CN108725742A - Aerostatics lets constraint release device fly away and aerostatics lets method fly away - Google Patents
Aerostatics lets constraint release device fly away and aerostatics lets method fly away Download PDFInfo
- Publication number
- CN108725742A CN108725742A CN201710252035.8A CN201710252035A CN108725742A CN 108725742 A CN108725742 A CN 108725742A CN 201710252035 A CN201710252035 A CN 201710252035A CN 108725742 A CN108725742 A CN 108725742A
- Authority
- CN
- China
- Prior art keywords
- aerostatics
- fly away
- lets
- controller
- restriction rope
- 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
- 238000000034 method Methods 0.000 title claims abstract description 24
- 238000005422 blasting Methods 0.000 claims abstract description 87
- 238000004880 explosion Methods 0.000 claims abstract description 29
- 239000006260 foam Substances 0.000 claims description 5
- 238000000926 separation method Methods 0.000 claims description 5
- 239000000853 adhesive Substances 0.000 claims description 4
- 230000001070 adhesive effect Effects 0.000 claims description 4
- 239000011505 plaster Substances 0.000 claims description 4
- 230000005540 biological transmission Effects 0.000 claims description 3
- 230000000994 depressogenic effect Effects 0.000 claims description 2
- 239000001307 helium Substances 0.000 abstract description 35
- 229910052734 helium Inorganic materials 0.000 abstract description 35
- SWQJXJOGLNCZEY-UHFFFAOYSA-N helium atom Chemical compound [He] SWQJXJOGLNCZEY-UHFFFAOYSA-N 0.000 abstract description 35
- 238000009434 installation Methods 0.000 description 5
- 238000010276 construction Methods 0.000 description 4
- -1 polyethylene Polymers 0.000 description 4
- 239000002360 explosive Substances 0.000 description 3
- 239000004698 Polyethylene Substances 0.000 description 2
- 239000004743 Polypropylene Substances 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 238000007667 floating Methods 0.000 description 2
- 229920000573 polyethylene Polymers 0.000 description 2
- 229920001155 polypropylene Polymers 0.000 description 2
- 238000005273 aeration Methods 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 239000007789 gas Substances 0.000 description 1
Classifications
-
- 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
- B64F1/12—Anchoring
Abstract
Constraint release device is let fly away the present invention provides a kind of aerostatics and aerostatics lets method fly away.Aerostatics lets constraint release device fly away:At least first restriction rope;At least one second restriction rope;The both ends of blasting bolt separator are connected with the second end of corresponding first restriction rope and the second end of the second restriction rope respectively;Controller, which is arranged on blasting bolt separator and is controlled with blasting bolt separator, to be connected;Ground remote control component includes master remote controller, is provided on master remote controller and locks key, solving locking key and explosion control key;Ground remote control component further includes sub remote controller, and explosion control key is provided on sub remote controller.When use, operating personnel only need station to be instructed to controller emission control by ground remote control component on ground, so that controller runs corresponding program, blasting bolt separator is driven to explode, at this point, the first restriction rope and the second restriction rope disconnect, letting fly away for helium balloon is realized, it is simple and fast, and synchronism is high.
Description
Technical field
The present invention relates to release engineering device technique field, in particular to a kind of aerostatics let fly away constraint release device and
Aerostatics lets method fly away.
Background technology
Near space aerostatics is current global hot research problem, and letting fly away for aerostatics such as helium balloon is to close on sky
Between one of the critical issue studied of aerostatics, helium balloon is in the stage of letting fly away in gas replenishment process, and buoyancy gradually increases, sphere by
Edge up height, is influenced by ground air-flow, and helium balloon shape and position are unstable during letting fly away, needs to carry out about helium balloon
Beam waits for that inflation is completed to carry out constraint release before letting fly away, ensures that helium balloon smoothly goes up to the air, work is let in completion fly away.
Existing constraint release scheme is mainly connected by buckle releaser with helium balloon seine force-supporting belt using hoist engine rope
It connects, during letting fly away, mouthpart is taken off by release and carries out constraint release.
During constraint relief, disarmed mode in the prior art has the following defects:
1, taking off mouthpart releasing, time-consuming, and poor synchronization easily leads to and lets fly away unsuccessfully;
2, buckle releaser installation site is limited, can only be mounted near hoist engine, increases the length and quality of lift-off rope, drop
The low payload of helium balloon.
Invention content
Quickly fly away constraint relief and synchronism being let near space helium balloon the main purpose of the present invention is to provide a kind of
Good aerostatics lets constraint release device fly away and aerostatics lets method fly away.
To achieve the goals above, according to an aspect of the invention, there is provided a kind of aerostatics lets constraint release dress fly away
It sets, including:At least first restriction rope, the first end of the first restriction rope with aerostatics for connecting;At least one second about
Binding yarn, the second restriction rope are arranged correspondingly with the first restriction rope, and the first end of the second restriction rope is for fixing on the ground;
Blasting bolt separator, the both ends of blasting bolt separator respectively with the second end and second of corresponding first restriction rope
The second end of restriction rope connects;Controller, controller be arranged on blasting bolt separator and with blasting bolt separator
Control connection;Ground remote control component, ground remote control component is used for controller emission control instruction so that blasting bolt separation dress
Explosion is set to detach corresponding first restriction rope and the second restriction rope, ground remote control component includes master remote controller, on master remote controller
It is provided with the locking key for being locked to controller, the solving locking key for being unlocked to controller and for control
Device sends the explosion control key of guiding detonating controlling instruction;Ground remote control component further includes sub remote controller, is provided on sub remote controller quick-fried
Fried control key.
