CN106275517A - A kind of moonscape base radioprotector - Google Patents
A kind of moonscape base radioprotector Download PDFInfo
- Publication number
- CN106275517A CN106275517A CN201510272684.5A CN201510272684A CN106275517A CN 106275517 A CN106275517 A CN 106275517A CN 201510272684 A CN201510272684 A CN 201510272684A CN 106275517 A CN106275517 A CN 106275517A
- Authority
- CN
- China
- Prior art keywords
- base
- moonscape
- radioprotector
- cable system
- power supply
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
Abstract
The invention provides a kind of moonscape base radioprotector, described device includes: cable system (2) and power supply (7), and described cable system (2) is the arc net that some plain conductors (6) form;Cover on the building surface of moonscape base (1);Described power supply (7) is connected with cable system (2), for providing electric current for cable system (2);When all plain conductors (6) loading current, magnetic field can be produced and form field region around;So that ultra rays deflect away from base building, play the effect of protection radiation.Assembly of the invention has simple in construction, low cost, the feature easily realized;Utilize the moonscape base radioprotector of the present invention, can effectively reduce equipment and radiation that personnel are suffered, provide condition for the safe operation of moonscape base.
Description
Technical field
The present invention relates to the radiation protection technique of manned deep space space flight, particularly relate to the radiation of a kind of moonscape base anti-
Protection unit.
Background technology
Particle Environment near the moon (includes the secondary near by the deep space Particle Environment of lunar effect and menology
Environment), the galactic comic ray (GCR) of interplanetary space, solar energetic particles (SEP) be all the heat of current research
Point.Extraterrestrial ultra rays include galactic comic ray and solar cosmic ray, may to spacecraft and spacefarer
Cause radiation damage, especially in the case of the survey of deep space protected departing from earth magnetosphere, the radiation problem of ultra rays
Unavoidably.The produced harm of Radiation On Human body can be divided into early effect and remote effect two kinds according to time of occurrence:
Early effect can cause nausea and vomiting, suffer from diarrhoea, has blood in stool, is dehydrated, collapses and the acute effect such as shock, even results in
Personnel death;It is remote effect that spacefarer endangers maximum, wherein the most dangerous with cancer, next to that nervus centralis
The damage of system, the 3rd is hereditary effect.Therefore for solving the radiation such as the space ultra rays personnel for manned space flight
The threat brought is run, it is necessary to the radiation being suffered the base being in moonscape is protected with equipment.
The universal means protected space radiation at present is to increase shielding thickness, there is the problem that owing to increasing
Add the space flight amount of thinking highly of thus cause launch cost to increase.
Summary of the invention
It is an object of the invention to the drawbacks described above overcoming the method at present space radiation protected to exist, propose
A kind of moonscape base radioprotector, this preventer utilizes plain conductor loading current to produce magnetic field,
Thus charged radiating particle is carried out deflection and expels.
To achieve these goals, the present invention proposes a kind of moonscape base radioprotector, described device
Including: cable system 2 and power supply 7, described cable system 2 is the arc net of some plain conductor 6 compositions;Cover
On the building surface in moonscape base 1;Described power supply 7 is connected with cable system 2, for providing for cable system 2
Electric current;When all plain conductor 6 loading currents, magnetic field can be produced and form field region around.
In technique scheme, the outer surface of described plain conductor 6 is cased with sheath 5.
In technique scheme, the sense of current in described plain conductor 6 is consistent.
In technique scheme, the quantity of described plain conductor 6 is no less than 2.
In technique scheme, in described plain conductor 6, electric current is not less than 1A.
In technique scheme, the resistivity of described plain conductor 6 is not more than 10-6Ωm。
In technique scheme, the sectional area of described plain conductor 6 is not less than 1cm2。
It is an advantage of the current invention that:
1, utilize the moonscape base radioprotector of the present invention, can effectively reduce equipment and personnel are suffered
Radiation, for the safe operation of moonscape base provide condition;
2, assembly of the invention has simple in construction, low cost, the feature easily realized.
Accompanying drawing explanation
Fig. 1 is the composition schematic diagram of the moonscape base radioprotector of the present invention;
Fig. 2 is that the moonscape base radioprotector of the present invention deflects showing of expelling to space radiation particle
It is intended to;
Fig. 3 is the A-A generalized section of Fig. 1;
Fig. 4 is the cable system of the radioprotector of the present invention schematic top plan view on building surface, base;
Fig. 5 is the electric theory diagram of the radioprotector of the present invention.
