CN109204769A - A kind of small-sized zero stratification of wind floating balloon launched in the air - Google Patents
A kind of small-sized zero stratification of wind floating balloon launched in the air Download PDFInfo
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- CN109204769A CN109204769A CN201811267072.7A CN201811267072A CN109204769A CN 109204769 A CN109204769 A CN 109204769A CN 201811267072 A CN201811267072 A CN 201811267072A CN 109204769 A CN109204769 A CN 109204769A
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- balloon
- master control
- air
- small
- launched
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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
- B64B1/40—Balloons
Abstract
The present invention relates to field of aircraft, and in particular to the small-sized zero stratification of wind floating balloon that one kind is launched in the air.Specifically include jettison system, jacking system, recovery system, master control system, load system, the jettison system, jacking system, recovery system, master control system and load system are sector structure, the jettison system, jacking system, recovery system, master control system and load system are drawer basket structure, multiple functional cards are provided with, multiple functional cards layers are from top to bottom sequentially connected.Floating balloon of the invention is designed exclusively for airborne ejection putting mode, have the characteristics that dispensing place is flexible, small in size, of long duration, stabilization in empty position, pose adjustment are flexible in sky, be easily recycled, it is applicable to the aircraft such as aircraft, unmanned plane and carries out ejection dispensing in the sky simultaneously, it is greatly reduced in equal volume compared to captive balloon, dirigible, it is not required to power device, is not required to ground pulling equipment.
Description
Technical field
The present invention relates to field of aircraft, and in particular to the small-sized zero stratification of wind floating balloon that one kind is launched in the air.
Background technique
Aerostatics is generally divided into dirigible, captive balloon, free balloon etc..Wherein, free balloon is generally used for orthodox flight
Device spatial altitude, unpowered device cannot achieve stable purpose in sky vulnerable to air-flow flow effect；Dirigible has power dress
It sets, windage can be overcome to a certain extent, but its power device will increase its energy consumption, so as to cause the shortening of time in sky；
Captive balloon is connected by capstan winch, hawser and ground system, has preferable wind resistance effect, but due to ground system placement
There are limitations, therefore the application environment of captive balloon is also restrained.
Summary of the invention
The technical problem to be solved in the present invention is to provide one kind to work in zero stratification of wind, does not need installation power device, drop
Low-power consumption is realized and stays empty small-sized zero stratification of wind floating balloon for a long time.
In order to solve the above-mentioned technical problem, the technical solution adopted by the present invention to solve the technical problems is:
A kind of small-sized zero stratification of wind floating balloon launched in the air, including jettison system, jacking system, recovery system, master control
System, load system, the jettison system, jacking system, recovery system, master control system and load system are fan-shaped knot
Structure, the jettison system, jacking system, recovery system, master control system and load system side are provided with PORT COM, institute
One can be formed by stating the PORT COM on jettison system, jacking system, recovery system, master control system and load system and being sequentially connected
Cylindrical structure, cylindrical structure are convenient for carrying out ejection dispensing, the jettison system, jacking system, recovery system, master in the sky
Control system and load system are arranged on pedestal；
The jettison system, jacking system, recovery system, master control system and load system are drawer basket structure, thereon
Multiple functional cards are provided with, multiple functional cards layers are from top to bottom sequentially connected.
Preferably, jettison system includes balloon utricule, air charging system, the first umbrella cabin, drag parachute cutter, first umbrella
The first drag parachute is provided in cabin, first umbrella cabin offers the umbrella outlet for the pop-up of the first drag parachute, the drag parachute
Cutter is arranged on the umbrella outlet；
The balloon utricule is arranged in balloon cabin, is provided in the balloon cabin for the inflation release of balloon utricule
Air charging system.
Preferably, the drag parachute cutter includes cutting support, and the cutting support passes through shaft and the balloon cabin
Connection is provided with torsional spring in the shaft, is provided with heater strip on the cutting support, the heater strip and the first drag parachute
Connecting rope abuts.
Preferably, the jacking system include the exhaust valve that the balloon utricule is set, multiple ballasts and for pair
The ballast clipper sheared and released.
Preferably, the ballast clipper includes cutter, and described cutter one end is provided with nut, and the nut is set in
On lead screw, the output shaft of the lead screw and motor is drivingly connected, and is provided with sawtooth, the cutter and institute on the blade of the cutter
The lanyard for stating ballast abuts.