Further, the periphery of blasting bolt separator is provided with mounting portion, and controller is fixed on by fastening structure
On mounting portion.
Further, mounting portion is to wrap up in the foam being located on blasting bolt separator.
Further, fastening structure is positioning adhesive plaster.
Further, power supply and antenna are provided on controller.
Further, explosion control key includes at least two buttons, to controller when at least two buttons are concurrently depressed
Send guiding detonating controlling instruction.
Further, blasting bolt separator includes:The both ends of sleeve, sleeve are both provided with along the axially extending of sleeve
Mounting hole;Two blasting bolts, two blasting bolts are separately mounted in the mounting hole at sleeve both ends, and the bottom of mounting hole
It is provided with the threaded hole being connect with blasting bolt.
Further, sleeve includes two end sleeves and the intermediate sleeve that is connected between two end sleeves, two
Mounting hole is opened in respectively in two end sleeves, and blasting bolt includes main part and the threaded shank that is connected with main part, intermediate
Sleeve has threaded hole and the both ends through intermediate sleeve, the main part of two blasting bolts are respectively arranged in mounting hole, spiral shell
Bar portion is meshed with the internal thread at the threaded hole both ends of intermediate sleeve respectively, so that two blasting bolts are connected by intermediate sleeve
It connects.
Further, two end sleeves are connected adjacent to the end formation one of intermediate sleeve with corresponding mounting hole
Connecting hole, the aperture of connecting hole are less than the aperture of mounting hole so that mounting hole forms a stepped hole with connecting hole;Outside main part
Diameter is more than the outer diameter of threaded shank, and the aperture of mounting hole is more than the outer diameter of main part, and the aperture of connecting hole is less than the outer diameter of main part
And more than the outer diameter of threaded shank, so that main part is stayed in mounting hole to make threaded shank be pierced by end sleeve.
Further, end sleeve and intermediate sleeve are connected with each other, are structure as a whole or the structure to be separated from each other.
Further, resigning breach is provided on sleeve, the pilot on blasting bolt is pierced by sleeve from resigning breach.
Further, it further includes connector that aerostatics, which lets constraint release device fly away, and connector is used for the first restriction rope
Second end and the second end of the second restriction rope are connected to the end of blasting bolt separator.
Further, connector is connection bolt.
Further, the first restriction rope and the second restriction rope are four, four first restriction ropes and four second constraints
Rope is separately positioned on all directions four direction of aerostatics.
Another invention according to the present invention provides a kind of aerostatics and lets method fly away, and aerostatics lets about method fly away using upper
The aerostatics stated lets the realization of constraint release device fly away, and the aerostatics method of letting fly away includes the following steps:It is detached and is filled using blasting bolt
It sets and connects corresponding first restriction rope and the second restriction rope;It is sent and is locked to controller using the locking key of master remote controller
Instruction;Aerostatics is inflated, until aerostatics rises to predetermined altitude;It is sent out to controller using the solving locking key of master remote controller
Send unlock instruction;Using sub remote controller and or master remote controller on explosion control key to controller send guiding detonating controlling instruct, lead to
Cross controller control blasting bolt separator explosion and so that the first restriction rope and the second restriction rope disconnect it is floating to let fly away
Pocket.
Further, aerostatics is let fly away all controllers on constraint release device and is referred to using identical frequency band and control
It enables.
Further, at the same press explosion control key all buttons to controller send guiding detonating controlling instruction, otherwise not
Send guiding detonating controlling instruction.
It applies the technical scheme of the present invention, since the aerostatics in the present invention is let fly away in constraint release device through the spiral shell that explodes
Bolt separator connects the first restriction rope and the second restriction rope, when needing to let aerostatics fly away, first by the floating of unaerated
Device is placed in ground laying area on the ground, and by the first restriction rope, the second restriction rope, blasting bolt separator and
After controller assembles, aerostatics is inflated using air blower so that aerostatics slowly rises, when needing to aerostatics, example
When such as helium balloon constraint relief, operating personnel only need station to refer to controller emission control by ground remote control component on ground
It enables so that controller runs corresponding program, drives blasting bolt separator to explode, at this point, the first restriction rope and second is about
Binding yarn disconnects, and realizes letting fly away for helium balloon, simple and fast.When the first restriction rope and the second restriction rope are set as more
When, it is disconnected convenient for making more first restriction ropes and the second restriction rope realize to synchronize, ensures the smooth lift-off of helium balloon.
