CN108128437A - Dirigible lets system fly away and dirigible lets method fly away - Google Patents
Dirigible lets system fly away and dirigible lets method fly away Download PDFInfo
- Publication number
- CN108128437A CN108128437A CN201711172743.7A CN201711172743A CN108128437A CN 108128437 A CN108128437 A CN 108128437A CN 201711172743 A CN201711172743 A CN 201711172743A CN 108128437 A CN108128437 A CN 108128437A
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- CN
- China
- Prior art keywords
- dirigible
- drawstring
- fly away
- constraint
- hoist engine
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- 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.)
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Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64B—LIGHTER-THAN AIR AIRCRAFT
- B64B1/00—Lighter-than-air aircraft
- B64B1/66—Mooring attachments
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F1/00—Ground or aircraft-carrier-deck installations
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Abstract
The present invention relates to a kind of dirigibles to let system fly away, and the dirigible system of letting fly away includes：Flexibility platform, the flexibility platform can be laid on the ground to support dirigible to be let fly away；Moveable platform；Hoist engine, the hoist engine are arranged on the moveable platform；Power supply unit, the power supply unit are arranged on the moveable platform；Drawstring is assisted, one end of the auxiliary drawstring is connected to dirigible head, and the other end can be operated by staff；Constrain drawstring；One end of the constraint drawstring is connected to dirigible tail portion, and the other end is connected to the hoist engine；Cutter device；The cutter device can cut off the constraint drawstring to release the constraint to dirigible.The invention further relates to a kind of dirigibles to let method fly away.
Description
Technical field
The present invention relates to airship technology fields, let system fly away more particularly to a kind of dirigible and dirigible lets method fly away.
Background technology
Dirigible as it is a kind of by natural buoyancy realize flight aircraft, during letting fly away, due to volume excessively
It is huge, and dirigible surface utricule is ultralight easy damaged material, equipment and hull easily contact to earth it is impaired, therefore, for dirigible energy
Smoothly lift-off, needs a kind of safe and reliable dirigible and lets method fly away.
Invention content
The purpose of the present invention is one of at least solving the above problems, which is achieved through the following technical solutions：
The present invention relates to a kind of dirigibles to let system fly away, and the dirigible system of letting fly away includes：
Flexibility platform, the flexibility platform can be laid on the ground to support dirigible to be let fly away；
Moveable platform；
Hoist engine, the hoist engine are arranged on the moveable platform；
Power supply unit, the power supply unit are arranged on the moveable platform, can provide electric power for the hoist engine；
Drawstring is assisted, one end of the auxiliary drawstring is connected to dirigible head, and the other end of the auxiliary drawstring can be by
Staff operates；
Drawstring is constrained, one end of the constraint drawstring is connected to dirigible tail portion, and the other end of the constraint drawstring is connected to
The hoist engine；And
Cutter device, the cutter device can cut off the constraint drawstring to release the constraint to dirigible.
Preferably, the dirigible system of letting fly away is provided with two constraint drawstrings and two hoist engines, described to fly
Ship tail portion is symmetrically arranged two connectors for being useful for connecting two constraint drawstrings respectively, the every constraint drawstring point
It is not connected to a hoist engine.
It is further preferred that the flexibility platform includes arrangement shield on the ground, the bubble being arranged on the shield
Foam pad and the antistatic film being arranged on the foam pad.
It is further preferred that the connector that the constraint drawstring is disposed through at the dirigible tail portion is formed and is drawn wearing
Rope so that two fag ends of the constraint drawstring are connected to the hoist engine；The auxiliary drawstring is disposed through dirigible head
The connector at place is formed to wearing drawstring so that the free end that two fag ends of the auxiliary drawstring are formed can be grasped by staff
Make.
It is further preferred that the connector is U-shaped hook.
It is further preferred that the cutter device includes Synchronization Control cabinet and two cutters, described two cutter energy
It is enough separately mounted on two constraint drawstrings, described two cutters are electrically connected with the Synchronization Control cabinet so that institute
Described two constraint drawstrings of cutter turned off in synchronization two can be controlled by stating Synchronization Control cabinet.
