CN102923295A - Method for mooring radar by kite high altitude - Google Patents
Method for mooring radar by kite high altitude Download PDFInfo
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- CN102923295A CN102923295A CN2011102248775A CN201110224877A CN102923295A CN 102923295 A CN102923295 A CN 102923295A CN 2011102248775 A CN2011102248775 A CN 2011102248775A CN 201110224877 A CN201110224877 A CN 201110224877A CN 102923295 A CN102923295 A CN 102923295A
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Abstract
The invention discloses a method for mooring a radar by a kite at high altitude. The kite flies to the upper-level jet stream at southern and northern latitudes 30 to 50 degrees and 8 to 12 kilometers away from the ground, the wind direction and the wind speed of the upper-level jet stream are stable all year around, and the mooring radar moored below the kite. By the method for mooring the radar by the kite at high altitude, all weather operation can be realized, the annual work days are more than and equal to 360 days, and the method is safe and suitable for mooring the high-altitude radar; and equipment is simple.
Description
[affiliated technical field]:
The invention belongs to the high altitude kite balloon field of radar.
[background technology]:
At present, known high altitude kite balloon radar is comprised of equipment on the ground and high-altitude (dirigible) balloon equipment etc.Because the relation of cable weight, present common high altitude kite balloon radar operating altitude is at 3000 meters, and limiting altitude is 6000 meters.50 meters length of balloon volume diameter are at 100 meters, owing to volume and cable reason in the strong wind sky, thundery sky will be reduced to ground with balloon mooring radar and quit work.
[summary of the invention]:
Quit work at strong wind and thundery sky in order to overcome existing aerostat mooring radar, the invention provides a kind of high-altitude kite mooring radar method.That kite flying is arrived south, north latitude 30-50 degree, height 8,000 to 12 km high-level jet streams (also claiming the high-altitude jet flow), the long-term wind direction of high-level jet stream, wind speed are stablized, and the mooring radar is tethered in the kite below.This high-altitude kite mooring radar method energy all weather operation, be no less than 360 days a year working day, and the radar maximum height can be operated in 8000 meters to 12000 meters height.And use safety, equipment simple, be applicable to mooring high-altitude radar.
The technical solution adopted for the present invention to solve the technical problems is: at the surface wind direction turntable radio receiving equipment, computer monitoring equipment are housed, it is characterized in that: ground kite operating control, kite angle of attack setting device, rope, kite, prevent that aircraft from knocking generating set, sensor, the communication apparatus on kite device, the kite.
Described wind direction turntable: be for kite and other mechanism above the rotating disk, forever down the wind set up on one side.The electricity consumption of radar wayside equipment is connected with electrical network by cable.
Described ground kite operating control is characterized in that: add that with 2-4 section winch pulling force sensor and rotary angle transmitter form.Be the usefulness of control kite Windward angle, maximum with the angled lift of air-flow when the kite surface, when the kite surface is parallel to air-flow, kite lift is minimum.
Described kite angle of attack setting device is characterized in that: winch cylinder and rotary angle transmitter are installed above weight, and rope twines at cylinder, is used for adjusting kite front and back Windward angle.
Described rope is characterized in that: adopt superhigh molecular weight polyethylene fibers (UHMWPE) manufacturing.It is the third generation high-performance special fiber after carbon fiber, aramid fiber, it be not only specific modulus in the present high-performance fiber, fiber that strength-to-density ratio is the highest (strength-to-density ratio be iron and steel 8-15 doubly, higher by 40% than aramid fiber), and have light weight, softness, low temperature resistant, UV resistant, shock-resistant, seawater corrosion resistance, wear-resisting a, chemical resistance, not absorbing water, is unique high-performance fiber that can float on the surface.
Described kite is characterized in that: shape is shown the flexible kite of gliding parachute; For the lead-in wire that makes the stressed even kite of kite adopts pulley structure; Adopt the traction control rope to separate with the lift heavy rope.
The described aircraft that prevents knocks the kite device, kite can fly to the top, convective zone, and the height of aircarrier aircraft is assurance aircarrier aircraft safety just, setting prevents that aircraft from knocking the kite device, is characterized in that: aluminium foil, the red light of flicker, the multitime flash lamp of placing radar signal reflected on the kite.