Description of the drawings
The accompanying drawings which form a part of this application are used to provide further understanding of the present invention, and of the invention shows
Meaning property embodiment and its explanation are not constituted improper limitations of the present invention for explaining the present invention.In the accompanying drawings:
The aerostatics that Fig. 1 diagrammatically illustrates the present invention lets the blasting bolt separator part of constraint release device fly away
Front view;
The aerostatics that Fig. 2 diagrammatically illustrates the present invention lets the blasting bolt separator part of constraint release device fly away
Vertical view;
The aerostatics that Fig. 3 diagrammatically illustrates the present invention lets the blasting bolt separator part of constraint release device fly away
Side view;
Fig. 4 diagrammatically illustrates the connection control planning that aerostatics of the invention lets the control section of constraint release device fly away
Figure;And
The aerostatics that Fig. 5 diagrammatically illustrates the present invention lets vertical view when constraint release device lets aerostatics fly away fly away.
Wherein, above-mentioned attached drawing includes the following drawings label:
10, the first restriction rope;20, the second restriction rope;30, blasting bolt separator;31, sleeve;311, resigning breach;
31a, end sleeve;31b, intermediate sleeve;32, mounting hole;32a, connecting hole;33, threaded hole;34, blasting bolt;34a, main body
Portion;34b, threaded shank;40, connector;50, hoist engine;60, helium balloon;70, controller;71, power supply;72, antenna;80,
Ground remote control component;81, master remote controller;811, key is locked;812, solving locking key;813, explode control key;82, sub remote controller;90,
Mounting portion;100, ground laying area;110, air blower.
Specific implementation mode
It should be noted that in the absence of conflict, the features in the embodiments and the embodiments of the present application can phase
Mutually combination.The present invention will be described in detail below with reference to the accompanying drawings and embodiments.
It should be noted that term used herein above is merely to describe specific implementation mode, and be not intended to restricted root
According to the illustrative embodiments of the application.As used herein, unless the context clearly indicates otherwise, otherwise singulative
It is also intended to include plural form, additionally, it should be understood that, when in the present specification using term "comprising" and/or " packet
Include " when, indicate existing characteristics, step, operation, device, component and/or combination thereof.
It should be noted that term " first " in the description and claims of this application and above-mentioned attached drawing, "
Two " etc. be for distinguishing similar object, without being used to describe specific sequence or precedence.It should be appreciated that using in this way
Data can be interchanged in the appropriate case, so that presently filed embodiment described herein for example can be in addition to herein
Sequence other than those of diagram or description is implemented.In addition, term " comprising " and " having " and their any deformation, it is intended that
Be to cover it is non-exclusive include, for example, containing the process of series of steps or unit, method, system, product or equipment not
Those of be necessarily limited to clearly to list step or unit, but may include not listing clearly or for these processes, side
The intrinsic other steps of method, product or equipment or unit.
For ease of description, herein can with use space relative terms, as " ... on ", " in ... top ",
" ... upper surface ", " above " etc., for describing such as a device shown in the figure or feature and other devices or spy
The spatial relation of sign.It should be understood that spatially relative term is intended to comprising the orientation in addition to device described in figure
Except different direction in use or operation.For example, if the device in attached drawing is squeezed, it is described as " in other devices
It will be positioned as " under other devices or construction after part or construction top " or the device of " on other devices or construction "
Side " or " under other devices or construction ".Thus, exemplary term " ... top " may include " ... top " and
" in ... lower section " two kinds of orientation.The device can also other different modes positioning (be rotated by 90 ° or be in other orientation), and
And respective explanations are made to the opposite description in space used herein above.
Shown in Fig. 1 to Fig. 5, according to an embodiment of the invention, provides a kind of aerostatics and lets constraint release device fly away,
It includes at least first restriction rope 10, at least second restriction rope 20, explosion that this, which faces aerostatics to let constraint release device fly away,
Bolt separator 30, controller 70 and ground remote control component 80.Aerostatics in the present invention can be that aerostat such as faces
Near space aerostatics, in the present embodiment, which is the helium balloon 60 applied near space, which is substantially in ball
Shape.
Wherein, the first end of the first restriction rope 10 with helium balloon 60 for connecting;Second restriction rope 20 and the first restriction rope
10 are arranged correspondingly, and the first end of the second restriction rope 20 is for fixing on the ground;When installation, blasting bolt is detached
The both ends of device 30 are connect with the second end of the second end of the first restriction rope 10 of corresponding setting and the second restriction rope 20 respectively;
Controller 70, which is arranged on blasting bolt separator 30 and is controlled with blasting bolt separator 30, to be connected;Ground remote control component
80 are used for 70 emission control instruction of controller so that blasting bolt separator 30 is actually occurring explosion suitable, and then solves
Except the constraint to helium balloon 60.
It is let fly away in constraint release device by aerostatics in this present embodiment and is connected by blasting bolt separator 30
The aerostatics of unaerated is placed on ground by the first restriction rope 10 and the second restriction rope 20 first when needing to let aerostatics fly away
On ground laying area 100 in, and by the first restriction rope 10, the second restriction rope 20, blasting bolt separator 30 and control
After device 70 assembles, aerostatics is inflated using air blower 110 so that aerostatics slowly rises, when needing to aerostatics, example
When such as 60 constraint relief of helium balloon, operating personnel only need station to emit control to controller 70 by ground remote control component 80 on ground
System instruction so that controller 70 runs corresponding program, drives blasting bolt separator 30 to explode, at this point, the first restriction rope
10 and second restriction rope 20 disconnect, realize that helium balloon 60 is let fly away, it is simple and fast.When by the first restriction rope 10 and second about
When binding yarn 20 is set as more, convenient for make more first restriction ropes 10 and the second restriction rope 20 realize synchronize disconnect, protect
Demonstrate,prove the smooth lift-off of helium balloon 60.
