CN109737024A - A kind of photon thrust superposition aircraft propulsion system - Google Patents
A kind of photon thrust superposition aircraft propulsion system Download PDFInfo
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- CN109737024A CN109737024A CN201910175501.6A CN201910175501A CN109737024A CN 109737024 A CN109737024 A CN 109737024A CN 201910175501 A CN201910175501 A CN 201910175501A CN 109737024 A CN109737024 A CN 109737024A
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- 239000011797 cavity material Substances 0.000 claims description 19
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- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 claims description 3
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- 230000008901 benefit Effects 0.000 claims description 2
- 238000005516 engineering process Methods 0.000 abstract description 9
- 238000011160 research Methods 0.000 abstract description 4
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- 238000000034 method Methods 0.000 description 5
- 239000000446 fuel Substances 0.000 description 2
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- 238000005259 measurement Methods 0.000 description 1
- 230000000505 pernicious effect Effects 0.000 description 1
- 239000003380 propellant Substances 0.000 description 1
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Abstract
The invention discloses a kind of photon thrusts to be superimposed aircraft propulsion system, belongs to aerospace field, and in particular to photon thrust is superimposed aircraft propulsion system.All carried out research to no working medium Push Technology both at home and abroad: according to Einstein theory, nineteen fifty-three is proposed using photon source as the photon rocket of main structural components, unfortunately be that scientific research institution of none country realized photon rocket；2000, Britain it is proposed that it is excessively a kind of with electromagnetic wave be practical working medium electromagnetic drive engine；The U.S. in 2005 and Japan in 2010 develop the solar sail transmitted using photon as working media respectively.Although space flight Push Technology constantly makes progress and develops in recent years, there is no crossing over the raising of property always.The light wave of influence, different-waveband based on photon incidence angle and reflection angle variation to thrust distinguishes the pressure of reflecting surface, reflects thrust superposition theory, propose a kind of photon thrust superposition aircraft propulsion system, it is proposed of the invention and openly technical possibility will be provided for the flight of deep space and ultra-deep sky, while also will found full new growth engines for China's space industry.
Description
Technical field
The present invention relates to aerospace fields to fit more particularly to the propulsion system in aerospace craft engine
It is a kind of new reason of space flight Push Technology for solving the design problem and efficiency of aerospace craft engine propulsion system
By new method.
Background technique
To in this period of the beginning of this century since German Research V1, V2 guided missile during the Second World War, space flight Push Technology
There is no the development of great-leap-forward for theory innovation and technology innovation.Various ballistic missiles, carrier rocket, space shuttle main body push away
It is also built upon into technology on the basis of chemical rocket.The working time of chemical rocket is short but consumption is big, and ion
The very faint demand for being unable to satisfy people at all of the thrust of rocket.
Deep space flight is carried out, traditional chemical rocket has been difficult to take on heavy responsibilities.It is sent out based on photon thrust superimposing technique
The engine of new generation that exhibition is got up, by the interspace destroyer, interspace escort vessel, aircraft carrier, matt to be run in Future Outer Space
The offers such as fast guided missile, deep space unmanned probing device oceangoing voyage power the most basic.
According to Einstein theory, quality and the energy quality that is associated can be converted into kinetic energy, and nineteen fifty-three proposes with light
Component be main structural components photon rocket, unfortunately be none country scientific research institution realized photon fire
Arrow；2000, Britain it is proposed that it is excessively a kind of with electromagnetic wave be practical working medium electromagnetic drive engine, allow electromagnetic wave in a taper
Cavity in launched repeatedly to generate thrust；The U.S. in 2005 and Japan in 2010 develop to transmit respectively to be situated between by work of photon
The solar sail of matter generates thrust using the optical pressure of sunlight and is navigated by water, but this thrust very little.Photon thrust is superimposed aircraft
Propulsion system does not use any chemical fuel and chemical propellant during the work time, and the aggregation that thrust may be implemented obtains
High thrust reaches subvelocity of light flight.
Summary of the invention
In order to make up at present without working medium electromagnetic propulsion technology and ion propulsion technology thrust is small, cruise duration is short defect,
The present invention reflects mechanics principle and thrust superimposing technique using optical pressure as theoretical basis, using photon, devise a kind of structure it is simple,
Easy to operate, energy-saving and environment-friendly photon thrust is superimposed aircraft propulsion system, realizes and is pushed away greatly by the generation of small input power
Power, it is hereby achieved that big acceleration, makes to can achieve high speed in the propulsion system short time, and do not use and appoint during this
What chemical fuel, will not generate any pernicious gas.