It is further preferred that it is provided with pulling force sensor on the constraint drawstring.
In addition, the invention further relates to the dirigibles for letting system implementation fly away by above-mentioned dirigible to let method fly away, the dirigible is let fly away
Method includes：
Flexibility platform is laid on the ground by the appropriate location in boathouse, and dirigible to be let fly away is arranged in the flexibility
On platform so that dirigible head is towards boathouse gate；
Moveable platform is arranged near one end for placing dirigible tail portion of the flexibility platform, described removable
Hoist engine and power supply unit are arranged on platform；
The one end for assisting drawstring is connected to dirigible head, the one end for constraining drawstring is connected to dirigible tail portion, and will about
The other end of beam drawstring is connected to the hoist engine；
To being inflated after dirigible integrated debugging by being arranged on the inflating port on dirigible head, by the people that works in gas replenishment process
The dirigible head that member is gradually lifted by operating the free end control of the auxiliary drawstring, when dirigible head in vertical state and reaches
During to predetermined altitude, stop to dirigible head inflating；
Dirigible is continued to inflate by the inflating port for being arranged on dirigible tail portion, dirigible is made to continue lifting until all liftoff be in
Vertical state；
Dirigible is made to be moved to the surface of the moveable platform by the auxiliary drawstring, continue to dirigible inflation until
The buoyancy of dirigible meets pre-provisioning request；
Dirigible is reduced on the moveable platform by the hoist engine, dirigible is carried by the moveable platform
Remove boathouse, release auxiliary drawstring, discharged dirigible to safe altitude by the hoist engine, cut off by cutter device described in
Drawstring is constrained, completes to let dirigible fly away.
Preferably, two constraint drawstrings are symmetrically connected to dirigible tail portion, two is arranged on the moveable platform
Hoist engine, two constraints drawstring are respectively connected to a hoist engine.
It is further preferred that the cutter device includes Synchronization Control cabinet and two electrically connected with the Synchronization Control cabinet
The Synchronization Control cabinet is arranged on the moveable platform by cutter, is moved carrying dirigible by the moveable platform
Go out boathouse and discharged dirigible to safe altitude by the hoist engine, constrained at every and a cutter is installed on drawstring,
Two constraint drawstrings described in described two cutter turned off in synchronization are controlled by the Synchronization Control cabinet.
The advantage of the invention is that：In gas replenishment process, hull is always in buoyant weight equilibrium state, utricule uniform force,
Only by auxiliary drawstring control hull posture, smaller to utricule damage, equipment is without danger of colliding with；Hull is raised to perpendicular by horizontality
During straight state, process is slow, has time enough to carry out security protection, monitoring, inspection to hull equipment；After dirigible outbound, lead to
It crosses hoist engine release drawstring and improves dirigible tail height, prevent from tilting because of the excessive dirigible of wind speed, ground is rubbed in tail portion, can adapt to arbitrary
The outbound of height dirigible is let fly away；The simultaneously operating of two hoist engines avoids the excessive situation of single-point stress, and arrangement and stress are closed
Reason, easy to operate, the connection and releasing of rope and hull are easily operated；Entirely inflate, to let process fly away fully controllable, reversible,
Dirigible when something goes wrong, multi channel airship's posture to inflate when original state.
Description of the drawings
By reading the detailed description of hereafter preferred embodiment, it is various other the advantages of and benefit it is common for this field
Technical staff will become clear.Attached drawing is only used for showing the purpose of preferred embodiment, and is not considered as to the present invention
Limitation.And throughout the drawings, the same reference numbers will be used to refer to the same parts.In the accompanying drawings：
Fig. 1 is shown lets signal of the system in the case where dirigible is in inflated condition fly away according to the dirigible of embodiment of the present invention
Figure；
Fig. 2 shows let system fly away according to the dirigible of embodiment of the present invention to inflate completion and in shape to be let fly away in dirigible
The schematic diagram of state.
