acceleration provided of position gravitation).
F＝kmv
2-mg；
In above formula: F for the lift m externally provided be the quality of annulus 1, v is the linear velocity of annulus 1, and k is the gravitational field curvature of position, and g is the gravitational acceleration of position.
Changed the rotative speed of annulus by external force, need external force to keep the axis L of rotating ring to point to the center of circle and the earth's core O of gravitational field radius of curvature simultaneously, aircraft just can be made to move between different gravitational field curved surfaces.
Rotating part schematic diagram of the present invention is as Fig. 2, and this figure is only principle of specification.Figure comprises: the rotating ring 1 of prevailing quality distribution, and the spoke 2 of support and fastening effect and the center 3 of rotation, the center 3 of rotation can be bearing.
Prevailing quality concentrates on the rotating ring 1 of prevailing quality distribution of rotation, and material also can be able to be microcosmic particle with rest mass for macroscopic material, as proton or electronics.
As shown in Figure 3, Fig. 3 is practical application schematic diagram of the present invention, the non-design drawing of this figure, is only principle of specification.Figure comprises: the rotating ring 1 of prevailing quality distribution, main shaft 4, drive motor 5, supplementary module 6, vacuum (-tight) housing 7.
Wherein supplementary module 6 comprises, assistive drive coil, energy regenerating coil and magnetic suspension, restraint device, stabilizing device, measurement and control setup, the rotating ring 1 of prevailing quality distribution is accelerated with the assistive drive coil in drive motor 5 or supplementary module 6, magnetic suspension in supplementary module 6, restraint device, stabilizing device, measurement and control setup make the annulus of High Rotation Speed stablize, in order to prevent annulus and windage from generating heat, the rotating ring 1 of prevailing quality distribution is sealed in vacuum (-tight) housing 7.Energy regenerating coil when the rotating ring 1 of prevailing quality distribution needs to slow down in supplementary module 6 is used for reclaiming kinetic energy.
The antagonistic force rotated with the rotating ring 1 needing reverse dicyclo or driving engine more than two to offset prevailing quality distribution on board the aircraft and the deflecting force of earth rotation.This driving engine only provides lift (antigravity), also needs other forms of driving engine to keep flight attitude and heading on board the aircraft.
The present invention adopts the linear velocity of rotating object to overcome the mode of gravitation, and can use in endoatmosphere and outer space, without the need to overwork medium, capacity weight is significantly improved.
Claims (7)
1. the method for gravitational field Curvature-driven engine, is characterized in that: replace straight-line motion by circular movement, when gravitation cannot provide the centripetal acceleration relative to center of attraction, provides antigravity.
2. the method for gravitational field Curvature-driven engine according to claim 1, is characterized in that: described with circular movement replacement straight-line motion is: the curvature of earth surface is about k=1/6.4*10
6rice
-1, the object of moving linearly, curvature k=0, the object moved in a circle on ground level thus is also 0 relative to the curvature in the earth's core; The terrestrial attraction be subject to when the particle of a circular movement on that plane is thus mg, so when the speed of this particle is greater than
meter per second, namely during the first cosmic velocity, centnifugal force is greater than this particle of terrestrial attraction and starts to provide lift; When all particles relative to the centnifugal force in the earth's core make a concerted effort the total force being greater than aircraft time, aircraft leaves ground;
In above-mentioned formula: v
0represent minimum line speed; G represents the acceleration due to gravity of earth surface; K represents gravitational field curvature.
3. the method for gravitational field Curvature-driven engine according to claim 2, it is characterized in that: the gravitation face of waiting of described earth surface is an approximate ball, gravitational field Curvature-driven current reference be one with the annulus waiting the tangent High Rotation Speed in gravitation face, when the linear velocity of the rotating ring (1) of prevailing quality distribution is greater than v
0time, gravitational field Curvature-driven engine starts to play antigravity effect;
Utilize plane of rotation curvature to be approximately zero curved surface being less than gravitational field curved surface as the rotative speed v of annulus and be greater than v
0externally lift is exported time (critical value of the maximum centripetal acceleration provided of position gravitation);
F＝kmv
2-mg；
In above formula: F for the lift m externally provided be the quality of annulus (1), v is the linear velocity of annulus 1, and k is the gravitational field curvature of position, and g is the gravitational acceleration of position;
Changed the rotative speed of annulus by external force, need external force to keep the axis L of rotating ring to point to the center of circle and the earth's core O of gravitational field radius of curvature simultaneously, aircraft just can be made to move between different gravitational field curved surfaces.
4. the method for gravitational field Curvature-driven engine according to claim 2, is characterized in that: the material of the rotating ring (1) of described prevailing quality distribution is macroscopic material or the microcosmic particle with rest mass.
5. the method for gravitational field Curvature-driven engine according to claim 4, is characterized in that: the described microcosmic particle with rest mass comprises proton or electronics.