In order to achieve the above objectives, the technical solution adopted in the present invention includes:
A kind of photon thrust superposition aircraft propulsion system, a thrust unit include (1) remaining light recover, (2) recycling
Generator, (3) (6) reflecting plate, (4) (12) reflection adjustment mirror, (5) (14) light filling transmitter, (7) turning joint, (8) vacuum
Pump, (9) promote mainly light source, (10) power supply assembly, (11) control module, (13) cable, (15) photon thrust and are superimposed power cavity；Institute
Propulsion system is stated to be formed by 10000 independent thrust unit stack combinations, for convenience of introduce the present invention by principle by its
It is specific to divide quinquepartite.
A kind of above-mentioned photon thrust is superimposed aircraft propulsion system, and (9) promote mainly the light that light source transmission power is 1.5KW
Wave is radiated on (6) reflecting plate, and by an optical pressure is obtained after the total reflection of (6) reflecting plate, (light is oblique incidence to light wave herein, is obtained
To optical pressure need actual measurement and calculating), and so on light wave constantly reflect in the cavity, each reflecting plate just optical pressure not
Disconnected gathering together acts on entire cavity.
A kind of above-mentioned photon thrust is superimposed aircraft propulsion system, promotes mainly light wave due to reflection efficiency problem and passes through every time
After crossing figure (6) baffle reflection, the heat that part energy is changed into mirror surface will necessarily be lost, at this time the transmitter meeting of (5) light filling
According to the energy lost after several secondary reflections in front, being automatically replenished photon makes the light wave power after supplementing photon still be 1.5KW.
A kind of above-mentioned photon thrust is superimposed aircraft propulsion system, it is main enter light wave with fill into light wave both sides' incidence angle
Degree may not be consistent, and the two needs to do a secondary light wave angle by (12) reflection adjustment mirror with angle regulation function before merging
Adjustment, so
Complete to merge afterwards, and so on featured light wave constantly reflect in the cavity, and supplemented.
A kind of above-mentioned photon thrust is superimposed aircraft propulsion system, since light wave needs to keep direction one in the cavity
Show and be converted into thermal energy to reduce luminous energy to the greatest extent, air in cavity is detached by (8) vacuum pump, obtains a vacuum
Space.
A kind of above-mentioned photon thrust is superimposed aircraft propulsion system, according to the currently known earth at a distance from the sun,
The optical pressure that the earth obtains is 0.4 gram, and the optical pressure that such mirror-reflection obtains is very small, and photon thrust superposition engine is set
Counting overall length is 150 meters, can once calculate to obtain 1200 grams of thrusts according to the reflection of every 5 cm distance, thrust unit sectional area is
36 square centimeters, 10000 thrust units are superimposed to form available 12 tons of the thrust of an engine assembly, due to photon
Incident angle problem calculates the half that can at least obtain vertical incidence thrust, converts into the thrust after calculating for 6 tons.
Technical characteristics of the present invention are summarized as follows:
It 150 meters of propulsion system total length, is formed by 10000 thrust unit stack combinations, the cross-sectional area of single thrust unit
For 6X6=36 square centimeter.The light wave that featured light source transmission power is 1.5KW, light wave power after reflection can be lost, light filling
The power that transmitter supplement loses makes power be maintained at 1.5KW.Main incident ray and benefit angle of incident light have deviation, instead
It penetrates adjustment mirror and completes light angle adjustment, keep two light angles consistent.It is carbon fiber that photon thrust, which is superimposed power cavity cavity material,
It ties up, vacuumizes in cavity to reduce energy loss.
Detailed description of the invention
In order to illustrate more clearly of technical solution of the present invention, attached drawing is special to the technology of the present invention in conjunction with specific embodiments hereinafter
Sign has made further explaination.Used specific embodiment attached drawing first is that can help other field personnel understand the present invention, two
It is that can provide visual reference for designer in the art, technical staff.This part is to the brief of used attached drawing
Illustrate:
Fig. 1 is the structure principle chart of one thrust unit of propulsion system of the present invention；
Fig. 2 is the structural perspective of one thrust unit of propulsion system of the present invention；
Fig. 3 is the more thrust unit superposition two-dimensional representations of propulsion system of the present invention；
Fig. 4 is the more thrust unit assembly schematic three dimensional views of propulsion system of the present invention；
In figure: (1) remaining light recover；(2) generator is recycled；(3) reflecting plate；(4) reflection adjustment mirror；(5) light filling transmitter；
(6) reflecting plate；(7) turning joint；(8) vacuum pump；(9) light source is promoted mainly；(10) power supply assembly；(11) control module；(12) anti-
Penetrate adjustment mirror；(13) cable；(14) light filling transmitter；(15) photon thrust is superimposed power cavity.
Specific embodiment
It is careful below with reference to the preferred embodiment of the invention and attached drawing, be fully described by Design and manufacturing process of the invention.