Specific embodiment
The illustrative embodiments of the disclosure are more fully described below with reference to accompanying drawings.Although this public affairs is shown in attached drawing
The illustrative embodiments opened, it being understood, however, that may be realized in various forms the disclosure without the reality that should be illustrated here
The mode of applying is limited.It is to be able to be best understood from the disclosure, and can be by this public affairs on the contrary, providing these embodiments
The range opened completely is communicated to those skilled in the art.
According to the embodiment of the present invention, propose that a kind of dirigible lets system fly away, which is preferably used for putting down
Fluid layer dirigible.As shown in Figure 1, the dirigible system of letting fly away includes：Flexibility platform 1, moveable platform 4, hoist engine 6, power supply unit,
Assist drawstring 2, constraint drawstring 3 and cutter device.Wherein, flexibility platform 1 can be laid on ground in the appropriate location in boathouse
To support dirigible to be let fly away on face.Hoist engine 6 and power supply unit are arranged on moveable platform 4, and power supply unit can be
Hoist engine 6 provides electric power.One end of auxiliary drawstring 2 is connected to dirigible head, and the other end can be operated by staff.Constraint is drawn
One end of rope 3 is connected to dirigible tail portion, and the other end is connected to hoist engine 6.
As depicted in figs. 1 and 2, the dirigible system of letting fly away of the invention is preferably provided with two constraint drawstrings 3 and two volumes
Raise machine 6.Correspondingly, dirigible tail portion is symmetrically arranged two connectors for connecting two constraint drawstrings respectively, every constraint
One end of drawstring is connected to dirigible tail portion by a connector, and the other end is connected to a hoist engine.Two hoist engines 6 can
Synchronous working with identical speed so that discharge or withdraw two constraint drawstrings 3.In addition, as shown in Figure 1, preferably in dirigible head
Portion sets four auxiliary drawstrings, to control dirigible during dirigible inflation and movement, if equipment occurs before letting fly away
Failure can pass through above-mentioned four auxiliary drawstring reverse reclamation hulls.
According to a preferred embodiment of the invention, constraint drawstring 3 is disposed through the connector of dirigible tail portion and is formed pair
Wear drawstring so that two fag ends of constraint drawstring 3 are connected to hoist engine 6.Similarly, auxiliary drawstring 2 is disposed through dirigible head
The connector in portion is formed to wearing drawstring so that the free end that two fag ends of auxiliary drawstring 2 are formed can be operated by staff.
Correspondingly, it is set to the connector for connection constraints drawstring 3 of dirigible tail portion and is set to the auxiliary for connecting of dirigible head
The connector for helping drawstring 2 is preferably U-shaped hook or is provided with the connector of the other structures of connecting hole, in order to let fly away
When drawstring is released from dirigible.Preferably, constraint drawstring 3 and auxiliary drawstring 2 are made of polythene material.
According to the present invention to be preferably carried out mode, flexibility platform 1 includes the placement ground object of arrangement on the ground and punctures
Damage shield, the placement dirigible equipment foam pad to collide with being arranged on shield and the table being arranged on foam pad of dirigible utricule
The smooth antistatic film in face.
According to the present invention to be preferably carried out mode, cutter device includes Synchronization Control cabinet 5 and two cutters (do not show
Go out).Two cutters can be separately mounted on two constraint drawstrings 3, and cutter and Synchronization Control cabinet can pass through cable
Couple with power supply unit, and two cutters are electrically connected with Synchronization Control cabinet 5 so that Synchronization Control cabinet 5 can monitor cutting
The state of device.When needing to let fly away in dirigible, Synchronization Control cabinet 5 controls two cutter turned off in synchronization, two constraint drawstrings.
Preferably, it constrains on drawstring 3 and is provided with pulling force sensor, the process that can be inflated by pulling force sensor in dirigible
The surplus buoyancy of middle monitoring dirigible, so that it is determined that dirigible lets opportunity fly away.When that will let dirigible fly away, pulling force sensor can be from
It is released on constraint drawstring 3.
It is further preferred that lighting device, photographic device and act of rescue area can also be set on moveable platform 4
Domain.Hoist engine 6 have the function of a key delay liter, slow drop, and can be set as needed and adjust the speed of folding and unfolding drawstring, and have
Standby power-off automatic brake functions.
