CN107054610A - The scheme of kite balloon airship in sky when a kind of long - Google Patents
The scheme of kite balloon airship in sky when a kind of long Download PDFInfo
- Publication number
- CN107054610A CN107054610A CN201710401339.6A CN201710401339A CN107054610A CN 107054610 A CN107054610 A CN 107054610A CN 201710401339 A CN201710401339 A CN 201710401339A CN 107054610 A CN107054610 A CN 107054610A
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- Prior art keywords
- kite balloon
- balloon airship
- hull
- gondola
- scheme
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64B—LIGHTER-THAN AIR AIRCRAFT
- B64B1/00—Lighter-than-air aircraft
- B64B1/06—Rigid airships; Semi-rigid airships
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64B—LIGHTER-THAN AIR AIRCRAFT
- B64B1/00—Lighter-than-air aircraft
- B64B1/66—Mooring attachments
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- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
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Abstract
The invention provides it is a kind of long when the scheme of kite balloon airship in sky, solar battery array and energy-storage battery are carried by dirigible, pass through effective energy management, the endlessly energy can be provided for the load carried, improve the self-supplying capacity of kite balloon airship, for kite balloon airship it is long when work in sky provide the necessary technical guarantee, it can be up to the several months between staying space-time.By the way that each system integration of kite balloon airship is met in highway and air transport requirement shelter to one, it is possible to achieve the rapid transport deployment of kite balloon airship.
Description
Technical field
The present invention relates to vehicle technology field, it is more particularly to a kind of when can be long in empty pending flight device.
Background technology
With scientific and technological progress and the development of military modernization, carry associated load progress air-borne early warning using aerial platform and detect
Look into, telecommunications guarantee, remote sensing mapping, the condition of a disaster monitoring etc. task be widely used, aerial platform provide it is wide
Observation visual angle and covering power, with more preferable survival ability and ability to communicate.Conventional aerial platform include satellite, aircraft,
Aerostatics etc., satellite and aircraft due to involving great expense, can effectively using the time it is short the shortcomings of, limit application.Now may be used
To give full play to the advantage of aerostatics, for it is long when lasting aerial observation, communication relaying etc..Aerostatics, which belongs to, is lighter than air
Airborne vehicle, according to the difference of operation principle, aerostatics can be divided into dirigible, captive balloon and fire balloon etc..
Conventional mooring system includes aircraft, compound heaving pile and ground installation, heaving pile connection aircraft and ground installation,
Because pending flight device uses surface power supply, so existing power transmission cable has the communications cable in compound heaving pile again.Although this is tethered at
System can extend the hang time of aircraft, but compound heaving pile turns into the heavy burden of aircraft, with the lifting of flying height,
Hawser weight is accordingly lifted, and the flying height of serious restriction aircraft, flight range is also limited, and flight heavy burden load is also limited.
Kite balloon airship provides buoyancy using the gas of air is lighter than, it is meant that dirigible does not simultaneously need extra power to tie up
Flying height is held, how to solve to carry load and power to turn into the key issue of influence kite balloon airship hang time.
The content of the invention
The scheme of kite balloon airship in sky when the present invention proposes a kind of long, solar battery array and energy storage are carried by dirigible
Battery, by effective energy management, can provide the endlessly energy so that the self-supplying capacity of kite balloon airship to carry load
Effectively improve, be that work in sky provides the necessary technical guarantee when kite balloon airship is long, it can be up to the several months between staying space-time.
The present invention uses following any technical scheme.
The scheme of kite balloon airship in sky when a kind of long, including hull, drag-line, gondola, ground anchor system and earth station
According to any of the above-described technical scheme, it is characterised in that described hull profile is lower resistance ship shape, can be effective
Kite balloon airship wind loading rating is improved, is made using high-strength light hull material so that hull can obtain higher superpressure performance
With relatively low slip, be conducive to maintaining hull shape, keep dirigible buoyancy.
According to any of the above-described technical scheme, it is characterised in that described hull top or head possess one or more valves
Door gear, for bleed air operation in emergency circumstances, hull bottom, head or side possess one or more charge/discharge gas
Mouthful, for letting fly away before charge operation and gas reclaimer operation.
According to any of the above-described technical scheme, it is characterised in that described hull rear portion is empennage, for increasing kite balloon airship
Transverse direction and directional static stability, it is ensured that carry load being capable of steady operation.
According to any of the above-described technical scheme, it is characterised in that described drag-line, including boundling on hull draws in the net and even
Connect the mooring guy of gondola and ground anchor system.
According to any of the above-described technical scheme, it is characterised in that described boundling draws in the net for the buoyancy of hull to be converged at
A bit, it is connected by rotatable device with gondola, buoyancy is transferred to gondola.
According to any of the above-described technical scheme, it is characterised in that described gondola bottom passes through rotatable device and mooring guy
Connection, designated flying zone is anchored at by dirigible and gondola.
