CN103863546A - Novel large-sized aerostat releasing mode - Google Patents
Novel large-sized aerostat releasing mode Download PDFInfo
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- CN103863546A CN103863546A CN201410080887.XA CN201410080887A CN103863546A CN 103863546 A CN103863546 A CN 103863546A CN 201410080887 A CN201410080887 A CN 201410080887A CN 103863546 A CN103863546 A CN 103863546A
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- 239000002360 explosive Substances 0.000 claims description 7
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- 238000000034 method Methods 0.000 description 14
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- 230000009286 beneficial effect Effects 0.000 description 1
- 239000012141 concentrate Substances 0.000 description 1
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- 238000007599 discharging Methods 0.000 description 1
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Abstract
The invention discloses a novel large-sized aerostat releasing mode, mainly comprising the following steps of inflating an aerostat, connecting with multiple windproof ropes with releasable lengths, and connecting the tail end of the aerostat with releasing ropes connected with a hoisting bin and a transition winch respectively, wherein the hoisting bin and the transition winch are horizontally spaced by a distance; connecting the hoisting bin with the tail end of the aerostat by a parachute, and connecting a connection rope of the hoisting bin with multiple hoisting bin releasing ropes; releasing the windproof ropes till the transition winch releasing ropes are about to bear force, adjusting the winch to position the windproof ropes at the loosening state, and transferring the aerostat buoyancy to the transition winch releasing ropes from the windproof ropes; disconnecting all windproof ropes, releasing the transition winch ropes, and lifting the aerostat to lift the hoisting bin, wherein the aerostat buoyancy is fully transferred to the hoisting bin releasing ropes from the transition winch ropes; cutting off the transition winch ropes, releasing the hoisting bin releasing ropes and lifting the hoisting bin; synchronously cutting off the hoisting bin releasing ropes to finish the whole releasing. According to the novel large-size aerostat releasing mode, the releasing flexibility, safety and reliability of the large-sized aerostat are greatly improved, and the lifting stability of the hoisting bin is improved.
Description
Technical field
The present invention relates to a kind of novel large scale aerostat delivery mode, belong to aerospace dirigible application.
Background technology
Aerostat, as a kind of cheap high-altitude means of delivery, plays very important effect in multi-disciplinary space science research.Because balloon volume is generally tens thousand of to hundreds thousand of and even up to a million cubic meters, flying height can reach 30-50 kilometer, load capacity is hundreds of kilograms to several tons, and therefore, the success or failure of the flight test of the delivery mode of this large-sized aerostat to whole aerostat play a part very important.
1783, first fire balloon went up to the air in France in the world, and the mankind have just started to utilize aerostat to explore the practical activity of space secret since then.Through the development of decades, various countries have developed the method for releasing of several different balloons.More external countries, such as France, once used easy air bag to do static release, aerostat connects gondola by parachute, cuts off after windproof rope, aerostat relies on buoyancy to rise rapidly, although this granting is simple and convenient, comes with some shortcomings: Once you begin test windproof rope and cut off, balloon is just no longer controlled, and gondola taken up time vibrations by balloon larger, be unfavorable for the instrument and equipment safety in gondola.
The method for releasing of the aerostat of development afterwards, mainly all concentrates on and improves the anchor fitting discharging for controlling starting stage balloon.Frenchman adopts a kind of soft method for releasing: be exactly by a roller device control balloon spheroid, and between parachute and gondola, increase a saloon, this method for releasing is with respect to static release, although it is not high to site requirements, can provide more than two load simultaneously, rise with saloon but gondola can experience elder generation, after departing from saloon, freely decline a bit of, driven by parachute the process rising again, the instrument and equipment in gondola is still subject to the instable impact of gondola.