Preferably, the recovery system includes balloon clipper, the second umbrella cabin and Radio Beacon, is opened up on the balloon cabin
There is the ball mouth for being used for ejecting balloon utricule, is provided on the ball mouth for carrying out cutting release to the balloon utricule of pop-up
Balloon clipper, be provided in second umbrella cabin and slow down the second drag parachute to fall for floating balloon.
Preferably, the balloon clipper includes Cut Block, and the inside of the ball mouth is arranged in the Cut Block, described
Be provided with shearing cylinder on Cut Block, be provided with blade on the shearing cylinder piston rod bar, be additionally provided on the ball mouth with
The grooving that the blade matches.
Preferably, the Radio Beacon use GPS, Beidou Navigation System integrated positioning, can by Beidou Navigation System to
Ground receiver personnel send specific location coordinate.
Preferably, the master control system includes master control shell, is provided with computer card, switching value on the master control shell
Board, power supply media board and battery board, the master control case top are provided with cover board, offer movable plate on the cover board,
It is provided in the movable plate and connect external-connected port with the computer card.
Preferably, the load system can be remote measuring and controlling, satellite/inertia complex navigation, environmental testing sensor, light
Learn people's one or more combination in detecting devices, communication relay set etc..
Beneficial effects of the present invention:
1, floating balloon of the invention is designed exclusively for airborne ejection putting mode, flexible, small in size with dispensing place,
In empty of long duration, in empty position stabilization, pose adjustment is flexible, be easily recycled the features such as, while it is applicable to aircraft, unmanned plane
Equal aircraft carry out ejection dispensing in the sky, greatly reduce in equal volume compared to captive balloon, dirigible, are not required to power device, are not required to
Ground pulling equipment, can rapid deployment, flexible, it is without any requirement to ground place, even if to region with a varied topography
It can be observed.
2, floating balloon works in quasi- zero stratification of wind, therefore may be implemented to drop under conditions of unpowered systems and external force traction
Low overall power consumption realizes that ultra-long time is stablized and stays sky.
3, master control system can carry out high speed processing to mass data, to jettison system, jacking system, recovery system, load
System carries out information exchange and control by communication interface, to flexibly accurately complete to fly control task.
Detailed description of the invention
Fig. 1 is the small-sized zero stratification of wind floating balloon structure schematic diagram that one kind of the invention is launched in the air.
Fig. 2 is jettison system structural schematic diagram of the invention.
Fig. 3 is balloon cabin structure schematic diagram of the invention.
Fig. 4 is master control system structural schematic diagram of the invention.
Fig. 5 is the first umbrella cabin structure schematic diagram of the invention.
Figure label explanation: 1, jettison system；11, balloon utricule；12, air charging system；13, the first umbrella cabin；14, drag parachute
Cutter；15, umbrella outlet；16, the first drag parachute；17, balloon cabin；2, jacking system；3, recovery system；31, balloon clipper；
32, Radio Beacon；4, master control system；41, master control shell；42, computer card；43, switching value board；44, power supply media board；45,
Battery board；46, cover board；47, movable plate；48, PORT COM；
Specific embodiment
The present invention will be further explained below with reference to the attached drawings and specific examples, so that those skilled in the art can be with
It more fully understands the present invention and can be practiced, but illustrated embodiment is not as a limitation of the invention.
Referring to Fig.1, shown in Fig. 2, Fig. 3, Fig. 4, Fig. 5, a kind of small-sized zero stratification of wind floating balloon launched in the air, including launch
System 1, jacking system 2, recovery system 3, master control system 4, load system, the jettison system 1, jacking system 2, recovery system
3, master control system 4 and load system are sector structure, the jettison system 1, jacking system 2, recovery system 3, master control system
System 4 and load system side are provided with PORT COM 48, the jettison system 1, jacking system 2, recovery system 3, master control
PORT COM 48 in system 4 and load system, which is sequentially connected, can form a cylindrical structure, and cylindrical structure is convenient in sky
In carry out ejection dispensing, especially suitable for airborne ejection launch specific application environment, the jettison system 1, jacking system 2,
Recovery system 3, master control system 4 and load system are arranged on pedestal；
The jettison system 1, jacking system 2, recovery system 3, master control system 4 and load system are drawer basket structure,
Multiple functional cards are provided with, multiple functional cards layers are from top to bottom sequentially connected.
