CN102310940A - Space station - Google Patents
Space station Download PDFInfo
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- CN102310940A CN102310940A CN2010102280441A CN201010228044A CN102310940A CN 102310940 A CN102310940 A CN 102310940A CN 2010102280441 A CN2010102280441 A CN 2010102280441A CN 201010228044 A CN201010228044 A CN 201010228044A CN 102310940 A CN102310940 A CN 102310940A
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Abstract
The invention discloses a space station. The space station is arranged in an atmospheric layer. The space station comprises a support part, an energy part, a power part, an ecological residence part, a communication part, a detection part, a weapon part, a transport part, a lightening-protection part and an escape system part. The invention has the advantages that: by the space station built in the atmospheric layer, a radar detection range is widened, and the space station can work under all weather.
Description
Technical field
The present invention relates to a kind of space station, the space station that particularly a kind of atmospheric envelope is inner.
Background technology
We need make the sea level elevation of radar set high as much as possible.
Early warning plane can be surveyed the target in the defence area as a kind of radar set of flight effectively.But early warning plane can not all weather operations, the involving great expense of early warning plane.
Imagination: if the inner space station of a kind of atmospheric envelope is arranged then can solve the above problems.
Summary of the invention
The present invention forms in view of such problem, and provides a kind of atmospheric envelope inner space station, is intended to through building the inner space station of a kind of atmospheric envelope, to solve existing radar detection problem.
Technical solution of the present invention is following:
A kind of space station, this space station comprises:
Support section, this support section comprises: rope, the parts of power straight up are provided;
Energy part changes Department of Energy's branch and comprises: wind power generation plant, device of solar generating, ground transmission system, diesel power plant, gasoline power generation assembly, storage battery or its combination;
Power pack section, this power pack section comprises: screw propeller engine installation, jet engine or its combination;
Ecological inhabitation part, the ecological part of living comprises: humidity control apparatus, temperature control equipment, air conditioning equipment, light adjusting device, rain collector, lounge, work stall or its combination;
Communication part, this communication part comprises: wire communication device, wireless communication apparatus, navigation mark or its combination;
Probe portion, this probe portion comprises: radar detection apparatus, wireless monitoring device, sonar detection device, light detection device or its combination;
The weapon part, this weapon partly comprises: antiaircraft weapon, vacant lot weapon, machine gun, gun or its combination;
Transport section, this transport section comprises: jacking system;
Lightning-arrest part, this lightning-arrest part comprises: discharging rod and cable;
The escape device part, this escape device comprises: parachute, blimp, glider or its combination.
In a kind of space station of the present invention, comprise three at least with ground bonded assembly rope in the said rope.
In a kind of space station of the present invention, the said parts of power straight up that provide comprise: helium balloon, hydrogen balloon or its combination.
In a kind of space station of the present invention, said ground transmission system is through the cable transmission electric energy, and this cable is along said rope cabling.
In a kind of space station of the present invention, said power pack section is installed in this space station that guarantees to deal with storm of said space station all around and does not squint as much as possible.
In a kind of space station of the present invention, said rain collector comprises baffle plate and the water storage container that is looped around around the said space station.
In a kind of space station of the present invention, said space station be shaped as the bowl structure that tips upside down on the horizontal surface, the line segment ED among Fig. 1 is less than the camber line EGD among Fig. 1.
In a kind of space station of the present invention, said hydrogen balloon comprises: one or more, said helium balloon comprises: one or more.
Advantage of the present invention: the present invention makes that through building the inner space station of a kind of atmospheric envelope the scope of radar detection is openr, and can all weather operations.
Description of drawings
Fig. 1 is the schematic configuration scheme drawing of a kind of space station of the present invention.
The figure number explanation:
Line segment AE: rope
Line segment BF: rope
Line segment CD: rope
Line segment GJ: rope
Line segment GK: rope
Line segment HE: baffle plate
Line segment DI: baffle plate
Figure EFDG: spatial bins
Point A: the fulcrum of stationary rope
Point B: the fulcrum of stationary rope
Point C: the fulcrum of stationary rope
1: balloon
The specific embodiment
The preferred forms that is used for embodiment of the present invention below according to description of drawings.
Fig. 1 shows the schematic configuration scheme drawing of a kind of space station of the present invention.