In conjunction with shown in Fig. 1 to Fig. 3, the blasting bolt separator 30 in the present embodiment includes sleeve 31 and two explosion spiral shells
Bolt 34.
Wherein, the sleeve 31 in the present embodiment includes being located at the end sleeve at 31 both ends of sleeve and being connected to two end sleeves
Intermediate sleeve between cylinder, the intermediate throughholes of end sleeve form mounting hole 32, and when installation, two blasting bolts 34 are installed respectively
In the mounting hole 32 of the end sleeve at the both ends of sleeve 31, the aperture of the intermediate throughholes of intermediate sleeve is less than in end sleeve
Between through-hole, the and bottom of mounting hole 32 is provided with the threaded hole being connect with blasting bolt 34 in the intermediate throughholes of intermediate sleeve
33, which extends along the axis direction of sleeve 31, and after installing, two blasting bolts 34 are oppositely arranged, and is convenient for
Suitable opportunity occurs explosion and releases the constraint to aerostatics.
Two above-mentioned blasting bolts 34 are internally provided with explosive, when needing to 60 constraint relief of helium balloon, only need
Make explosive charge in blasting bolt 34, it is simple to operate.
The position that the middle part of sleeve 31 in the present embodiment is threaded hole 33 is relatively thin, i.e. the outer diameter of intermediate sleeve
It is smaller than the outer diameter of end sleeve, and the explosive in blasting bolt 34 is mounted on the end of blasting bolt 34, it is quick-fried when starting
Fried bolt 34 realizes that explosion time, sleeve 31 generate explosion in the both ends for being provided with threaded hole 33, i.e. the both ends explosion of intermediate sleeve
Section and disconnect so that the first restriction rope 10 and the second restriction rope 20 disconnect so that 60 constraint relief of helium balloon and
It lets fly away.
In other embodiments of the invention, a blasting bolt 34 can also be only set, i.e., only in two end sleeves
In one in be arranged blasting bolt 34, as long as sleeve 31 can be blown up to other modes of texturing split, the present invention guarantor
Within the scope of shield.
During actual installation, it is provided with resigning breach 311 on the sleeve 31 in the present embodiment, blasting bolt is installed
When 34, the pilot on blasting bolt 34 is set to be pierced by sleeve 31 from the resigning breach 311, and then convenient for connecting with controller 70
It connects.Certainly, in other embodiments of the invention, can also above-mentioned resigning breach 311 be set to through-hole or groove, as long as
Other modes of texturing under the design of the present invention, within protection scope of the present invention.
In other unshowned embodiments of the present invention, it can also be not provided with pilot, and set in blasting bolt
Control chip is set, by remote controler remote control blasting bolt 34 is exploded.Shown in Fig. 1 to Fig. 3, the present embodiment
In aerostatics to let constraint release device fly away further include connector 40, which is used for the second end of the first restriction rope 10
The end of blasting bolt separator 30 is connected to the second end of the second restriction rope 20.
Preferably, the connector 40 in the present embodiment is connection bolt, installs the first restriction rope 10 and the second restriction rope 20
When, the through-hole passed through for connection bolt is provided on the side wall at the both ends of sleeve 31, first so that connection bolt is along perpendicular to set
The direction of the axis of cylinder 31 is threaded through in through-hole, then by the second end of the second end of the first restriction rope 10 and the second restriction rope 20
It is fixed on the stud of connection bolt, fixing nut is finally used to be fixed on bolt is connected on sleeve 31, it is simple and convenient.
In other embodiments of the invention, can also will connection bolt be set as pin either rivet or axis pin or
The structures such as buckle, as long as other deformations that the first restriction rope 10 and the second restriction rope 20 can be fixedly connected on sleeve 31
Mode, within protection scope of the present invention.
In the present embodiment, the first restriction rope 10 and the second restriction rope 20 are more, more first restriction ropes 10 and
Two restriction ropes 20 are arranged correspondingly, and are realized and connected by blasting bolt separator 30, when needs are contacted to helium balloon
When 60 constraint, it is only necessary to control the blasting bolt 34 on blasting bolt separator 30 by controller 70 and explode simultaneously
, the synchronism that is easy to implement during helium balloon 60 is let fly away.
Specifically, the first restriction rope 10 in the present embodiment is the seine force-supporting belt that polyethylene is made, the seine
Force-supporting belt is four, and four seine force-supporting belts are uniformly connected to the periphery of helium balloon 60, convenient for steadily constraining in helium balloon
In near space.Seine force-supporting belt in the present embodiment is high-strength polyethylene band, is sewed in spherome surface.
The periphery of blasting bolt separator 30 in the present embodiment is provided with mounting portion 90, and controller 70 is tied by fastening
Structure (not shown) is fixed on mounting portion 90.
Preferably, the mounting portion 90 in the present embodiment is to wrap up in the foam being located on blasting bolt separator 30, fastening knot
Structure is positioning adhesive plaster, and when installation, controller 70 is mounted on foam, and controller 70 is then mounted on foam by adhesive plaster
On, it is simple in structure, it is reliable and stable.