The functional cards of each system using drawer cage design, muti-piece functional cards stacking place connection, can to greatest extent on
Reduce equipment volume.
Jettison system 1 include balloon utricule 11, air charging system 12, the first umbrella cabin 13, drag parachute cutter 14, described first
The first drag parachute 16 is provided in umbrella cabin 13, first umbrella cabin 13 offers the umbrella outlet for the pop-up of the first drag parachute 16
15, the drag parachute cutter 14 is arranged on the umbrella outlet 15；
The balloon utricule 11 is arranged in balloon cabin 17, is provided in the balloon cabin 17 for filling to balloon utricule 11
The air charging system 12 of gas release.
The drag parachute cutter 14 includes cutting support, and the cutting support is connected by shaft and the balloon cabin 17
It connects, torsional spring is provided in the shaft, be provided with heater strip on the cutting support, the heater strip and the first drag parachute 16
Connecting rope abuts.
The jacking system 2 includes the exhaust valve that the balloon utricule 11 is arranged in, multiple ballasts and is used for progress
The ballast clipper sheared and released, 4 communication connection of the exhaust valve, ballast clipper and master control system, when balloon utricule
When air pressure is higher in 11, master control system 4 controls exhaust valve and a certain amount of gas is discharged；When air pressure is relatively low in balloon utricule 11,
Master control system 4 controls ballast clipper and discharges a certain amount of ballast to reduce weight bearing, to reach aerostatic buoyancy and gravity
Balance.
The ballast clipper includes cutter, and described cutter one end is provided with nut, and the nut is set on lead screw,
The output shaft of the lead screw and motor is drivingly connected, and sawtooth, the cutter and the ballasting are provided on the blade of the cutter
The lanyard of object abuts.
The recovery system 3 includes balloon clipper 31, the second umbrella cabin and Radio Beacon 32, is opened up on the balloon cabin 17
There is the ball mouth for being used for ejecting balloon utricule 11, is provided on the ball mouth for being cut to the balloon utricule 11 of pop-up
The balloon clipper 31 of release is provided in second umbrella cabin and slows down the second drag parachute to fall for floating balloon, described
Radio Beacon 32 persistently carries out positioning and position coordinates is sent to surface detection equipment in real time.
Second umbrella cabin is identical with 13 structure of the first umbrella cabin.
The balloon clipper 31 includes Cut Block, and the inside of the ball mouth, the shearing is arranged in the Cut Block
Seat on be provided with shearing cylinder, be provided with blade on the shearing cylinder piston rod bar, be additionally provided on the ball mouth with it is described
The grooving that blade matches.
The Radio Beacon 32 uses GPS, Beidou Navigation System integrated positioning, can be connect to the ground by Beidou Navigation System
Receipts personnel send specific location coordinate, and searchable personnel quickly give for change, improve recovery efficiency.
The master control system 4 includes master control shell 41, is provided with computer card 42, switching value on the master control shell 41
Board 43, power supply media board 44 and battery board 45 are provided with cover board 46 at the top of the master control shell 41, open on the cover board 46
Equipped with movable plate 47, it is provided in the movable plate 47 and connect external-connected port with the computer card 42.
Computer card 42, as core chip, can fast implement complicated algorithm using DSP, and use fpga chip
Interface Expanding and Function Extension are carried out, so that high speed, steadily realization fly control function.
The load system can be remote measuring and controlling, satellite/inertia complex navigation, environmental testing sensor, optical detection
People's one or more combination in equipment, communication relay set etc..
The dispensing stage, specific step is as follows:
A, ejection guns pops up floating balloon apparatus；
B, first umbrella cabin 13 opens the first drag parachute 16 and slows down；
C, the air charging system 12 carries out fast aeration to the balloon utricule 11 and discharges balloon utricule 11 to balloon
Outside cabin 17；
D, the drag parachute cutter 14 carries out cutting release to the first drag parachute 16；
Specific step is as follows for recovery stage:
A, the balloon clipper 31 shears and releases the balloon utricule 11；
B, second umbrella cabin opens the second drag parachute and carries out deceleration whereabouts
C, the Radio Beacon 32 persistently carries out positioning and position coordinates is sent to surface detection equipment in real time
The zero stratification of wind floating balloon completes ejection in the dispensing stage, parachute-opening, unlocks, kicks off, inflates, cuts etc. and operate.