The release gear often adopting is now except with roller device control balloon spheroid, gondola is arranged on dynamic mobility car by specific device, and this method has improved the stability of gondola lift-off, but all more single to the control of balloon and gondola, underaction is tighter to the requirement in place.The method for releasing of Chinese Academy of Sciences's aerostat that study of high energy physics adopts is: by control the release of starting stage balloon with the self-propelled vehicle of winch, and on balloon, be provided with releaser, on releaser, be connected with a drogue-parachute, releaser is connected with winch by rope.The advantage of this method maximum is the stability having improved in gondola uphill process, device therefor is few, and releaser is reclaimed, but also more single to the control of balloon, and releaser is in the effect time receiving next time of drogue-parachute, has the danger of interfering with whole device.
Therefore need the one more can actv. control balloon, to reach the release of safety and reliability, and at utmost guarantee that the large scale aerostat of gondola stability discharges solution.
Summary of the invention
In order to address the above problem, the present invention proposes a kind of large scale aerostat delivery mode.The object of the invention is to improve alerting ability in large scale aerostat dispose procedure with, gondola the stability in lift-off process and balloon is discharged to the controllability of starting stage.
The novel large scale aerostat of one provided by the invention delivery mode, mainly comprises the steps:
(1) aerostat inflation, is connected with the many windproof ropes that can discharge length, and the end of aerostat connects respectively and has the gondola of horizontal interval (HI) distance and the release rope of transition winch, and the connection cord of gondola is restricted and is connected with many gondolas releases;
(2) discharge windproof rope, discharge rope will load time to transition winch, adjust winch and make windproof rope in relaxed state, make balloon buoyancy transfer to transition winch rope by windproof rope;
(3) disconnect all windproof ropes, discharge transition winch rope, promote balloon, nacelle lifting is got up, balloon buoyancy is transferred to gondola completely by transition winch rope and discharges rope;
(4) excision transition winch rope, discharges gondola and discharges rope, promotes gondola;
(5) turned off in synchronization gondola discharges rope, completes entirety and discharges.
Described windproof rope is preferably the windproof rope of four-way.
Described gondola discharges rope and is preferably three-dimensional release rope.
Be preferably in gondola release rope end and be provided with the transition rope with explosive bolt.
Described windproof rope and transition winch be all placed in one movably on bogey for good.
Between the connection cord of balloon end and the connection cord of gondola, can be connected with parachute.
Preferably, described windproof rope is the windproof rope of four-way, described gondola discharges rope and restricts for three-dimensional discharges, between the connection cord of balloon end and the connection cord of gondola, be connected with parachute, wherein, the concrete operations of step (3) are: the windproof rope of excision four-way, discharge fast transition winch rope, promote balloon and parachute, after parachute entirety is liftoff, suitably pretension far-end point of release rope, continue to discharge transition winch, parachute is stretching gradually, by nacelle lifting to certain altitude, balloon buoyancy is transferred to three-dimensional completely by transition winch rope and discharges rope.
More preferably, the concrete operations of step (4) are: adjust three-dimensional release rope, parachute hanging point is adjusted to directly over gondola, excision transition winch rope, adjusts three-dimensional and discharge the long and synchronous slowly release of restricting, and promotes gondola.
Compared with prior art, the invention has the beneficial effects as follows:
(1) what balloon was purposeful completed, and twice buoyancy shifts, and twice buoyancy while shifting all in controllable reversible state, in the time of the weather conditions that run into sudden change, can retract in time, effectively improved the safety and reliability of dispose procedure;
(2) first by the stretching parachute of transition winch rope, rising certain altitude discharges rope rising certain altitude by three-dimensional to gondola afterwards again, is finally going up to the air along with the beginning of whole experiment.The slow release of multistage rope has greatly improved the stability of gondola in the time of lift-off;
(3) in buoyancy transfer process, need constantly to adjust three-dimensional and discharge rope position, so discharge rope and parachute junction in three-dimensional, design one section of transition rope with explosive bolt, three-dimensional discharges rope end and is provided with spring, after explosive bolt cuts off, three-dimensional discharges rope can be regained fast, so just avoids the interference of rope and gondola, has guaranteed the safety of gondola.