Certainly, in other embodiments of the invention, mounting portion 90 and location structure can also be disposed as to positioning card
Controller 70, is fixed on blasting bolt separator 30 by button by locating fastener, as long as under the design of the present invention
Other modes of texturing, within protection scope of the present invention.
It is provided with power supply 71 and antenna 72 on controller 70 in the present embodiment, by the effect of power supply 71,
Convenient for being powered to controller 70, by the effect of antenna 72, convenient for receiving the control instruction that ground remote control component 80 is sent.
Power supply 71 in the present embodiment could be provided as other power supply units such as accumulator or rechargeable battery, as long as
It is other modes of texturing under the design of the present invention, is within the scope of the invention.
In conjunction with shown in Fig. 4, the ground remote control component 80 in the present embodiment includes master remote controller 81, is set on the master remote controller 81
It is equipped with the locking key 811 for being locked to controller 70, the solving locking key 812 for being unlocked to controller and is used for
The explosion control key 813 of guiding detonating controlling instruction is sent to controller 70.
Preferably, explosion control key 813 includes at least two buttons, to controller 70 when at least two buttons are pressed simultaneously
Guiding detonating controlling instruction is sent, prevents from accidentally pressing any one button and so that blasting bolt separator 30 is missed quick-fried.Pressing in the present embodiment
Key is two, certainly, in other embodiments of the invention, it is more than two can also to set button to.
Ground remote control component 80 in the present embodiment further includes sub remote controller 82, and explosion control is provided on sub remote controller 82
Key 813.
It locks to controller 70 in use, pressing and locking key 811, controller 70 can not receive the transmission of sub remote controller 82
Control instruction.It presses solving locking key 812 to unlock to controller 70, while K1 the and K2 keys for the control key 813 that explodes then send ignition control
System instruction, does not otherwise send instruction.Controller 70 still can receive the control instruction that master remote controller 81 is sent in locking state.
Aerostatics lets all controllers 70 on constraint release device fly away and uses similar frequency bands and instruction, i.e. a main remote control
Device 81 and sub remote controller 82 can send all controllers 70 guiding detonating controlling instruction.
In the present embodiment, it further includes hoist engine 50 that aerostatics, which lets constraint release device fly away, and the hoist engine 50 and second is about
Binding yarn 20 connects, and accordingly, the hoist engine 50 in the present embodiment is four, it is preferable that the second restriction rope 20 is hoist engine rope, should
Hoist engine rope is the polypropylene rope of a diameter of 16mm, by blasting bolt separator 30 with four seine load band connections;Inflation
In the process, four first restriction ropes 10 and four second restriction ropes 20 are arranged on all directions four direction of helium balloon 60,
It controls four groups of hoist engines 50 to work, four polypropylene rope length is adjusted, so as to adjust 60 height of helium balloon and position.
According to another aspect of the present invention, it provides a kind of aerostatics and lets method fly away, the aerostatics in the present embodiment is let fly away
Method is let constraint release device fly away using above-mentioned aerostatics and is realized.
Specifically, the aerostatics method of letting fly away includes the following steps:
During aerostatics is let fly away, first with blasting bolt separator 30 by corresponding first restriction rope 10 and
Two restriction ropes 20 connect.It recycles the locking key 811 on master remote controller 81 to be sent to controller 70 and locks instruction, make control
Device 70 is in locking state;Air blower 110 is recycled to be inflated aerostatics so that aerostatics rises to predetermined altitude, so
The solving locking key 812 of master remote controller 81 is utilized to send unlock instruction to controller 70 afterwards, convenient for ground remote control component 80 to controller
70 send guiding detonating controlling instruction;Finally recycle explosion control key 813 on sub remote controller 82 or master remote controller 81 to control
Device 70 sends guiding detonating controlling instruction, is controlled by blasting bolt separator 30 explodes so that the first restriction rope 10 by controller 70
It is disconnected with the second restriction rope 20 to let aerostatics fly away, prevents from accidentally pressing explosion control key 813 so that blasting bolt separator
30 explosions.
During actual use, controller 70 by the locking key 811 on master remote controller 81 lock in often lock
State is to prevent explosion control key 813 from sending guiding detonating controlling instruction to controller 70, until solving locking key 812 is sent to controller 70
Unlock instruction ensures that the aerostatics in the present embodiment lets the control stability of the control method of constraint release device and reliable fly away
Property.
Aerostatics in the present embodiment let fly away all controllers 70 on constraint release device using identical frequency band and
Control instruction, i.e. a master remote controller 81 and sub remote controller 82 can send all controllers 70 guiding detonating controlling instruction.
It locks to controller 70 in use, pressing and locking key 811, controller 70 can not receive the transmission of sub remote controller 82
Control instruction.It presses solving locking key 812 to unlock to controller 70, while K1 the and K2 keys for the control key 813 that explodes then send ignition control
System instruction, does not otherwise send instruction, avoids accidentally pressing K1 or K2 keys and blasting bolt separator 30 being caused to explode.