The dirigible method of letting fly away for letting system implementation fly away by above-mentioned dirigible includes the following steps：
Flexibility platform 1 is laid on the ground by the appropriate location in boathouse, dirigible to be let fly away is arranged in flexible flat
On platform 1 so that dirigible head is towards boathouse gate；
Moveable platform 4 is arranged near one end for placing dirigible tail portion of flexibility platform 1, in moveable platform 1
Upper arrangement hoist engine 6 and power supply unit；
The one end for assisting drawstring 2 is connected to dirigible head, the one end for constraining drawstring 3 is connected to dirigible tail portion, and will
The other end of constraint drawstring 3 is connected to hoist engine 6；
After being completed to dirigible integrated debugging and determining that weather, equipment state are normal, by the inflation for being arranged on dirigible head
Mouth is inflated, and the free end of drawstring 2 is assisted to control the dirigible head being gradually lifted by operation by staff in gas replenishment process
Portion, and constrain dirigible tail portion by hoist engine when dirigible head is in vertical state and when reaching predetermined altitude, stops to dirigible head
Portion is inflated, and is contacted gas tube by high-altitude operation vehicle, is closed charge valve；
Dirigible is continued to inflate by the inflating port for being arranged on dirigible tail portion, dirigible is made to continue lifting until all liftoff be in
Vertical state；
By staff by the surface for assisting drawstring 2 that dirigible is made to be moved to moveable platform 4, continue to inflate dirigible
Until the buoyancy of dirigible meets pre-provisioning request；
Dirigible is reduced on moveable platform 4 by hoist engine 6, is determining that equipment is normal and external environment meets the requirements
In the case of, dirigible is carried by moveable platform 4 and removes boathouse, auxiliary drawstring 2 is released, is discharged dirigible by hoist engine 6
It to safe altitude, obtains after letting instruction fly away, constraint drawstring 3 is cut off by cutter device, completes to let dirigible fly away.
According to the mode that is preferably carried out present invention as described above, cutter device include Synchronization Control cabinet 5 and with it is synchronous
Two cutters that switch board 5 electrically connects, Synchronization Control cabinet 5 is arranged on moveable platform 4, is passing through moveable platform 4
It carries dirigible and removes boathouse and pass through hoist engine 6 and discharge dirigible to safe altitude, constrained at every and one is installed on drawstring 3
Cutter controls two constraint drawstrings described in two cutter turned off in synchronization by Synchronization Control cabinet 5.
The foregoing is only a preferred embodiment of the present invention, but protection scope of the present invention be not limited thereto,
Any one skilled in the art in the technical scope disclosed by the present invention, the change or replacement that can be readily occurred in,
It should be covered by the protection scope of the present invention.Therefore, protection scope of the present invention should be with the protection model of the claim
Subject to enclosing.
Claims (10)
1. a kind of dirigible lets system fly away, which is characterized in that the dirigible system of letting fly away includes：
Flexibility platform, the flexibility platform can be laid on the ground to support dirigible to be let fly away；
Moveable platform；
Hoist engine, the hoist engine are arranged on the moveable platform；
Power supply unit, the power supply unit are arranged on the moveable platform, can provide electric power for the hoist engine；
Drawstring is assisted, one end of the auxiliary drawstring is connected to dirigible head, and the other end of the auxiliary drawstring can be by working
Personnel operate；
Drawstring is constrained, one end of the constraint drawstring is connected to dirigible tail portion, and the other end for constraining drawstring is connected to described
Hoist engine；And
Cutter device, the cutter device can cut off the constraint drawstring to release the constraint to dirigible.
2. dirigible according to claim 1 lets system fly away, which is characterized in that the dirigible system of letting fly away is provided with two institutes
Constraint drawstring and two hoist engines are stated, the dirigible tail portion, which is symmetrically arranged, to be useful for connecting two constraint drawings respectively
Two connectors of rope, the every constraint drawstring are respectively connected to a hoist engine.