In the stage in sky, the such environmental effects such as balloon is illuminated by the light, temperature, air pressure change, between balloon interior air pressure and atmospheric pressure
Pressure difference changes, and when air pressure is higher in balloon utricule 11, a certain amount of gas is discharged main controller controls exhaust valve；Work as gas
When air pressure is relatively low in sacculus body 11, main controller controls ballast clipper discharges a certain amount of ballast to reduce weight bearing, thus
Reach the balance of aerostatic buoyancy and gravity.In recovery stage, effective load separation is completed, Radio Beacon 32 is negative in recovery system 3
Transfer destination location information is blamed, the Radio Beacon 32 uses GPS, Beidou integrated positioning, and can send specific location by Beidou
Coordinate.The relevant operation in above each stage needs a variety of environmental informations of control system quick obtaining, and can complete complexity at a high speed
Operation, therefore, the master control system 4 of the floating balloon, as core chip, can fast implement complicated algorithm using DSP, and
And Interface Expanding and Function Extension are carried out using fpga chip, so that high speed, steadily realization fly control function.
The present invention can still realize long-time stable in empty, dispensing place is flexible without power device, without cable connection
Floating balloon can be used for realizing ultra-long time monitoring in sky, investigation, data communication, scientific experiment measurement, calamity in a certain region
The purpose of evil early warning.
The floating balloon work is in quasi- zero stratification of wind of stratosphere, by air flow effect very little, therefore in unpowered device
Sky is stayed with still may be implemented to stablize in the case where external force traction.
Embodiment described above is only to absolutely prove preferred embodiment that is of the invention and being lifted, protection model of the invention
It encloses without being limited thereto.Those skilled in the art's made equivalent substitute or transformation on the basis of the present invention, in the present invention
Protection scope within.Protection scope of the present invention is subject to claims.
Claims (10)
1. the small-sized zero stratification of wind floating balloon that one kind is launched in the air, which is characterized in that including jettison system, jacking system, recycling
System, master control system, load system, the jettison system, jacking system, recovery system, master control system and load system are equal
For sector structure, the jettison system, jacking system, recovery system, master control system and load system side are provided with logical
Port is interrogated, the PORT COM on the jettison system, jacking system, recovery system, master control system and load system successively connects
A cylindrical structure can be formed by connecing, cylindrical structure convenient for carrying out ejection dispensing in the sky, the jettison system, jacking system,
Recovery system, master control system and load system are arranged on pedestal；
The jettison system, jacking system, recovery system, master control system and load system are drawer basket structure, are arranged thereon
There are multiple functional cards, multiple functional cards layers are from top to bottom sequentially connected.
2. the small-sized zero stratification of wind floating balloon launched in the air as described in claim 1, which is characterized in that jettison system includes gas
Sacculus body, air charging system, the first umbrella cabin, drag parachute cutter, are provided with the first drag parachute in first umbrella cabin, and described first
Umbrella cabin offers the umbrella outlet for the pop-up of the first drag parachute, and the drag parachute cutter is arranged on the umbrella outlet；
The balloon utricule is arranged in balloon cabin, is provided in the balloon cabin for the inflation to the inflation release of balloon utricule
Device.
3. the small-sized zero stratification of wind floating balloon launched in the air as claimed in claim 2, which is characterized in that the drag parachute cutting
Device includes cutting support, and the cutting support is connect by shaft with the balloon cabin, and torsional spring is provided in the shaft, described
Heater strip is provided on cutting support, the heater strip is abutted with the connecting rope of the first drag parachute.
4. the small-sized zero stratification of wind floating balloon launched in the air as claimed in claim 2, which is characterized in that the jacking system packet
Include the exhaust valve that the balloon utricule is set, multiple ballasts and for the ballast clipper sheared and released.
5. the small-sized zero stratification of wind floating balloon launched in the air as claimed in claim 4, which is characterized in that the ballast shearing
Device includes cutter, and described cutter one end is provided with nut, and the nut is set on lead screw, the output shaft of the lead screw and motor
It is drivingly connected, is provided with sawtooth on the blade of the cutter, the cutter is abutted with the lanyard of the ballast.