As it can be seen that when letting aerostatics fly away, in aeration phase, after receiving 70 unlock instruction of controller, two master remote controllers 81 are grasped
Make personnel and march around the arena respectively to be unlocked operation to four group controllers 70.Ensure not will produce maloperation before unlock.Control
After device 70 processed receives guiding detonating controlling instruction, four 82 operating personnel of sub remote controller press rapidly K1 and K2 and ignite key simultaneously, four groups
Blasting bolt separator 30 on the hawser of hoist engine 50 acts on simultaneously, and the hawser of hoist engine 50 is detached with seine force-supporting belt,
Aerostatics constraint release is completed to let fly away.The configuration of two 81 operating personnel of master remote controller and four 82 operating personnel of sub remote controller
Design ensures effectively to send guiding detonating controlling instruction.
During constraining aerostatics, such as helium balloon 60, the hoist engine rope of seine force-supporting belt and hoist engine 50 passes through
Connection is bolted to sleeve 31, and two blasting bolts 34 are installed in series, and one end is located in the mounting hole 32 of sleeve 31, the other end
It being connected through a screw thread to threaded hole 33, after ground remote control component 80 sends out guiding detonating controlling instruction, two blasting bolts 34 detonate,
Ensure that blasting bolt separator 30 explodes to disconnect, realize separation, releases the constraint to helium balloon 60, two blasting bolts 34
Redundancy Design ensures the reliable of separation.
During near space helium balloon 60 is let fly away, the synchronism and rapidity of 60 constraint release of helium balloon are high.The present invention
It is breakthrough take 34 Redundancy Design of double blasting bolts, and devise branch sleeve 31, solve near space helium balloon and put
Fly the synchronism of constraint release, rapidity problem, convenient for letting helium balloon 60 fly away, the present invention effectively realizes near space helium
The simultaneously and rapidly releasing constrained when the constraint of 60 position of helium balloon is fixed during ball is let fly away and lets fly away, ensure to let fly away it is smooth into
Row.
The foregoing is only a preferred embodiment of the present invention, is not intended to restrict the invention, for the skill of this field
For art personnel, the invention may be variously modified and varied.All within the spirits and principles of the present invention, any made by repair
Change, equivalent replacement, improvement etc., should all be included in the protection scope of the present invention.
Claims (17)
1. a kind of aerostatics lets constraint release device fly away, which is characterized in that including:
At least first restriction rope (10), the first end of first restriction rope (10) with aerostatics for connecting;
At least one second restriction rope (20), second restriction rope (20) set correspondingly with first restriction rope (10)
It sets, the first end of second restriction rope (20) is for fixing on the ground;
Blasting bolt separator (30), the both ends of the blasting bolt separator (30) are respectively with corresponding described first
The second end of restriction rope (10) is connected with the second end of second restriction rope (20);
Controller (70), the controller (70) be arranged on the blasting bolt separator (30) and with the blasting bolt
Separator (30) control connection;
Ground remote control component (80), the ground remote control component (80) be used for the controller (70) emission control instruct so that
Blasting bolt separator (30) explosion is to detach corresponding first restriction rope (10) and second restriction rope
(20), the ground remote control component (80) includes master remote controller (81), is provided with for described on the master remote controller (81)
Locking key (811) that controller (70) is locked, the solving locking key (812) for being unlocked to the controller (70) and
Explosion control key (813) for sending guiding detonating controlling instruction to the controller (70);
The ground remote control component (80) further includes sub remote controller (82), and the explosion control is provided on the sub remote controller (82)
Key (813) processed.
2. aerostatics according to claim 1 lets constraint release device fly away, which is characterized in that the blasting bolt separation dress
The periphery for setting (30) is provided with mounting portion (90), and the controller (70) is fixed on the mounting portion (90) by fastening structure
On.
3. aerostatics according to claim 2 lets constraint release device fly away, which is characterized in that the mounting portion (90) is to wrap up in
The foam being located on the blasting bolt separator (30).
4. aerostatics according to claim 2 lets constraint release device fly away, which is characterized in that the fastening structure is positioning
Adhesive plaster.
5. aerostatics according to claim 1 lets constraint release device fly away, which is characterized in that set on the controller (70)
It is equipped with power supply (71) and antenna (72).
6. aerostatics according to claim 1 lets constraint release device fly away, which is characterized in that the explosion control key
(813) include at least two buttons, draw to described in the controller (70) transmission when at least two button is concurrently depressed
Quick-fried control instruction.
7. aerostatics according to claim 1 lets constraint release device fly away, which is characterized in that the blasting bolt separation dress
Setting (30) includes:
Sleeve (31), the both ends of the sleeve (31) are both provided with the axially extending mounting hole (32) along the sleeve (31);
Two blasting bolts (34), described two blasting bolts (34) are separately mounted to the mounting hole at the sleeve (31) both ends
(32) in, and the bottom of the mounting hole (32) is provided with the threaded hole (33) being connect with the blasting bolt (34).
8. aerostatics according to claim 7 lets constraint release device fly away, which is characterized in that the sleeve (31) includes two
A end sleeve (31a) and the intermediate sleeve (31b) being connected between two end sleeves (31a), two mounting holes (32) point
Be not opened in two end sleeves (31a), the blasting bolt (34) include main part (34a) and with main part (34a) phase
Threaded shank (34b) even, the intermediate sleeve (31b) have threaded hole (33) and the both ends through the intermediate sleeve (31b),
The main part (34a) of described two blasting bolts (34) is respectively arranged in the mounting hole (32), the threaded shank (34b) point
It is not meshed with the internal thread at the threaded hole of the intermediate sleeve (31b) (33) both ends, so that two blasting bolts (34)
It is connected by the intermediate sleeve (31b).
