CN1470432A - Method for building work platform at high-altitude stratosphere - Google Patents
Method for building work platform at high-altitude stratosphere Download PDFInfo
- Publication number
- CN1470432A CN1470432A CNA031269761A CN03126976A CN1470432A CN 1470432 A CN1470432 A CN 1470432A CN A031269761 A CNA031269761 A CN A031269761A CN 03126976 A CN03126976 A CN 03126976A CN 1470432 A CN1470432 A CN 1470432A
- Authority
- CN
- China
- Prior art keywords
- altitude
- operation platform
- altitude operation
- platform
- advection layer
- 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
Images
Landscapes
- Wind Motors (AREA)
Abstract
The invention refers to air work appliance, which includes following steps: a. constructs mooring pier on ground or under water, sets bearing universal joint on the mooring pier; b. sets air work platform on which there sets bearing universal joint; c. one end of the cable connects to mooring pier, the other end connects to air work platform; d. the air work platform is pulled by copter which is driven by aeroboat, fire balloon or turbine jet engine, makes it located in the stratosphere with the same height to cable; the character is: 1. it can stay in the air for a long time; 2. it can achieves the work in the air; 3. the stay time doesn't need power; 4. the efficient load is large; 5. it can be applies to many fields such as military affairs, aviation, spaceflight, communication and weather and so on.
Description
Technical field:
The present invention relates to aerial work equipment.
Background technology:
By atmospherical vertical stratification, can be divided into convective zone, advection layer, middle level and thermosphere to atmosphere.The bottom of the above atmosphere in ground is called the convective zone, and the air pressure on top, convective zone is about 200hPa, and the height on top, convective zone is higher than winter in summer, near under the line about 17-18 kilometer, and the on average about 10-12 kilometer of middle latitude, high latitude is the 8-9 kilometer.
Is advection layer from the top, convective zone upward to about 50 kilometers.The about 1hPa of air pressure on advection layer top.The lower stratosphere temperature is very little with height change, and high stratosphere is because exist ozone layer (22-35 kilometer place), and ozone absorbs solar ultraviolet radiation increases ambient-air temperature.The inversion structure of this top heat makes the advection layer atmospheric stability, and convection current is very weak, and air moves horizontally mostly.Advection layer aqueous vapor and dust seldom do not have cloud and weather phenomenon in the convective zone yet.In the convective zone, the most basic feature is: atmosphere moves row along the latitude circle direction around the earth substantially, at low latitudes east wind often in vogue, is called as easterlies, is called the trade wind belt again, and the Northern Hemisphere is the northeast trades band, and the southern hemisphere is southeast trade band.Mid latitudes is prevailing westerlies then, is called as the westerlies.Its latitude of striding is than east wind bandwidth.West wind intensity increases with latitude, and strong wind appears near 20,000 handkerchiefs in 30 ° of-40 ° of sky, and both the height that begins of advection layer was called the planet westerly jet.General wind speed can not be lower than 100KM/H.And wind direction and wind speed are all more stable.And it is constant year in year out.
Therefore utilize stratospheric huge and stable wind-force, setting up high-altitude operation platform at advection layer just becomes possibility.This in the high-altitude building flat-bed practice, will be to multi-field, the multi-disciplinary research and development utilization in space, high-altitude, provide and showed fine prospect.
Existing aerial work platform is served as by aircraft, dirigible, fire balloon, and their common feature is movably, the continuous conversion in skyborne position, and because of needs power, the time of leaving a blank is very limited.A lot of aerial works are difficult to once finish, some task even at all can't finish.Though artificial satellite can be done long-time stop aloft, it still is difficult to be competent at apart from the earth some work too far away outside atmospheric envelope.
The objective of the invention is to: need not power after a kind of lift-off is provided, aloft can stop for a long time, at atmospheric envelope with interior a kind of method of building job platform at the high-altitude advection layer of finishing certain regional work.