Reference:
1, moonscape base 2, cable system 3, cosmic-ray particle
4, the moon 5, sheath 6, plain conductor
7, power supply 8, current monitor
Detailed description of the invention
The present invention will be described in detail with preferred embodiment below in conjunction with the accompanying drawings.
As it is shown in figure 1, a kind of moonscape base radioprotector, described device includes: cable system 2 and electricity
Source 7, described cable system 2 is the arc net of some plain conductor 6 compositions;Cover building in moonscape base 1
Build on surface;Described power supply 7 is connected with cable system 2, for providing electric current for cable system 2.
As in figure 2 it is shown, when all plain conductor 6 loading currents, magnetic field can be produced and forms field regions around
Territory, so that ultra rays deflect away from base building, plays the effect of protection radiation;
The outer surface of the most described plain conductor 6 is cased with sheath 5, it is to avoid metal is directly exposed to space ion
Body causes current loss.The sense of current in described plain conductor 6 is consistent, it is to avoid owing to the sense of current is inconsistent
Magnetic field shielding effect is caused to reduce.
As shown in Figure 4, it is preferable that the quantity of described plain conductor 6 is no less than 2, to form the biggest preventing
Mask amasss.
In the present embodiment, when in described plain conductor 6, electric current is 53.8 megamperes (MA), can make to deflect
Proton energy reach 300MeV.
Preferably, the material of described plain conductor 6 is copper.
Preferably, the resistivity of described plain conductor 6 is 1.76 × 10-8Ω m, it is to avoid the heat consumption caused due to resistance
Excessive.
Preferably, the sectional area of described plain conductor 6 is 1cm2, it is to avoid owing to conductor cross-section is too small and it is lost excessive.
As it is shown in figure 5, described device also includes current monitor 8, for monitoring the electric current in plain conductor 6.When
Power supply 7 exports current load and flows in the plain conductor 6 covering building surface, base, it is possible to producing about
Magnetic field, the action of a magnetic field orders about charged particle in the Lorentz force of cosmic-ray particle and deflects, thus decreases directly
The number of particles of incident base building, thus equipment and personnel are played protective action.
It should be noted last that, above example is only in order to illustrate technical scheme and unrestricted.Although
With reference to embodiment, the present invention is described in detail, it will be understood by those within the art that, to the present invention
Technical scheme modify or equivalent, without departure from the spirit and scope of technical solution of the present invention, it is equal
Should contain in the middle of scope of the presently claimed invention.
Claims (7)
1. a moonscape base radioprotector, described device includes: cable system (2) and power supply (7),
It is characterized in that, described cable system (2) is the arc net that some plain conductors (6) form;Cover at the moon
On the building surface in base, surface (1);Described power supply (7) is connected with cable system (2), is used for as cable system (2)
Electric current is provided;When all plain conductors (6) loading current, magnetic field can be produced and form field region around.
Moonscape base the most according to claim 1 radioprotector, it is characterised in that described metal
The outer surface of wire (6) is cased with sheath (5).
Moonscape base the most according to claim 1 radioprotector, it is characterised in that described metal
The sense of current in wire (6) is consistent.
Moonscape base the most according to claim 1 radioprotector, it is characterised in that plain conductor
(6) quantity is no less than 2.
Moonscape base the most according to claim 1 radioprotector, it is characterised in that described metal
Wire (6) interior electric current is not less than 1A.