Accompanying drawing explanation
Fig. 1 is the integrality before the large scale aerostat of a kind of novel large scale aerostat delivery mode of the present invention discharges;
Fig. 2 is that the buoyancy for the first time of a kind of novel large scale aerostat delivery mode of the present invention shifts schematic diagram;
Fig. 3 is that the buoyancy for the second time of a kind of novel large scale aerostat delivery mode of the present invention shifts schematic diagram;
Fig. 4 is schematic diagram after the buoyancy for the second time of a kind of novel large scale aerostat delivery mode of the present invention shifts;
Fig. 5 is secondary lifting schematic diagrams of gondola of a kind of novel large scale aerostat delivery mode of the present invention;
Fig. 6 is that the entirety of a kind of novel large scale aerostat delivery mode of the present invention discharges schematic diagram;
Fig. 7 is the parachute end and the connection mode schematic diagram that discharges rope of a kind of novel large scale aerostat delivery mode of the present invention.
The specific embodiment
Below in conjunction with drawings and Examples, the present invention is described in further detail.First according to the example of Fig. 1, complete the inflation inspection of aerostat 1, with the windproof rope 2(4 of four-way root, as follows) connect, carry out gondola 7 simultaneously and discharge rope 9(3 root with three-dimensional, as follows), the connection of parachute 6, rope 4 and the parachute 6 of balloon 1 end are connected with the release rope 8 on transition winch 5.Transition winch 5 is placed on self-propelled vehicle 3.
As shown in Figure 2, discharge the windproof rope 4 of four-way, discharge rope 8 will load time to transition winch, the whole winch 5 of slow-action confirms that four windproof ropes 4 are in relaxed state, suitably adjust transition winch 5, aerostat 1 is fixed on to proper height, and balloon buoyancy is transferred to transition winch rope 8 by the windproof rope 2 of four-way.
As shown in Figures 3 and 4, the windproof rope 2 of excision four-way, discharge fast transition winch rope 8, promote balloon 1 and parachute 6, after parachute entirety is liftoff, suitably pretension far-end point of release rope, continue to discharge transition winch 5, parachute 6 is stretching gradually, gondola 7 is promoted to certain altitude, balloon buoyancy is transferred to three-dimensional completely by transition winch rope 8 and discharges rope 9.
As shown in Figure 5, adjust three-dimensional and discharge winch 10, parachute 6 hanging points are adjusted to directly over gondola 7, excision transition winch rope 8, adjusts three-dimensional release winch rope long 9 synchronous slowly release, promotes gondola 7 to design height.
As shown in Figure 6, confirm that avionics signal is normal, turned off in synchronization three-dimensional discharges rope 9, completes entirety and discharges.
In buoyancy transfer process, need constantly to adjust three-dimensional and discharge rope position, so discharge rope and parachute junction in three-dimensional, designed one section of transition rope with explosive bolt, three-dimensional discharges rope end and is provided with spring.Fig. 7 has indicated the annexation of the three-dimensional release rope c of parachute a, explosive bolt b and end band spring.After explosive bolt cuts off, three-dimensional discharges rope can be regained fast, so just avoids the interference of rope and gondola, has guaranteed the safety of gondola.
Claims (8)
1. a novel large scale aerostat delivery mode, is characterized in that: mainly comprise the steps:
(1) aerostat inflation, is connected with the many windproof ropes that can discharge length, and the end of aerostat connects respectively and has the gondola of horizontal interval (HI) distance and the release rope of transition winch, and the connection cord of gondola is restricted and is connected with many gondolas releases;
(2) discharge windproof rope, discharge rope will load time to transition winch, adjust winch and make windproof rope in relaxed state, make balloon buoyancy transfer to transition winch rope by windproof rope;
(3) disconnect all windproof ropes, discharge transition winch rope, promote balloon, nacelle lifting is got up, balloon buoyancy is transferred to gondola completely by transition winch rope and discharges rope;
(4) excision transition winch rope, discharges gondola and discharges rope, promotes gondola;
(5) turned off in synchronization gondola discharges rope, completes entirety and discharges.