Generating set on the described kite is characterized in that: kite is equipped with light-duty wind power plant.That the contriver is in the patent of declaring before " wind energy collecting flabellum umbrella " 201120057145.7.
Described sensor is characterized in that: laying temperature sensor, air velocity transducer, altimeter, humidity sensor, GPS sensor, obliquity sensor on the kite.
Described communication apparatus is characterized in that: kite is installed radio digital communication equipment, and state and the radar signal of kite reached ground.
The invention has the beneficial effects as follows that with communication cable and electric power supply cable between cancellation ground and the radar, radar can be placed higher spatial domain, is not afraid of strong wind and thunderstorm weather, simple in structure, cost is low, and maintenance cost is low.
[description of drawings]:
The present invention is further described below in conjunction with drawings and Examples.
Fig. 1 is schematic diagram of the present invention.
Fig. 2 is kite figure of the present invention.
Fig. 3 is adjustment cylinder figure of the present invention.
[specific embodiment]:
Schematic diagram of the present invention shown in Figure 1, at wind direction turntable (1) kite operating control (2) being installed is that the control kite is used, the state of high-altitude kite is passed to ground by wireless digital signal, and ground kite operating control is adjusted the state of flight of high-altitude kite constantly by drag rope (3).Kite among the figure (4), lift heavy rope (5), radar system (6).
Kite figure of the present invention shown in Figure 2, the state of high-altitude kite is passed to ground by wireless digital signal, and ground kite operating control is adjusted the state of flight of high-altitude kite constantly by drag rope (3).Kite among the figure (4), lift heavy rope (5), radar system (6), assembly pulley (7), cylinder (8), make kite even at various inclination angles lower stress.
Fig. 3 is adjustment cylinder figure of the present invention.Lift heavy rope (5), radar system (6), cylinder (8), reductor and electrical motor (9) among the figure, by sensor and computer controlled cylinder, can adjust the angle that facings the wind of kite, kite can work as parachute usefulness in kite lands process.
Claims (9)
1. high-altitude kite mooring radar method is characterized in that: kite operating control, kite angle of attack setting device, rope, kite, prevent that aircraft from knocking generating set, sensor, the communication apparatus on kite device, the kite.
2. high-altitude kite mooring radar method according to claim 1, described kite operating control is characterized in that: add that with 2-4 section winch pulling force sensor and rotary angle transmitter form.
3. high-altitude kite mooring radar method according to claim 1, described kite angle of attack setting device is characterized in that: winch cylinder and rotary angle transmitter are installed above weight, and rope twines at cylinder, is used for adjusting Windward angle before and after the kite.
4. high-altitude kite mooring radar method according to claim 1, described rope is characterized in that: adopt superhigh molecular weight polyethylene fibers (UHMWPE) manufacturing.
5. high-altitude kite mooring radar method according to claim 1, described kite is characterized in that: shape is shown the flexible kite of gliding parachute; For the lead-in wire that makes the stressed even kite of kite adopts pulley structure; Adopt the traction control rope to separate with the lift heavy rope.
6. high-altitude kite mooring radar method according to claim 1, the described aircraft that prevents knocks the kite device, it is characterized in that: aluminium foil, the red light of flicker, the multitime flash lamp of placing radar signal reflected on the kite.
7. high-altitude kite mooring radar method according to claim 1, the generating set on the described kite is characterized in that: kite is equipped with light-duty wind power plant.
8. high-altitude kite mooring radar method according to claim 1, described sensor is characterized in that: laying temperature sensor, air velocity transducer, altimeter, humidity sensor, GPS sensor, obliquity sensor on the kite.