Space station of the present invention comprises as follows:
Support section, this support section comprises: rope, the parts of power straight up are provided; The maximum of this rope is born pulling force need be big as much as possible, so that make all ropes all be in the tensioned state under the big pulling force, and make spatial bins EFDG stable as much as possible; At least comprise three with ground bonded assembly rope in this rope, so that make spatial bins be in stabilized conditions more easily; The said parts of power straight up that provide comprise: hydrogen balloon, helium balloon or its combination, and generally we adopt helium balloon, because helium balloon is more secure and reliable to use; Generally we adopt the combination conduct of a plurality of balloons that the parts of power straight up are provided, so that failure-free pulling force more is provided, even after one of them perhaps several balloon damages, can also make this parts keep operation.
Energy part, this Department of Energy (DOE) divides and comprises: wind power generation plant, device of solar generating, ground transmission system, diesel power plant, gasoline power generation assembly, storage battery or its combination; Generally we adopt wind power generation plant, device of solar generating, ground transmission system and the storage battery composition as this part; Because can obtain energy at an easy rate at aerial wind power generation plant of height and device of solar generating; Because it is this spatial bins is passed through lanyard on the ground, so also very convenient ground-surface electric energy transmitting to space station through cable.
Power pack section, this power pack section comprises: screw propeller engine installation, jet engine or its combination; This power pack section be installed in spatial bins EFDG around guarantee that to deal with storm this spatial bins does not squint as much as possible; Because when this space station is crossed in big wind; Can make this space station overall offset; When surpassing the amplitude that is allowed to, just need to promote this spatial bins, so that this spatial bins is returned in the scope that is allowed to through power pack section.
Ecological inhabitation part, the ecological part of living comprises: humidity control apparatus, temperature control equipment, air conditioning equipment, light adjusting device, rain collector, lounge, work stall or its combination; Owing to be in high altitude environment; The environment of high altitude environment is abominable: the time and when dry and moist, temperature is lower, oxygen content is not enough, solar radiation is strong, do not have tap water etc., so we need corresponding humidity control, adjustment, air regulation, light adjusting and rainwater collection etc.; The rainwater harvester is to gather and preserve rainwater through being looped around said spatial bins EFDG ring baffle and water storage container all around.
Communication part, this communication part comprises: wire communication device, wireless communication apparatus, navigation mark or its combination; This communication part is used to carry out communication with ground unit or aerial unit, and navigation mark wherein is used to let other flight unit discern the position of this space station, with the generation of crash-avoidance accident.
Probe portion, this probe portion comprises: radar detection apparatus, wireless monitoring device, sonar detection device, light detection device or its combination; This probe portion be used to through continuously, seamlessly scan with keep watch on the unknown object in this defence area, space station or do not have identity markings object dynamically.
The weapon part, this weapon partly comprises: antiaircraft weapon, vacant lot weapon, machine gun, gun or its combination; This weapon partly is used to defence or implement attacks, and wherein antiaircraft weapon and machine gun are used to hit airbound target, and wherein the vacant lot weapon is used to hit terrain object, and wherein gun are used to this space station and garrison personnel's usefulness of defending oneself.
Transport section, this transport section comprises: jacking system; This jacking system is used to go up and down to travel to and fro between between ground and the spatial bins, so that the goods and materials of spatial bins obtain supplying with.
Lightning-arrest part, this lightning-arrest part comprises: discharging rod and cable; If being struck by lightning in the high-altitude will be a very serious thing, be very crucial part so take shelter from the thunder.
Escape device, this escape device comprises: parachute, blimp, glider or its combination.We can not guarantee that our space station passes away never, so the safety of protection staff and relevant device just seems particularly important, we can make these goods and materials and personnel obtain actv. through escape device to withdraw safely in the time of needs.
Spatial bins EFDG is shaped as the bowl structure that tips upside down on the horizontal surface, and Fig. 1 middle conductor ED is less than Fig. 1 mean line EGD; This structure is used to as wind when the horizontal direction of this spatial bins is blown over, and provides a thrust straight up to guarantee the stable of this spatial bins.
Foregoing description only proposes as a kind of enforceable technical scheme of a kind of space station of the present invention, and conduct is not to its structure or technology limitation condition.
Claims (8)
1. space station, this space station comprises:
Support section, this support section comprises: rope, the parts of power straight up are provided;
Energy part changes Department of Energy's branch and comprises: wind power generation plant, device of solar generating, ground transmission system, diesel power plant, gasoline power generation assembly, storage battery or its combination;
Power pack section, this power pack section comprises: screw propeller engine installation, jet engine or its combination;
Ecological inhabitation part, the ecological part of living comprises: humidity control apparatus, temperature control equipment, air conditioning equipment, light adjusting device, rain collector, lounge, work stall or its combination;
Communication part, this communication part comprises: wire communication device, wireless communication apparatus, navigation mark or its combination;
Probe portion, this probe portion comprises: radar detection apparatus, wireless monitoring device, sonar detection device, light detection device or its combination;
The weapon part, this weapon partly comprises: antiaircraft weapon, vacant lot weapon, machine gun, gun or its combination;
Transport section, this transport section comprises: jacking system;
Lightning-arrest part, this lightning-arrest part comprises: discharging rod and cable;
The escape device part, this escape device comprises: parachute, blimp, glider or its combination.