9. aerostatics according to claim 8 lets constraint release device fly away, which is characterized in that described two end sleeves
(31a) forms a connecting hole being connected with corresponding mounting hole (32) adjacent to the end of the intermediate sleeve (31b)
(32a), the aperture of the connecting hole (32a) are less than the aperture of the mounting hole (32) so that the mounting hole (32) with it is described
Connecting hole (32a) forms a stepped hole;The outer diameter of the main part (34a) is more than the outer diameter of the threaded shank (34b), the peace
The aperture for filling hole (32) is more than the outer diameter of main part (34a), and the aperture of the connecting hole (32a) is less than the outer of main part (34a)
Diameter and more than threaded shank (34b) outer diameter, so that main part (34a) is stayed to make threaded shank (34b) be pierced by end sleeve (31a)
In mounting hole (32).
10. aerostatics according to claim 8 lets constraint release device fly away, which is characterized in that the end sleeve (31a)
It is connected with each other, is structure as a whole or structure to be separated from each other with the intermediate sleeve (31b).
11. aerostatics according to claim 7 lets constraint release device fly away, which is characterized in that set on the sleeve (31)
It is equipped with resigning breach (311), the pilot on the blasting bolt (34) is pierced by the sleeve from the resigning breach (311)
(31)。
12. aerostatics according to claim 1 lets constraint release device fly away, which is characterized in that the aerostatics is let fly away about
It further includes connector (40) that beam, which releases device, and the connector (40) is used for the second end of first restriction rope (10) and institute
The second end for stating the second restriction rope (20) is connected to the end of the blasting bolt separator (30).
13. aerostatics according to claim 12 lets constraint release device fly away, which is characterized in that the connector (40) is
Connect bolt.
14. aerostatics according to any one of claim 1 to 13 lets constraint release device fly away, which is characterized in that described
First restriction rope (10) and second restriction rope (20) are four, four first restriction ropes (10) and four described
Two restriction ropes (20) are separately positioned on all directions four direction of the aerostatics.
15. a kind of aerostatics lets method fly away, which is characterized in that the aerostatics is let method fly away and appointed using in claim 1 to 14
Aerostatics described in one lets the realization of constraint release device fly away, and the aerostatics method of letting fly away includes the following steps:
Corresponding first restriction rope (10) and the second restriction rope (20) are connected using the blasting bolt separator (30)
It picks up and;
It is sent to the controller (70) using the locking key (811) of the master remote controller (81) and locks instruction;
Aerostatics is inflated, until the aerostatics rises to predetermined altitude;
Using the solving locking key (812) of the master remote controller (81) unlock instruction is sent to the controller (70);
Using the sub remote controller (82) and or the master remote controller (81) on the explosion control key (813) to the control
Device (70) processed sends guiding detonating controlling instruction, by the controller (70) controls blasting bolt separator (30) explosion
So that first restriction rope (10) and second restriction rope (20) are disconnected to let the aerostatics fly away.
16. aerostatics according to claim 15 lets method fly away, which is characterized in that the aerostatics lets constraint release dress fly away
All controllers (70) set use identical frequency band and control instruction.
17. aerostatics according to claim 15 lets method fly away, which is characterized in that while pressing the explosion control key
(813) all buttons send guiding detonating controlling instruction to the controller (70), otherwise do not send guiding detonating controlling instruction.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201710252035.8A CN108725742A (en) | 2017-04-17 | 2017-04-17 | Aerostatics lets constraint release device fly away and aerostatics lets method fly away |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201710252035.8A CN108725742A (en) | 2017-04-17 | 2017-04-17 | Aerostatics lets constraint release device fly away and aerostatics lets method fly away |
Publications (1)
Publication Number | Publication Date |
---|---|
CN108725742A true CN108725742A (en) | 2018-11-02 |
Family
ID=63924684
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201710252035.8A Pending CN108725742A (en) | 2017-04-17 | 2017-04-17 | Aerostatics lets constraint release device fly away and aerostatics lets method fly away |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN108725742A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
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 |
Citations (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2282366A1 (en) * | 1974-08-19 | 1976-03-19 | Centre Nat Etd Spatiales | Controlled or automatic balloon release mechanism - with clamp on neck of envelope released by explosive bolts |