2. novel large scale aerostat delivery mode according to claim 1, is characterized in that: described windproof rope is the windproof rope of four-way.
3. novel large scale aerostat delivery mode according to claim 1, is characterized in that: described gondola discharges rope and restricts for three-dimensional discharges.
4. novel large scale aerostat delivery mode according to claim 1, is characterized in that: discharge rope end at gondola and be provided with the transition rope with explosive bolt.
5. novel large scale aerostat delivery mode according to claim 1, is characterized in that: described windproof rope and transition winch are all placed in one movably on bogey.
6. novel large scale aerostat delivery mode according to claim 1, is characterized in that: between the connection cord of balloon end and the connection cord of gondola, be connected with parachute.
7. novel large scale aerostat delivery mode according to claim 1, it is characterized in that: described windproof rope is the windproof rope of four-way, described gondola discharges rope and restricts for three-dimensional discharges, between the connection cord of balloon end and the connection cord of gondola, be connected with parachute, wherein, the concrete operations of step (3) are: the windproof rope of excision four-way, discharge fast transition winch rope, promote balloon and parachute, after parachute entirety is liftoff, suitably pretension far-end point of release rope, continue to discharge transition winch, parachute is stretching gradually, by nacelle lifting to certain altitude, balloon buoyancy is transferred to three-dimensional completely by transition winch rope and discharges rope.
8. novel large scale aerostat delivery mode according to claim 7, it is characterized in that: the concrete operations of step (4) are: adjust three-dimensional and discharge rope, parachute hanging point is adjusted to directly over gondola, excision transition winch rope, adjust three-dimensional and discharge the long and synchronous slowly release of restricting, promote gondola.
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| CN201410080887.XA CN103863546B (en) | 2014-03-06 | 2014-03-06 | A kind of large scale aerostat delivery mode |
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| CN201410080887.XA CN103863546B (en) | 2014-03-06 | 2014-03-06 | A kind of large scale aerostat delivery mode |
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| CN103863546B CN103863546B (en) | 2016-08-24 |
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Cited By (14)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104890851A (en) * | 2015-05-25 | 2015-09-09 | 湖南航天机电设备与特种材料研究所 | Near space balloon system safety release method |
| CN105109660A (en) * | 2015-08-14 | 2015-12-02 | 东莞前沿技术研究院 | Cutting releasing system |
| CN105438432A (en) * | 2015-08-26 | 2016-03-30 | 梁子康 | Controllable manned balloon |
| CN106005350A (en) * | 2016-05-19 | 2016-10-12 | 东莞前沿技术研究院 | Flying method for large balloon |
| CN106335621A (en) * | 2015-12-11 | 2017-01-18 | 中国特种飞行器研究所 | Air-drop type balloon air retention system |
| CN106553747A (en) * | 2015-09-28 | 2017-04-05 | 东莞前沿技术研究院 | The piece-rate system of ballast |
| WO2017185958A1 (en) * | 2016-04-28 | 2017-11-02 | 东莞前沿技术研究院 | Aerostat launching system |
| CN108128437A (en) * | 2017-11-22 | 2018-06-08 | 北京天恒长鹰科技股份有限公司 | Dirigible lets system fly away and dirigible lets method fly away |