Moonscape base the most according to claim 1 radioprotector, it is characterised in that described metal
The resistivity of wire (6) is not more than 10-6Ωm。
Moonscape base the most according to claim 1 radioprotector, it is characterised in that described metal
The sectional area of wire (6) is not less than 1cm2。
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201510272684.5A CN106275517A (en) | 2015-05-25 | 2015-05-25 | A kind of moonscape base radioprotector |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201510272684.5A CN106275517A (en) | 2015-05-25 | 2015-05-25 | A kind of moonscape base radioprotector |
Publications (1)
Publication Number | Publication Date |
---|---|
CN106275517A true CN106275517A (en) | 2017-01-04 |
Family
ID=57634614
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201510272684.5A Pending CN106275517A (en) | 2015-05-25 | 2015-05-25 | A kind of moonscape base radioprotector |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN106275517A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN109974526A (en) * | 2019-04-29 | 2019-07-05 | 北京空间飞行器总体设计部 | A kind of manned moon landing's radiation protection method based on assembling shield |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN2424600Y (en) * | 2000-02-27 | 2001-03-21 | 郝明学 | Combination electromagnetic protecting net |
US20100323900A1 (en) * | 2008-12-11 | 2010-12-23 | Mitsubishi Heavy Industries, Ltd. | Superconducting coil apparatus |
US8575580B1 (en) * | 2010-12-13 | 2013-11-05 | The Boeing Company | Radiation shield device and associated method |
CN104464866A (en) * | 2014-12-27 | 2015-03-25 | 王德龙 | Principle of high-energy cosmic-ray shielding device or high-energy proton stream (proton gun or knife) emitter |
-
2015
- 2015-05-25 CN CN201510272684.5A patent/CN106275517A/en active Pending
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN2424600Y (en) * | 2000-02-27 | 2001-03-21 | 郝明学 | Combination electromagnetic protecting net |
US20100323900A1 (en) * | 2008-12-11 | 2010-12-23 | Mitsubishi Heavy Industries, Ltd. | Superconducting coil apparatus |
US8575580B1 (en) * | 2010-12-13 | 2013-11-05 | The Boeing Company | Radiation shield device and associated method |
CN104464866A (en) * | 2014-12-27 | 2015-03-25 | 王德龙 | Principle of high-energy cosmic-ray shielding device or high-energy proton stream (proton gun or knife) emitter |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN109974526A (en) * | 2019-04-29 | 2019-07-05 | 北京空间飞行器总体设计部 | A kind of manned moon landing's radiation protection method based on assembling shield |
CN109974526B (en) * | 2019-04-29 | 2021-07-13 | 北京空间飞行器总体设计部 | Manned lunar landing radiation protection method based on assembly shield |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
JP6856248B2 (en) | Lightning strike suppression type lightning rod | |
ECSP19011192A (en) | SHIELDED SUBMERSIBLE POWER CORD | |
MX2020002195A (en) | Fire-resistant energy storage devices and associated systems and methods. | |
CN106275517A (en) | A kind of moonscape base radioprotector | |
US9036323B1 (en) | Power feeder shielding for electromagnetic protection | |
US20160378148A1 (en) | Electromagnetic Pulse Protected Cable | |
US9420733B2 (en) | Electromagnetic pulse protected hard drive | |
Patil | Substation Earthing Design | |
Avakyan et al. | Possibilities of the forecast of generation of the high energy solar protons for the safety of Mars mission | |
Calvelli et al. | Space radiation superconducting shields | |
Dicarolo | Galactic cosmic rays dose mitigation inside a spacecraft by a superconductor “compact” toroid: A FLUKA Monte Carlo study | |
CN104901227A (en) | Hard insulating shield cover specialized for 35kV live operation | |
CN207854406U (en) | A kind of ultra-high voltage converter station valve Room double layer screen cage | |
Ballarino et al. | Powering the high-luminosity triplets | |
Townsend et al. | Radiation protection effectiveness of a proposed magnetic shielding concept for manned Mars missions | |
CN109974526B (en) | Manned lunar landing radiation protection method based on assembly shield | |
Bhatia et al. | Safety analysis of TN-S and TN-CS earthing system | |
DK180143B1 (en) | Fire-resistant energy storage devices and associated systems and methods | |
Spunei et al. | Finding the Minimal Fitting Distance of a Lightning Rod Down-Conductor | |
Peterlin | Guidelines for electromagnetic compatibility provision in power plants and substations | |
US20160261094A1 (en) | Designs and arrangements of electrical power distribution units for attenuation of magnetic fields | |
US20170005253A1 (en) | Radiance Capture Techonolgy | |
Zou et al. | A Novel Collimation Method for Large Hadron Colliders | |
Peroni | Martian Modular Base | |
Pan et al. | The Electromagnetic Protection Method on the Guided Ammunition |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
C06 | Publication | ||
PB01 | Publication | ||
C10 | Entry into substantive examination | ||
SE01 | Entry into force of request for substantive examination | ||
RJ01 | Rejection of invention patent application after publication | ||
RJ01 | Rejection of invention patent application after publication |
Application publication date: 20170104 |