6. the method for gravitational field Curvature-driven engine according to claim 3, is characterized in that: the rotating ring (1) of described prevailing quality distribution is undertaken accelerating by the assistive drive coil in drive motor (5) or supplementary module (6);
Wherein supplementary module (6) comprises, assistive drive coil, energy regenerating coil and magnetic suspension, restraint device, stabilizing device, measurement and control setup, magnetic suspension in supplementary module (6), restraint device, stabilizing device, measurement and control setup make the annulus of High Rotation Speed stablize, in order to prevent annulus and windage from generating heat, the rotating ring (1) of prevailing quality distribution is sealed in vacuum (-tight) housing (7); Energy regenerating coil when the rotating ring 1 of prevailing quality distribution needs to slow down in supplementary module (6) is used for reclaiming kinetic energy.
7. the method for gravitational field Curvature-driven engine according to claim 1, it is characterized in that: described replaces straight-line motion with circular movement, when it is with time on board the aircraft, need reverse dicyclo or driving engine more than two to offset the antagonistic force of rotating ring 1 rotation and the deflecting force of earth rotation of prevailing quality distribution.This driving engine only provides lift and antigravity, also needs other forms of driving engine to keep flight attitude and heading on board the aircraft.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410804269.5A CN104608940A (en) | 2014-12-22 | 2014-12-22 | Method for driving engine by means of gravitational field curvature |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410804269.5A CN104608940A (en) | 2014-12-22 | 2014-12-22 | Method for driving engine by means of gravitational field curvature |
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| CN104608940A true CN104608940A (en) | 2015-05-13 |
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| CN201410804269.5A Pending CN104608940A (en) | 2014-12-22 | 2014-12-22 | Method for driving engine by means of gravitational field curvature |
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| DE3100233A1 (en) * | 1981-01-07 | 1982-07-22 | Stefan 8000 München Bernecker | Antigravity gyroscope |
| DE29715430U1 (en) * | 1997-04-02 | 1997-12-11 | Kaehler Kai | Aircraft with a buoyancy unit |
| FR2757824A1 (en) * | 1996-12-31 | 1998-07-03 | Europ Propulsion | METHOD AND SYSTEM FOR LAUNCHING SATELLITES ON NON-COPLANAR ORBITS USING LUNAR GRAVITATIONAL ASSISTANCE |
| US6116545A (en) * | 1998-04-09 | 2000-09-12 | Hughes Electronics Corporation | Free return lunar flyby transfer method for geosynchronous satellites |
| US20030006929A1 (en) * | 2000-03-07 | 2003-01-09 | Guanghua Huang | Experimental arrangements for measuring propagation speed of variational gravitational field |
| GB2403699A (en) * | 2003-01-08 | 2005-01-12 | Richard Kay | Anti-gravity drive |
| EP1679259A2 (en) * | 2005-01-06 | 2006-07-12 | Kawaguchi, Junichiro | Method of injecting plurality of spacecrafts into different orbits individually |
| CN101186236A (en) * | 2007-12-26 | 2008-05-28 | 北京控制工程研究所 | Orbit changing method for reducing space craft gravity loss |
| CN102935898A (en) * | 2012-11-30 | 2013-02-20 | 清华大学 | On-orbit flight verification method for universal gravitation perturbation of spatial pure gravitational orbit |
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Patent Citations (10)
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| DE3100233A1 (en) * | 1981-01-07 | 1982-07-22 | Stefan 8000 München Bernecker | Antigravity gyroscope |
| FR2757824A1 (en) * | 1996-12-31 | 1998-07-03 | Europ Propulsion | METHOD AND SYSTEM FOR LAUNCHING SATELLITES ON NON-COPLANAR ORBITS USING LUNAR GRAVITATIONAL ASSISTANCE |
| DE29715430U1 (en) * | 1997-04-02 | 1997-12-11 | Kaehler Kai | Aircraft with a buoyancy unit |
| US6116545A (en) * | 1998-04-09 | 2000-09-12 | Hughes Electronics Corporation | Free return lunar flyby transfer method for geosynchronous satellites |
| US20030006929A1 (en) * | 2000-03-07 | 2003-01-09 | Guanghua Huang | Experimental arrangements for measuring propagation speed of variational gravitational field |
| GB2403699A (en) * | 2003-01-08 | 2005-01-12 | Richard Kay | Anti-gravity drive |
| EP1679259A2 (en) * | 2005-01-06 | 2006-07-12 | Kawaguchi, Junichiro | Method of injecting plurality of spacecrafts into different orbits individually |
| CN101186236A (en) * | 2007-12-26 | 2008-05-28 | 北京控制工程研究所 | Orbit changing method for reducing space craft gravity loss |
| RU2478063C1 (en) * | 2011-07-20 | 2013-03-27 | Открытое акционерное общество "Ракетно-космическая корпорация "Энергия" имени С.П. Королева" | Space system for production of materials in space |
| CN102935898A (en) * | 2012-11-30 | 2013-02-20 | 清华大学 | On-orbit flight verification method for universal gravitation perturbation of spatial pure gravitational orbit |
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Application publication date: 20150513 |
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