Summary of the invention:
It comprises following content and step:
A, on ground or submerged structure mooring pier, it is universal on the mooring pier bearing to be set;
B, on ground high-altitude operation platform is set, it is universal that bearing is set on high-altitude operation platform;
C, usefulness hawser one end connect the mooring pier, and the other end connects high-altitude operation platform;
D, the helicopter that is used as power with dirigible, fire balloon or turbojet draw high-altitude operation platform, make its lift-off be positioned hawser with high high-altitude advection layer.
The advection layer of the operating altitude of high-altitude operation platform between the 11.000-30.000M of distance ground.
The mooring pier adopts reinforced concrete structure or other whole weight.
With the universal coupling link of doing of high-intensity bearing, connect mooring pier and high-altitude operation platform flexibly securely and make it can not come off fracture.
Hawser must have sufficient intensity to bear the stressed of the pulling force of high-altitude operation platform and windage, length should adopt the high-strength abrasion-proof corrosion resistant to touch lamination coating at 11.000-30.000M, as: material such as carbon fiber, aramid fiber, must make it can not broken, and lightning protection electric work energy is arranged.
High-altitude operation platform must have aerodynamic performance; The automatic compensation horizontal tail changes lift, by the normal limb orientation, protects special balance automatically, steadily reaches counterweight load, and himself lift should keep equating with its gravity.
High-altitude operation platform is provided with parachute, falls in case high-altitude operation platform is met under the fault, and when the speed of falling instantly surpassed 50 meters of per seconds, parachute was opened automatically, to ensure aerial and ground staff's device security.
On the high-altitude operation platform work stall can be set, lounge, meeting room, the happy chamber of mistake, facility or instrument and equipments such as boarding house, astronomy, meteorology, mapping, communication, navigation, solar electrical energy generation, wind-power electricity generation, power transformation, transmission of electricity, storage battery, lightning-arrest electricity.
The present invention compared with prior art has the following advantages:
1, fixed point remaining aloft in the time of growing;
2, the task that can fulfil assignment in the endoatmosphere;
3, do not need power in the skyborne time of stop;
4, capacity weight is big, and high-altitude operation platform can be accomplished more than the 100T;
5, can in wind-power electricity generation, solar electrical energy generation, military affairs, Aeronautics and Astronautics, communication,
Many fields such as meteorology.
Description of drawings:
Accompanying drawing 1 is a mooring pier scheme drawing of the present invention;
Accompanying drawing 2 is high-altitude operation platform scheme drawings of the present invention;
Accompanying drawing 3 is working state of system scheme drawings of the present invention.
Embodiment:
The first step: on ground or submerged structure mooring pier 1, bearing universal 2 is set on mooring pier 1;
Second step: high-altitude operation platform 4 is set on ground, bearing universal 2 is set on high-altitude operation platform 4;
The 3rd step: connect mooring pier 1 with hawser 3 one ends, the other end connects high-altitude operation platform 4;
The 4th step: the helicopter traction high-altitude operation platform 4 with dirigible, fire balloon or turbojet are used as power makes its lift-off be positioned hawser 3 with high high-altitude advection layer.
The advection layer of the operating altitude of high-altitude operation platform 4 between the 11.000-30.000M of distance ground.Mooring pier 1 usefulness reinforced concrete structure or other whole weight.Do coupling link with high-intensity bearing universal 2, connect mooring pier 1 flexibly securely and make it can not come off fracture with high-altitude operation platform 4.Hawser 3 must have sufficient intensity to bear the stressed of the pulling force of high-altitude operation platform 4 and windage, length should adopt the high-strength abrasion-proof corrosion resistant to touch lamination coating greater than 11.000-30.000M, as: material such as carbon fiber, aramid fiber, must make it can not broken, and lightning protection electric work energy is arranged.High-altitude operation platform 4 must have aerodynamic performance; The automatic compensation horizontal tail changes lift, by the normal limb orientation, protects special balance automatically, steadily reaches counterweight load, and himself lift should keep equating with its gravity.High-altitude operation platform 4 is provided with parachute, falls in case high-altitude operation platform 4 is met under the faults, and when the speed of falling instantly surpassed 50 meters of per seconds, parachute was opened automatically, to ensure aerial and ground staff's device security.On the high-altitude operation platform 4 work stall can be set, lounge, meeting room, the happy chamber of mistake, facility or instrument and equipments such as boarding house, astronomy, meteorology, mapping, communication, navigation, solar electrical energy generation, wind-power electricity generation, power transformation, transmission of electricity, storage battery, lightning-arrest electricity.