CN1278325A (en) * | 1997-11-06 | 2000-12-27 | 罗克泰克公开有限公司 | Controlled electromagnetic induction detonation system of a detonatable material |
US6234425B1 (en) * | 1999-05-11 | 2001-05-22 | Winzen Engineering Incorporated | Release fitting for balloons |
KR20120056731A (en) * | 2010-11-25 | 2012-06-04 | 한국항공우주연구원 | Apparatus for Take-off and Climb a Fixed wing Aircraft without a Runway |
CN102514714A (en) * | 2011-12-29 | 2012-06-27 | 天津曙光敬业科技有限公司 | Device and method for reducing harm caused by out-of-control of rotor helicopter |
CN103863546A (en) * | 2014-03-06 | 2014-06-18 | 马云鹏 | Novel large-sized aerostat releasing mode |
US9016634B1 (en) * | 2013-04-30 | 2015-04-28 | Google Inc. | Payload cut-down mechanism |
CN105109660A (en) * | 2015-08-14 | 2015-12-02 | 东莞前沿技术研究院 | Cutting releasing system |
CN105388912A (en) * | 2015-12-22 | 2016-03-09 | 上海交通大学 | Unmanned aerostat emergency control system and method |
CN105667755A (en) * | 2016-03-03 | 2016-06-15 | 上海交通大学 | Multi-point mooring device and flying method for aerostat |
CN106553747A (en) * | 2015-09-28 | 2017-04-05 | 东莞前沿技术研究院 | The piece-rate system of ballast |
CN206900627U (en) * | 2017-04-17 | 2018-01-19 | 深圳光启空间技术有限公司 | Aerostatics lets constraint release device fly away |
-
2017
- 2017-04-17 CN CN201710252035.8A patent/CN108725742A/en active Pending
Patent Citations (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2282366A1 (en) * | 1974-08-19 | 1976-03-19 | Centre Nat Etd Spatiales | Controlled or automatic balloon release mechanism - with clamp on neck of envelope released by explosive bolts |
CN1278325A (en) * | 1997-11-06 | 2000-12-27 | 罗克泰克公开有限公司 | Controlled electromagnetic induction detonation system of a detonatable material |
US6234425B1 (en) * | 1999-05-11 | 2001-05-22 | Winzen Engineering Incorporated | Release fitting for balloons |
KR20120056731A (en) * | 2010-11-25 | 2012-06-04 | 한국항공우주연구원 | Apparatus for Take-off and Climb a Fixed wing Aircraft without a Runway |
CN102514714A (en) * | 2011-12-29 | 2012-06-27 | 天津曙光敬业科技有限公司 | Device and method for reducing harm caused by out-of-control of rotor helicopter |
US9016634B1 (en) * | 2013-04-30 | 2015-04-28 | Google Inc. | Payload cut-down mechanism |
CN103863546A (en) * | 2014-03-06 | 2014-06-18 | 马云鹏 | Novel large-sized aerostat releasing mode |
CN105109660A (en) * | 2015-08-14 | 2015-12-02 | 东莞前沿技术研究院 | Cutting releasing system |
CN106553747A (en) * | 2015-09-28 | 2017-04-05 | 东莞前沿技术研究院 | The piece-rate system of ballast |
CN105388912A (en) * | 2015-12-22 | 2016-03-09 | 上海交通大学 | Unmanned aerostat emergency control system and method |
CN105667755A (en) * | 2016-03-03 | 2016-06-15 | 上海交通大学 | Multi-point mooring device and flying method for aerostat |
CN206900627U (en) * | 2017-04-17 | 2018-01-19 | 深圳光启空间技术有限公司 | Aerostatics lets constraint release device fly away |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
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 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
AU2005207595B2 (en) | Remote firing system | |
US20150241190A1 (en) | Electronic safe/arm system and methods of use thereof | |
US20100155540A1 (en) | Sling release mechanism | |
CN112478203B (en) | Recovery landing system suitable for large-load manned spacecraft | |
CN108725742A (en) | Aerostatics lets constraint release device fly away and aerostatics lets method fly away | |
WO2011091003A1 (en) | Airborne guidance unit for precision aerial delivery | |
CN105992730B (en) | Mechanical component for lifting balloon | |
CN110030891B (en) | Tunnel face full-section smooth blasting initiation system network | |
US9796484B2 (en) | Satellite system comprising two satellites attached to each other and method for launching them into orbit | |
CN206900627U (en) | Aerostatics lets constraint release device fly away | |
JPH036040B2 (en) | ||
TWI759797B (en) | Drone with parachute and control method thereof | |
US20200032466A1 (en) | Avalanche Control Device | |
US20220274705A1 (en) | Method, device, and system for avalanche control | |
CN206537481U (en) | Aerostatics lets constraint release device fly away | |
US4955563A (en) | Apparatus and method for controlled simultaneous opening of clustered parachutes | |
US5054398A (en) | Process and apparatus for dispersing submunition bodies | |
KR102114295B1 (en) | A holding and release mechanism for deployable structures cube satellite with multi-axis constraint capability | |
US9598179B2 (en) | Conductive attachment device | |
KR101267909B1 (en) | Parachute device | |
CN112224422B (en) | Dynamic test device for transmitting parachute | |
JP7218641B2 (en) | Remote Ignition Systems for Fireworks, Wireless Ignition Units, and Wireless Ignition Operators | |
JP6999355B2 (en) | Wireless non-explosive ignition tool, wireless non-explosive crushing system, and wireless non-explosive crushing method | |
RU2643307C2 (en) | Method of space installation of initially disclosed heat-resistant solid cordless parachute for multiton cargoes descent from the planet orbit | |
CN114056572A (en) | Air-drop type fuel oil power unmanned aerial vehicle, aerial vehicle and air-drop method |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PB01 | Publication | ||
PB01 | Publication | ||
SE01 | Entry into force of request for substantive examination | ||
SE01 | Entry into force of request for substantive examination |