3. dirigible according to claim 1 lets system fly away, which is characterized in that the flexibility platform includes arrangement on the ground
Shield, the foam pad being arranged on the shield and the antistatic film being arranged on the foam pad.
4. dirigible according to claim 1 lets system fly away, which is characterized in that the constraint drawstring is disposed through described fly
Connector at ship tail portion is formed to wearing drawstring so that two fag ends of the constraint drawstring are connected to the hoist engine；It is described
The connector that auxiliary drawstring is disposed through at dirigible head is formed to wearing drawstring so that two fag end shapes of the auxiliary drawstring
Into free end can be operated by staff.
5. dirigible according to claim 4 lets system fly away, which is characterized in that the connector is U-shaped hook.
6. dirigible according to claim 2 lets system fly away, which is characterized in that the cutter device include Synchronization Control cabinet and
Two cutters, described two cutters can be separately mounted on two it is described constraint drawstrings on, described two cutters with
The Synchronization Control cabinet electrically connects so that the Synchronization Control cabinet can be controlled described in described two cutter turned off in synchronization two
Constrain drawstring.
7. the dirigible according to any one of claim 1 to 6 lets system fly away, which is characterized in that on the constraint drawstring
It is provided with pulling force sensor.
8. the dirigible that dirigible according to claim 1 lets system implementation fly away lets method fly away, which is characterized in that the dirigible is put
Winged method includes：
Flexibility platform is laid on the ground by the appropriate location in boathouse, and dirigible to be let fly away is arranged in the flexibility platform
On so that dirigible head is towards boathouse gate；
Moveable platform is arranged near one end for placing dirigible tail portion of the flexibility platform, in the moveable platform
Upper arrangement hoist engine and power supply unit；
The one end for assisting drawstring is connected to dirigible head, the one end for constraining drawstring is connected to dirigible tail portion, and constraint is drawn
The other end of rope is connected to the hoist engine；
To being inflated after dirigible integrated debugging by being arranged on the inflating port on dirigible head, led in gas replenishment process by staff
It crosses and operates the dirigible head that the free end control of the auxiliary drawstring is gradually lifted, when dirigible head in vertical state and reaches pre-
When determining height, stop to dirigible head inflating；
Dirigible is continued to inflate by the inflating port for being arranged on dirigible tail portion, dirigible is made to continue lifting until all liftoff in vertical
State；
Dirigible is made to be moved to the surface of the moveable platform by the auxiliary drawstring, continued to dirigible inflation until dirigible
Buoyancy meet pre-provisioning request；
Dirigible is reduced on the moveable platform by the hoist engine, carrying dirigible by the moveable platform removes
Boathouse releases auxiliary drawstring, is discharged dirigible to safe altitude by the hoist engine, the constraint is cut off by cutter device
Drawstring is completed to let dirigible fly away.
9. dirigible according to claim 8 lets method fly away, which is characterized in that is symmetrically connected to two constraint drawstrings winged
Ship tail portion, arranges two hoist engines on the moveable platform, and two constraints drawstring is respectively connected to a hoist engine.