2. space station according to claim 1 is characterized in that: comprise three at least with ground bonded assembly rope in the said rope.
3. space station according to claim 1 is characterized in that: the said parts of power straight up that provide comprise: helium balloon, hydrogen balloon or its combination.
4. space station according to claim 1 is characterized in that: said ground transmission system is through the cable transmission electric energy, and this cable is along said rope cabling.
5. space station according to claim 1 is characterized in that: said power pack section is installed in this space station that guarantees to deal with storm of said space station all around and does not squint as much as possible.
6. space station according to claim 1 is characterized in that: said rain collector comprises baffle plate and the water storage container that is looped around around the said space station.
7. space station according to claim 1 is characterized in that: said space station be shaped as the bowl structure that tips upside down on the horizontal surface.
8. space station according to claim 3 is characterized in that: said hydrogen balloon comprises: one or more, said helium balloon comprises: one or more.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2010102280441A CN102310940A (en) | 2010-07-08 | 2010-07-08 | Space station |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2010102280441A CN102310940A (en) | 2010-07-08 | 2010-07-08 | Space station |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN102310940A true CN102310940A (en) | 2012-01-11 |
Family
ID=45424582
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2010102280441A Pending CN102310940A (en) | 2010-07-08 | 2010-07-08 | Space station |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN102310940A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105283382A (en) * | 2013-06-19 | 2016-01-27 | 章秀宁 | Flying object operating system |
| CN110816805A (en) * | 2019-11-12 | 2020-02-21 | 洲际联合超伦科技（北京）有限公司 | Tethered balloon task execution system and host system |
| FR3140066A1 (en) * | 2022-09-27 | 2024-03-29 | Edmond Thuries | MESOSPHERIC SENTINEL PLATFORM |
Citations (6)
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| CN1231976A (en) * | 1998-01-28 | 1999-10-20 | 株式会社电通Tec | Tethered balloon |
| CN1243484A (en) * | 1997-06-11 | 2000-02-02 | 末来概念公司 | Aerial cableway leading to aerostatic airborne body |
| CN1470432A (en) * | 2003-06-17 | 2004-01-28 | 威 杨 | Method for building work platform at high-altitude stratosphere |
| CN200941618Y (en) * | 2006-08-29 | 2007-08-29 | 张红彬 | Pre-warning monitoring system based on wired or radio network tech |
| CN101088862A (en) * | 2004-11-03 | 2007-12-19 | 游善宗 | Multipurpose midair gas preparing device |
| US20080265086A1 (en) * | 2007-04-27 | 2008-10-30 | Yee-Chun Lee | Long mission tethered aerostat and method of accomplishing |
-
2010
- 2010-07-08 CN CN2010102280441A patent/CN102310940A/en active Pending
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN1243484A (en) * | 1997-06-11 | 2000-02-02 | 末来概念公司 | Aerial cableway leading to aerostatic airborne body |
| CN1231976A (en) * | 1998-01-28 | 1999-10-20 | 株式会社电通Tec | Tethered balloon |
| CN1470432A (en) * | 2003-06-17 | 2004-01-28 | 威 杨 | Method for building work platform at high-altitude stratosphere |
| CN101088862A (en) * | 2004-11-03 | 2007-12-19 | 游善宗 | Multipurpose midair gas preparing device |
| CN200941618Y (en) * | 2006-08-29 | 2007-08-29 | 张红彬 | Pre-warning monitoring system based on wired or radio network tech |
| US20080265086A1 (en) * | 2007-04-27 | 2008-10-30 | Yee-Chun Lee | Long mission tethered aerostat and method of accomplishing |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105283382A (en) * | 2013-06-19 | 2016-01-27 | 章秀宁 | Flying object operating system |
| CN110816805A (en) * | 2019-11-12 | 2020-02-21 | 洲际联合超伦科技（北京）有限公司 | Tethered balloon task execution system and host system |
| FR3140066A1 (en) * | 2022-09-27 | 2024-03-29 | Edmond Thuries | MESOSPHERIC SENTINEL PLATFORM |
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Addressee: He Rencheng Document name: Notification that Application Deemed to be Withdrawn |
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Application publication date: 20120111 |