Claims (8)
1, a kind of method of building job platform at the high-altitude advection layer, it is characterized in that: it comprises following content and step:
A, on ground or submerged structure mooring pier, it is universal on the mooring pier bearing to be set;
B, on ground high-altitude operation platform is set, it is universal that bearing is set on high-altitude operation platform;
C, usefulness hawser one end connect the mooring pier, and the other end connects high-altitude operation platform;
D, the helicopter that is used as power with dirigible, fire balloon or turbojet draw high-altitude operation platform, make its lift-off be positioned hawser with high high-altitude advection layer.
2, method of building job platform at the high-altitude advection layer as claimed in claim 1 is characterized in that: the advection layer of the operating altitude of high-altitude operation platform between the 11.000-30.000M of distance ground.
3, method of building job platform at the high-altitude advection layer as claimed in claim 1 is characterized in that: the mooring pier adopts reinforced concrete structure or other whole weight.
4, method of building job platform at the high-altitude advection layer as claimed in claim 1 is characterized in that: with the universal coupling link of doing of high-intensity bearing, connect mooring pier and high-altitude operation platform flexibly securely and make it can not come off fracture.
5, method of building job platform at the high-altitude advection layer as claimed in claim 1, it is characterized in that: hawser must have sufficient intensity to bear the stressed of the pulling force of high-altitude operation platform and windage, length should be at 11.000-30.000M, adopt the high-strength abrasion-proof corrosion resistant to touch lamination coating, as: material such as carbon fiber, aramid fiber, must make it can not broken, and lightning protection electric work energy is arranged.
6, method of building job platform as claimed in claim 1 at the high-altitude advection layer, it is characterized in that: high-altitude operation platform must have aerodynamic performance; The automatic compensation horizontal tail changes lift, by the normal limb orientation, protects special balance automatically, steadily reaches counterweight load, and himself lift should keep equating with its gravity.
7, method of building job platform at the high-altitude advection layer as claimed in claim 1, it is characterized in that: high-altitude operation platform is provided with parachute, in case meeting under the fault, high-altitude operation platform falls, when the speed of falling instantly surpasses 50 meters of per seconds, parachute is opened automatically, to ensure aerial and ground staff's device security.
8, method of building job platform at the high-altitude advection layer as claimed in claim 1, it is characterized in that: on the high-altitude operation platform work stall can be set, the lounge, meeting room, the happy chamber of mistake, facility or instrument and equipments such as boarding house, astronomy, meteorology, mapping, communication, navigation, solar electrical energy generation, wind-power electricity generation, power transformation, transmission of electricity, storage battery, lightning-arrest electricity.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CNA031269761A CN1470432A (en) | 2003-06-17 | 2003-06-17 | Method for building work platform at high-altitude stratosphere |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CNA031269761A CN1470432A (en) | 2003-06-17 | 2003-06-17 | Method for building work platform at high-altitude stratosphere |
Publications (1)
Publication Number | Publication Date |
---|---|
CN1470432A true CN1470432A (en) | 2004-01-28 |
Family
ID=34153159
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CNA031269761A Pending CN1470432A (en) | 2003-06-17 | 2003-06-17 | Method for building work platform at high-altitude stratosphere |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN1470432A (en) |