10. dirigible according to claim 9 lets method fly away, which is characterized in that the cutter device includes Synchronization Control cabinet
Two cutters with being electrically connected with the Synchronization Control cabinet, the Synchronization Control cabinet is arranged on the moveable platform,
Dirigible removal boathouse is being carried by the moveable platform and is being discharged dirigible to safe altitude by the hoist engine,
A cutter is installed on every constraint drawstring, is controlled described in described two cutter turned off in synchronization by the Synchronization Control cabinet
Two constraint drawstrings.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711172743.7A CN108128437A (en) | 2017-11-22 | 2017-11-22 | Dirigible lets system fly away and dirigible lets method fly away |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711172743.7A CN108128437A (en) | 2017-11-22 | 2017-11-22 | Dirigible lets system fly away and dirigible lets method fly away |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN108128437A true CN108128437A (en) | 2018-06-08 |
Family
ID=62389733
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201711172743.7A Pending CN108128437A (en) | 2017-11-22 | 2017-11-22 | Dirigible lets system fly away and dirigible lets method fly away |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN108128437A (en) |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108891573A (en) * | 2018-07-13 | 2018-11-27 | 陕西铁鹰特种车有限公司 | The huge pollution-free transhipment of dirigible synchronizes the system of letting fly away |
| CN111547228A (en) * | 2020-04-15 | 2020-08-18 | 中国科学院空天信息创新研究院 | System for non-forming transfer and distribution of stratospheric airship |
| CN111547221A (en) * | 2020-04-15 | 2020-08-18 | 中国科学院空天信息创新研究院 | Non-forming distribution method for stratospheric airship |
| CN111547227A (en) * | 2020-04-02 | 2020-08-18 | 中国科学院空天信息创新研究院 | Method for issuing ultra-high altitude mooring aerostat |
| CN111824383A (en) * | 2020-06-15 | 2020-10-27 | 中国科学院空天信息创新研究院 | Synchronous release mechanism and high-altitude balloon restraint device |
| CN116353812A (en) * | 2023-05-22 | 2023-06-30 | 临舟(宁波)科技有限公司 | Offshore issuing system and method for stratospheric airship |
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| FR2985594A1 (en) * | 2012-01-10 | 2013-07-12 | Xiberras Louis | Device for cooling nuclear power plant by air, has balloon remotely controlled and maintained in association with ground by cables, which are wound and unwound by winches bonded to ground |
| CN103863546A (en) * | 2014-03-06 | 2014-06-18 | 马云鹏 | Novel large-sized aerostat releasing mode |
| CN104554695A (en) * | 2015-02-10 | 2015-04-29 | 襄阳宏伟航空器有限责任公司 | Remote control type precise airdrop system |
| CN106005350A (en) * | 2016-05-19 | 2016-10-12 | 东莞前沿技术研究院 | Flying method for large balloon |
| US9745040B1 (en) * | 2015-06-19 | 2017-08-29 | X Development Llc | Balloon launching apparatuses |
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| GB2164910A (en) * | 1984-10-02 | 1986-04-03 | Hiroo Kondo | Device for mooring airships |
| FR2985594A1 (en) * | 2012-01-10 | 2013-07-12 | Xiberras Louis | Device for cooling nuclear power plant by air, has balloon remotely controlled and maintained in association with ground by cables, which are wound and unwound by winches bonded to ground |
| CN103863546A (en) * | 2014-03-06 | 2014-06-18 | 马云鹏 | Novel large-sized aerostat releasing mode |
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Cited By (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108891573A (en) * | 2018-07-13 | 2018-11-27 | 陕西铁鹰特种车有限公司 | The huge pollution-free transhipment of dirigible synchronizes the system of letting fly away |
| CN108891573B (en) * | 2018-07-13 | 2023-09-05 | 陕西铁鹰特种车有限公司 | Pollution-free transportation synchronous flying system for giant airship |
| CN111547227A (en) * | 2020-04-02 | 2020-08-18 | 中国科学院空天信息创新研究院 | Method for issuing ultra-high altitude mooring aerostat |
| CN111547228A (en) * | 2020-04-15 | 2020-08-18 | 中国科学院空天信息创新研究院 | System for non-forming transfer and distribution of stratospheric airship |
| CN111547221A (en) * | 2020-04-15 | 2020-08-18 | 中国科学院空天信息创新研究院 | Non-forming distribution method for stratospheric airship |
| CN111547228B (en) * | 2020-04-15 | 2021-09-28 | 中国科学院空天信息创新研究院 | System for non-forming transfer and distribution of stratospheric airship |
| CN111824383A (en) * | 2020-06-15 | 2020-10-27 | 中国科学院空天信息创新研究院 | Synchronous release mechanism and high-altitude balloon restraint device |
| CN111824383B (en) * | 2020-06-15 | 2021-12-21 | 中国科学院空天信息创新研究院 | Synchronous release mechanism and high-altitude balloon restraint device |
| CN116353812A (en) * | 2023-05-22 | 2023-06-30 | 临舟(宁波)科技有限公司 | Offshore issuing system and method for stratospheric airship |
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Application publication date: 20180608 |