| CN108163219A (en) * | 2017-11-22 | 2018-06-15 | 北京天恒长鹰科技股份有限公司 | Dirigible lets system fly away without boathouse and lets method fly away |
| CN108263589A (en) * | 2016-12-30 | 2018-07-10 | 海口未来技术研究院 | Discharge the method for aerostatics |
| CN108725742A (en) * | 2017-04-17 | 2018-11-02 | 深圳光启空间技术有限公司 | Aerostatics lets constraint release device fly away and aerostatics lets method fly away |
| CN109398674A (en) * | 2018-09-11 | 2019-03-01 | 中国科学院光电研究院 | Tandem is tethered at aerostatics and its distribution method |
| CN111746774A (en) * | 2020-06-01 | 2020-10-09 | 中国科学院空天信息创新研究院 | High-altitude balloon issuing system and method |
| CN113212727A (en) * | 2020-06-01 | 2021-08-06 | 中国科学院空天信息创新研究院 | High-altitude balloon flight rotation damping system based on rope cage structure |
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| CN111547227B (en) * | 2020-04-02 | 2021-06-22 | 中国科学院空天信息创新研究院 | Method for issuing ultra-high altitude mooring aerostat |
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| US3195839A (en) * | 1962-09-27 | 1965-07-20 | Litton Systems Inc | Balloon payload launching technique |
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Cited By (19)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104890851A (en) * | 2015-05-25 | 2015-09-09 | 湖南航天机电设备与特种材料研究所 | Near space balloon system safety release method |
| CN105109660A (en) * | 2015-08-14 | 2015-12-02 | 东莞前沿技术研究院 | Cutting releasing system |
| CN105438432A (en) * | 2015-08-26 | 2016-03-30 | 梁子康 | Controllable manned balloon |
| CN106553747A (en) * | 2015-09-28 | 2017-04-05 | 东莞前沿技术研究院 | The piece-rate system of ballast |
| CN106335621A (en) * | 2015-12-11 | 2017-01-18 | 中国特种飞行器研究所 | Air-drop type balloon air retention system |
| WO2017185958A1 (en) * | 2016-04-28 | 2017-11-02 | 东莞前沿技术研究院 | Aerostat launching system |
| CN106005350A (en) * | 2016-05-19 | 2016-10-12 | 东莞前沿技术研究院 | Flying method for large balloon |
| WO2017198001A1 (en) * | 2016-05-19 | 2017-11-23 | 东莞前沿技术研究院 | Method for flying large balloon |
| US11052985B2 (en) | 2016-05-19 | 2021-07-06 | Dongguan Frontier Technology Institute | Method for flying large balloon |
| CN106005350B (en) * | 2016-05-19 | 2021-11-12 | 东莞前沿技术研究院 | Flying method of large balloon |
| CN108263589A (en) * | 2016-12-30 | 2018-07-10 | 海口未来技术研究院 | Discharge the method for aerostatics |
| CN108725742B (en) * | 2017-04-17 | 2024-06-11 | 佛山顺德光启尖端装备有限公司 | Aerostat flying constraint releasing device and aerostat flying method |
| CN108725742A (en) * | 2017-04-17 | 2018-11-02 | 深圳光启空间技术有限公司 | Aerostatics lets constraint release device fly away and aerostatics lets method fly away |
| CN108128437A (en) * | 2017-11-22 | 2018-06-08 | 北京天恒长鹰科技股份有限公司 | Dirigible lets system fly away and dirigible lets method fly away |
| CN108163219A (en) * | 2017-11-22 | 2018-06-15 | 北京天恒长鹰科技股份有限公司 | Dirigible lets system fly away without boathouse and lets method fly away |
| CN109398674A (en) * | 2018-09-11 | 2019-03-01 | 中国科学院光电研究院 | Tandem is tethered at aerostatics and its distribution method |
| CN111746774A (en) * | 2020-06-01 | 2020-10-09 | 中国科学院空天信息创新研究院 | High-altitude balloon issuing system and method |
| CN113212727A (en) * | 2020-06-01 | 2021-08-06 | 中国科学院空天信息创新研究院 | High-altitude balloon flight rotation damping system based on rope cage structure |
| CN111746774B (en) * | 2020-06-01 | 2021-09-28 | 中国科学院空天信息创新研究院 | High-altitude balloon issuing system and method |
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