9. high-altitude kite mooring radar method according to claim 1, described communication apparatus is characterized in that: kite is installed radio digital communication equipment.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2011102248775A CN102923295A (en) | 2011-08-08 | 2011-08-08 | Method for mooring radar by kite high altitude |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2011102248775A CN102923295A (en) | 2011-08-08 | 2011-08-08 | Method for mooring radar by kite high altitude |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN102923295A true CN102923295A (en) | 2013-02-13 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2011102248775A Pending CN102923295A (en) | 2011-08-08 | 2011-08-08 | Method for mooring radar by kite high altitude |
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Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106516151A (en) * | 2016-12-07 | 2017-03-22 | 青海利高智能设备有限公司 | Unmanned aerial vehicle mooring base |
| CN107914893A (en) * | 2017-10-30 | 2018-04-17 | 航宇救生装备有限公司 | One kind is carrier-borne to be tethered at umbrella wing unmanned plane |
| CN109502004A (en) * | 2018-12-25 | 2019-03-22 | 哈尔滨工业大学 | It is a kind of that aerostatics is tethered at based on balloon-kite mixed structure |
| CN111559489A (en) * | 2020-04-02 | 2020-08-21 | 中国科学院空天信息创新研究院 | High-altitude balloon issuing method carrying large-span unmanned aerial vehicle |
| CN111591429A (en) * | 2020-04-28 | 2020-08-28 | 西安九天飞艇制造有限公司 | Large airship ground mooring system and mooring method thereof |
| CN111911349A (en) * | 2020-08-20 | 2020-11-10 | 武汉大学 | High-altitude wind power generation system based on dynamic balance flapping wings |
| CN117963152A (en) * | 2024-03-29 | 2024-05-03 | 湖北华中电力科技开发有限责任公司 | Mooring method for mooring unmanned aerial vehicle |
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| US4768739A (en) * | 1986-12-15 | 1988-09-06 | Schnee Robert A | Emergency warning and signaling system |
| CA2172852A1 (en) * | 1996-03-28 | 1997-09-29 | Unknown | Kite balloon |
| CN101240778A (en) * | 2007-02-06 | 2008-08-13 | 李庆星 | Kite power generation method |
| US20100327104A1 (en) * | 2007-12-18 | 2010-12-30 | Thales | Device for maintaining the altitude of a payload having an altitude-maintenance energy source that is permanent and extracted from the surrounding medium |
| CN201730737U (en) * | 2010-08-11 | 2011-02-02 | 戴宁 | Two-string kite generator twisting preventive device |
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2011
- 2011-08-08 CN CN2011102248775A patent/CN102923295A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4768739A (en) * | 1986-12-15 | 1988-09-06 | Schnee Robert A | Emergency warning and signaling system |
| CA2172852A1 (en) * | 1996-03-28 | 1997-09-29 | Unknown | Kite balloon |
| CN101240778A (en) * | 2007-02-06 | 2008-08-13 | 李庆星 | Kite power generation method |
| US20100327104A1 (en) * | 2007-12-18 | 2010-12-30 | Thales | Device for maintaining the altitude of a payload having an altitude-maintenance energy source that is permanent and extracted from the surrounding medium |
| CN201730737U (en) * | 2010-08-11 | 2011-02-02 | 戴宁 | Two-string kite generator twisting preventive device |
Cited By (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106516151A (en) * | 2016-12-07 | 2017-03-22 | 青海利高智能设备有限公司 | Unmanned aerial vehicle mooring base |
| CN107914893A (en) * | 2017-10-30 | 2018-04-17 | 航宇救生装备有限公司 | One kind is carrier-borne to be tethered at umbrella wing unmanned plane |
| CN109502004A (en) * | 2018-12-25 | 2019-03-22 | 哈尔滨工业大学 | It is a kind of that aerostatics is tethered at based on balloon-kite mixed structure |
| CN111559489A (en) * | 2020-04-02 | 2020-08-21 | 中国科学院空天信息创新研究院 | High-altitude balloon issuing method carrying large-span unmanned aerial vehicle |
| CN111559489B (en) * | 2020-04-02 | 2021-06-25 | 中国科学院空天信息创新研究院 | High-altitude balloon issuing method carrying large-span unmanned aerial vehicle |
| CN111591429A (en) * | 2020-04-28 | 2020-08-28 | 西安九天飞艇制造有限公司 | Large airship ground mooring system and mooring method thereof |
| CN111591429B (en) * | 2020-04-28 | 2024-03-01 | 西安九天飞艇制造有限公司 | Ground mooring system and mooring method for large airship |
| CN111911349A (en) * | 2020-08-20 | 2020-11-10 | 武汉大学 | High-altitude wind power generation system based on dynamic balance flapping wings |
| CN117963152A (en) * | 2024-03-29 | 2024-05-03 | 湖北华中电力科技开发有限责任公司 | Mooring method for mooring unmanned aerial vehicle |
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Application publication date: 20130213 |