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN102310940A (en) * | 2010-07-08 | 2012-01-11 | 何仁城 | Space station |
CN102410144A (en) * | 2011-12-19 | 2012-04-11 | 杨礼诚 | Flying wind power generating system |
CN104808687A (en) * | 2015-04-28 | 2015-07-29 | 国家电网公司 | Control device and control method for unmanned airship control device for observing electrified detection bodies |
CN105075758A (en) * | 2015-09-22 | 2015-11-25 | 许琬晨 | Method and system for manually influencing weather |
CN107108031A (en) * | 2015-11-03 | 2017-08-29 | 以色列宇航工业有限公司 | Hovering flight device and its control method |
CN110645146A (en) * | 2019-10-31 | 2020-01-03 | 李良杰 | Kite type high-altitude wind driven generator |
-
2003
- 2003-06-17 CN CNA031269761A patent/CN1470432A/en active Pending
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN102310940A (en) * | 2010-07-08 | 2012-01-11 | 何仁城 | Space station |
CN102410144A (en) * | 2011-12-19 | 2012-04-11 | 杨礼诚 | Flying wind power generating system |
CN104808687A (en) * | 2015-04-28 | 2015-07-29 | 国家电网公司 | Control device and control method for unmanned airship control device for observing electrified detection bodies |
CN105075758A (en) * | 2015-09-22 | 2015-11-25 | 许琬晨 | Method and system for manually influencing weather |
CN107108031A (en) * | 2015-11-03 | 2017-08-29 | 以色列宇航工业有限公司 | Hovering flight device and its control method |
CN107108031B (en) * | 2015-11-03 | 2019-12-03 | 以色列宇航工业有限公司 | Hovering flight device and its control method |
US11148807B2 (en) | 2015-11-03 | 2021-10-19 | Israel Aerospace Industries Ltd. | Hovering aerial vehicle and method of flying same |
CN110645146A (en) * | 2019-10-31 | 2020-01-03 | 李良杰 | Kite type high-altitude wind driven generator |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US8006933B2 (en) | Airborne power station | |
US20110101692A1 (en) | Airborne wind powered generator | |
US20210197949A1 (en) | High altitude gravity energy storage | |
US9169014B2 (en) | Unmanned aerial vehicle and method of launching | |
US4350897A (en) | Lighter than air wind energy conversion system | |
PT103489A (en) | MODULAR SYSTEM OF ATMOSPHERIC RESOURCE DEVELOPMENT | |
CN101117941B (en) | Mooring line air balloon wind turbine generator | |
US8985499B2 (en) | Stratosphere tethered platform for multiple uses | |
US20140246862A1 (en) | Airborne wind energy system | |
WO2005067373A2 (en) | Hovering wind turbine | |
CN201781447U (en) | Inflation platform solar power station capable of floating in stratosphere | |
Aglietti et al. | Harnessing high-altitude solar power | |
CN1470432A (en) | Method for building work platform at high-altitude stratosphere | |
Aglietti et al. | Solar power generation using high altitude platforms feasibility and viability | |
US20190296685A1 (en) | Solar panel arrangement | |
US20150240785A1 (en) | Power generation device floating in the air | |
RU2642008C1 (en) | Anti-icing-balloon wind generator | |
Haslach | Wind energy- A resource for a human mission to Mars | |
US8985498B2 (en) | Stratosphere tethered photovoltaic power platform | |
CN102310940A (en) | Space station | |
EP2916000A1 (en) | Ligher-than-air device converting solar and wind energy | |
RU2506204C1 (en) | Method of locating high-altitude platform and high-altitude platform | |
KR101757275B1 (en) | Generation Plant on High Altitude Using Airship | |
RU162643U1 (en) | DEVICE FOR PLACING EQUIPMENT OF DIFFERENT FUNCTIONAL PURPOSE IN THE GROUND SPACE | |
O’Gairbhith | Assessing the viability of high altitude wind Resources in Ireland |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
C06 | Publication | ||
PB01 | Publication | ||
C10 | Entry into substantive examination | ||
SE01 | Entry into force of request for substantive examination | ||
C12 | Rejection of a patent application after its publication | ||
RJ01 | Rejection of invention patent application after publication |