Firstly, it is necessary to which explanation be institute's preferred embodiment is small-sized photon thrust superposition aircraft thrust power system
System for verifying reasonability, the feasibility of the program, and lays the foundation for the improvement in later period.The purpose of the present invention is improve
The thrust of aircraft propulsion promotes the cruising ability of aircraft.It is former using photon reflection mechanics using optical pressure as theoretical basis
Reason and thrust superimposing technique, each structure in one thrust unit of reasonable Arrangement, carry out master-plan and the rule of thrust cavity
It draws, especially the adjustment of reflecting plate mirror angle and positioning, after debugging good each thrust unit, superposition integrates to obtain total
Propulsion system.Input power is the light wave of 1.5KW, and the sectional area of a thrust unit is 36 square centimeters, selected implementation
Example propulsion system length is about 10 meters.Correlation test is carried out on this propulsion system, is generated after verifying photon reflection
Pressure superposition effect, study the influence to thrust of photon incidence angle and angle of reflection angle change, study the light wave of different-waveband
To the pressure difference of reflecting surface and energy loss problem.
Claims (5)
1. a kind of photon thrust is superimposed aircraft propulsion system, a thrust unit is recycled by (1) remaining light recover, (2)
Generator, (3) (6) reflecting plate, (4) (12) reflection adjustment mirror, (5) (14) light filling transmitter, (7) turning joint, (8) vacuum
Pump, (9) promote mainly light source, (10) power supply assembly, (11) control module, (13) cable, (15) photon thrust superposition power cavity this
A little parts form, it is characterized in that: 150 meters of propulsion system total length, it is formed by 10000 thrust unit stack combinations, promotes mainly light
Source transmission power is the light wave of 1.5KW, and light filling transmitter supplements loss power, and reflection adjustment mirror completes light angle adjustment, light
Sub- thrust superposition power cavity cavity material is carbon fiber, is vacuumized in cavity.
2. a kind of photon thrust according to claim 1 is superimposed aircraft propulsion system, it is characterized in that: propulsion system
It 150 meters of total length, is formed by 10000 thrust unit stack combinations, the cross-sectional area of single thrust unit is 6X6=36 square
Centimetre.
3. a kind of photon thrust according to claim 1 is superimposed aircraft propulsion system, it is characterized in that: featured light source
Transmission power is the light wave of 1.5KW, and light wave power after reflection can be lost, and the power that light filling transmitter supplement loses makes function
Rate is maintained at 1.5KW.
4. a kind of photon thrust according to claim 1 is superimposed aircraft propulsion system, it is characterized in that: main incident light
Line and benefit angle of incident light have deviation, and reflection adjustment mirror completes light angle adjustment, keeps two light angles consistent.
5. a kind of photon thrust according to claim 1 is superimposed aircraft propulsion system, it is characterized in that: photon thrust
Superposition power cavity cavity material is carbon fiber, is vacuumized in cavity to reduce energy loss.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910175501.6A CN109737024A (en) | 2019-03-08 | 2019-03-08 | A kind of photon thrust superposition aircraft propulsion system |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910175501.6A CN109737024A (en) | 2019-03-08 | 2019-03-08 | A kind of photon thrust superposition aircraft propulsion system |
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| Publication Number | Publication Date |
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| CN109737024A true CN109737024A (en) | 2019-05-10 |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2022105726A (en) * | 2022-02-02 | 2022-07-14 | 克弥 西沢 | Aerial structure, and space structure |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE1202580B (en) * | 1962-12-19 | 1965-10-07 | Boelkow Gmbh | Engine assembly for recoverable spacecraft |
| CA2489591A1 (en) * | 2002-06-12 | 2003-12-24 | Thomas Sash | Controlable rotorcraft using a pendulum |
| CN103590992A (en) * | 2013-11-30 | 2014-02-19 | 哈尔滨工业大学 | Photon micro propelling device and method based on active resonant cavity |
| GB201713135D0 (en) * | 2017-08-16 | 2017-09-27 | Reaux-Savonte Corey Kaizen | Quantum laser-driven engine |
-
2019
- 2019-03-08 CN CN201910175501.6A patent/CN109737024A/en active Pending
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE1202580B (en) * | 1962-12-19 | 1965-10-07 | Boelkow Gmbh | Engine assembly for recoverable spacecraft |
| CA2489591A1 (en) * | 2002-06-12 | 2003-12-24 | Thomas Sash | Controlable rotorcraft using a pendulum |
| CN103590992A (en) * | 2013-11-30 | 2014-02-19 | 哈尔滨工业大学 | Photon micro propelling device and method based on active resonant cavity |
| GB201713135D0 (en) * | 2017-08-16 | 2017-09-27 | Reaux-Savonte Corey Kaizen | Quantum laser-driven engine |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2022105726A (en) * | 2022-02-02 | 2022-07-14 | 克弥 西沢 | Aerial structure, and space structure |
| WO2023148992A1 (en) * | 2022-02-02 | 2023-08-10 | 克弥 西沢 | Aerial structure |
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