According to any of the above-described technical scheme, it is characterised in that described rotatable device can ensure hull or gondola
Boundling will not be made to draw in the net and mooring guy knotting when wind-engaging rotates.
According to any of the above-described technical scheme, it is characterised in that described gondola includes bird shell, gondola frame and load.
According to any of the above-described technical scheme, it is characterised in that described bird shell is streamlined shell, by whole gondola knot
Structure is wrapped up, the overall frontal resistance of reduction gondola.
According to any of the above-described technical scheme, it is characterised in that described gondola frame draws in the net and mooring guy for connecting boundling,
General design is taken, structural support can be provided for different mission payloads.
According to any of the above-described technical scheme, it is characterised in that described load include hull information gathering and control system,
Communication transmission system, energy resource system and mission payload, mission payload are required according to different task, can be set for emergency communication
Standby, earth observation equipment or early warning radar etc..
According to any of the above-described technical scheme, it is characterised in that the quantity of described solar battery array, according to task need
Arrangement is sought, is received in when letting fly away in gondola, to specifying after degree in outage, is stretched out by motion outside gondola, it is ensured that carry load
Energy resource supply.
According to any of the above-described technical scheme, it is characterised in that described ground anchor system, include shelter, mooring mast,
Aerating device, gas storage and retracting device, wrap-up and counterweight.
According to any of the above-described technical scheme, it is characterised in that the integrated particular design of described shelter, put for storing
Hull and drag-line before flying etc., and the other equipment of ground anchor system is integrated with, shelter meets highway and air transport requirement,
It is easy to transhipment to dispose.
According to any of the above-described technical scheme, it is characterised in that described mooring mast is Collapsible structure, is placed in shelter
Portion, when kite balloon airship is let fly away, mooring mast can be holded up, for fixing kite balloon airship.
According to any of the above-described technical scheme, it is characterised in that described aerating device can be integrated on mooring mast, be used for
Give kite balloon airship inflation.
According to any of the above-described technical scheme, it is characterised in that described gas storage and retracting device are located inside shelter,
For storing and reclaiming helium.
According to any of the above-described technical scheme, it is characterised in that described wrap-up is located inside shelter, for letting fly away and
Hull is reclaimed, and controls the resident height of kite balloon airship.
According to any of the above-described technical scheme, it is characterised in that described counterweight provides additional weight for anchor system, improve
The stability of anchor system, counterweight can be the fixed weight carried with shelter, or let fly away scene supplement water,
The interim counterweight such as sandstone or soil.
According to any of the above-described technical scheme, it is characterised in that described earth station, including communication apparatus, display device and
Control device etc..The communication that communication apparatus is used between equipment compartment, transmission hull relevant information and mission payload data, and
Show, and kite balloon airship and mission payload are controlled on display device according to mission requirements.
The solution have the advantages that：
1st, by choosing lower resistance ship shape, and made using high-strength light hull material so that hull can obtain higher
Superpressure performance and relatively low slip, it is ensured that in empty ability when kite balloon airship possesses long, while being conducive to keeping buoyancy, carry
High wind loading rating；
2nd, by carrying solar battery array, the energy constantly for needed for being provided dirigible meets energy circulation requirement, it is ensured that
Mission payload can non-stop run, the energy-storage battery of carrying remains to maintain to carry in the case of no supplement of solar energy in the daytime
Lotus operation for several days is to tens of days so that the ability of work in sky when this kite balloon airship possesses long.；
3rd, by the General design of gondola, effective guarantee can be provided for different mission requirements, and pass through gondola
Quick-replaceable, completes rapid switching of the kite balloon airship between different task pattern.
4th, by the integrated design of shelter, whole system can be integrated into a shelter, can be in accident
And disaster comes interim, is transported by automobile or aircraft, realizes convenient transport and the rapid deployment of kite balloon airship.
5th, the real-time monitoring to emphasis, hot zones can be realized by the expansion of Wireless remote control kite balloon airship.
Brief description of the drawings
The present invention is described in further detail with reference to the accompanying drawings and detailed description.
Fig. 1 represents the schematic diagram in empty kite balloon airship scheme when the present invention is a kind of long；
Fig. 2 represents the positive schematic diagram in empty kite balloon airship scheme when the present invention is a kind of long；
Fig. 3 represents the detailed maps of gondola of the present invention；
Fig. 4 represents the detailed maps of ground anchor system of the present invention；
Fig. 5 represents highway transportation schematic diagram of the present invention；
Fig. 6 represents air transport schematic diagram of the present invention；
In figure：1st, hull, 2, drag-line, 3, gondola, 4, ground anchor system, 5, haulage truck；
11st, discharge charge gas port, 12, valving, 13, empennage；
21st, boundling draws in the net, and 22, rotatable device, 23, mooring guy；
31st, including bird shell, 32, gondola frame, 33, load, 34, solar battery array；
41st, shelter, 42, mooring mast, 43, aerating device, 44, gas storage and retracting device, 45, wrap-up, 46, match somebody with somebody
Weight.