6. the small-sized zero stratification of wind floating balloon launched in the air as described in claim 1, which is characterized in that the recovery system packet
Balloon clipper, the second umbrella cabin and Radio Beacon are included, offers the ball mouth for being used for ejecting balloon utricule, institute on the balloon cabin
The balloon clipper being provided on ball mouth for carrying out cutting release to the balloon utricule of pop-up is stated, second umbrella is set in cabin
It is equipped with the second drag parachute to fall for the deceleration of floating balloon.
7. the small-sized zero stratification of wind floating balloon as claimed in claim 6 launched in the air, which is characterized in that the balloon clipper packet
Cut Block is included, the inside of the ball mouth is arranged in the Cut Block, and shearing cylinder, the shearing are provided on the Cut Block
It is provided with blade on cylinder piston rod bar, the grooving to match with the blade is additionally provided on the ball mouth.
8. the small-sized zero stratification of wind floating balloon launched in the air as claimed in claim 6, which is characterized in that the Radio Beacon uses
GPS, Beidou Navigation System integrated positioning, can by Beidou Navigation System to the ground reception staff send specific location coordinate.
9. the small-sized zero stratification of wind floating balloon launched in the air as described in claim 1, which is characterized in that the master control system packet
Master control shell is included, computer card, switching value board, power supply media board and battery board, institute are provided on the master control shell
It states master control case top and is provided with cover board, movable plate is offered on the cover board, be provided in the movable plate and the calculating
Machine board connects external-connected port.
10. the small-sized zero stratification of wind floating balloon launched in the air as described in claim 1, which is characterized in that the load system
It can be in remote measuring and controlling, satellite/inertia complex navigation, environmental testing sensor, optical detection devices, communication relay set etc.
People's one or more combination.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811267072.7A CN109204769B (en) | 2018-10-29 | 2018-10-29 | Small-size zero wind layer of aerial input floats air ball |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811267072.7A CN109204769B (en) | 2018-10-29 | 2018-10-29 | Small-size zero wind layer of aerial input floats air ball |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN109204769A true CN109204769A (en) | 2019-01-15 |
| CN109204769B CN109204769B (en) | 2020-04-21 |
Family
ID=64997492
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201811267072.7A Active CN109204769B (en) | 2018-10-29 | 2018-10-29 | Small-size zero wind layer of aerial input floats air ball |
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| Country | Link |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112540624A (en) * | 2020-12-10 | 2021-03-23 | 深圳市虹远通信有限责任公司 | Sounding balloon positioning method, system and storage medium |
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| JPH06127905A (en) * | 1991-09-05 | 1994-05-10 | Tatsuo Yoshiyasu | Ozone layer restoring device |
| 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 |
| US9174738B1 (en) * | 2013-04-14 | 2015-11-03 | Google Inc. | Drag disk, small |
| CN206476087U (en) * | 2017-01-10 | 2017-09-08 | 湖南航天远望科技有限公司 | One kind is tethered at floating balloon platform |
| CN108284937A (en) * | 2017-01-10 | 2018-07-17 | 湖南航天远望科技有限公司 | One kind being tethered at floating balloon platform |
| CN108298093A (en) * | 2018-01-26 | 2018-07-20 | 大连理工大学 | Parachute rope draw off gear |
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2018
- 2018-10-29 CN CN201811267072.7A patent/CN109204769B/en active Active
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH06127905A (en) * | 1991-09-05 | 1994-05-10 | Tatsuo Yoshiyasu | Ozone layer restoring device |
| US9174738B1 (en) * | 2013-04-14 | 2015-11-03 | Google Inc. | Drag disk, small |
| 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 |
| CN206476087U (en) * | 2017-01-10 | 2017-09-08 | 湖南航天远望科技有限公司 | One kind is tethered at floating balloon platform |
| CN108284937A (en) * | 2017-01-10 | 2018-07-17 | 湖南航天远望科技有限公司 | One kind being tethered at floating balloon platform |
| CN108298093A (en) * | 2018-01-26 | 2018-07-20 | 大连理工大学 | Parachute rope draw off gear |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112540624A (en) * | 2020-12-10 | 2021-03-23 | 深圳市虹远通信有限责任公司 | Sounding balloon positioning method, system and storage medium |
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|---|---|
| CN109204769B (en) | 2020-04-21 |
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