Embodiment
The present invention will be described below in conjunction with the accompanying drawings, and described preferred embodiment is merely to illustrate and explained this hair
It is bright, it is not intended to limit the present invention.
As Figure 1-Figure 4, the scheme of kite balloon airship in sky when a kind of long, including hull 1, drag-line 2, gondola 3, ground anchoring
System 4 and earth station.
The monnolithic case of above-mentioned hull 1 is promotion low-resistance ship shape, can improve kite balloon airship wind loading rating, hull 1 is adopted
Made of Lightweight high-strength composite material, higher superpressure performance and relatively low slip can be obtained, be conducive to maintaining hull shape
Shape, holding dirigible buoyancy, and reduce the adverse effect to load.
Above-mentioned discharge charge gas port 11 be located at hull 1 bottom, head or side, for letting fly away before charge operation with
And gas reclaimer operation.
Above-mentioned valving 12 is located at the top or head of hull 1, can be realized in emergency circumstances by ground control
Bleed air operation.
Above-mentioned empennage 13 is located at hull rear portion, can increase the transverse direction and directional static stability of kite balloon airship, it is ensured that take
Band load being capable of steady operation.
The boundling that above-mentioned drag-line 2 is included on hull draws in the net 21 and mooring guy 23.
Above-mentioned boundling draws in the net 21 for the buoyancy of hull 1 to be converged at a bit, passes through rotatable device 22 and gondola 3
Connection, gondola 3 is transferred to by buoyancy.
The bottom of above-mentioned gondola 3 is connected by rotatable device 22 with mooring guy 23, and hull 1 is anchored at gondola 3
Designated flying zone.
Above-mentioned rotatable device 22, by the particular design of itself, the rotary motion for connecting two ends is separated, can be with
Ensure wind-engaging rotate when will not make boundling draw in the net 21 and mooring guy 23 knot.
Above-mentioned gondola 3 includes bird shell 31, gondola frame 32 and load 33.Bird shell 31 is streamlined shell, will be whole
The encapsulated by structures of gondola 3 is got up, the overall frontal resistance of reduction, reduces the disturbance to Portable device.
Above-mentioned gondola frame 32, which is used to connecting boundling, draws in the net 21 and mooring guy 23, by taking General design, Ke Yiwei
Different mission payloads provides structural support, gondola is possessed interchangeability.
Above-mentioned load 33 includes hull information gathering and control system, communication transmission system, energy resource system and task
Load, mission payload is required according to different task, can be emergency communication equipment, earth observation equipment or early warning radar etc.
The quantity of above-mentioned solar battery array 34, is arranged according to the difference of mission payload, solar energy when letting fly away
Array 34 is received in gondola 3, to specify degree in outage after, by motion stretching gondola 3 outside, daytime solar cell
Array 34 absorbs solar energy, maintains the energy resource supply in the daytime of load 33, and by unnecessary energy storage into energy-storage battery, it is ensured that
The night energy resource supply of load 33.Energy-storage battery remains to maintain load 33 to work in the case of no supplement of solar energy in the daytime
A few days to tens of days.
Above-mentioned ground anchor system 4 includes shelter 41, mooring mast 42, aerating device 43, gas storage and reclaims dress
Put 44, wrap-up 45 and counterweight 46.
The above-mentioned integrated particular design of shelter 41, for storing hull 1 and drag-line 2 before letting fly away etc., and is integrated with
The other equipment of ground anchor system 4, makes whole kite balloon airship to be integrated within a shelter 41.Shelter 41 meets highway
With air transport requirement, it is easy to transhipment to dispose, as shown in figure 1, whole system can realize the motor-driven of dirigible by haulage truck 5
Deployment.
Above-mentioned mooring mast 42 is Collapsible structure, is placed in inside shelter 41, when kite balloon airship is let fly away, and mooring mast 42 is erected
Rise, for fixing kite balloon airship.
Above-mentioned aerating device 43 can be integrated on mooring mast 42, for being inflated to kite balloon airship.
Above-mentioned gas storage and retracting device 44 are located inside shelter 41, for storing and reclaiming helium.
Above-mentioned wrap-up 45 is located inside shelter 41, for letting and reclaiming hull 1 fly away, and controls staying for kite balloon airship
Stay height.
Above-mentioned counterweight 46 is that ground anchor system 4 provides additional weight, improves the stability of ground anchor system 4, matches somebody with somebody
It can be the fixed weight carried with shelter 41 to weigh 46, or let water, sandstone or soil of scene supplement etc. fly away
Interim counterweight.
Above-mentioned earth station includes communication apparatus, display device and control device etc..Communication apparatus be used for equipment compartment it
Between communication, transmission hull relevant information and mission payload data, and showing on the display device, and according to mission requirements to being
Dirigible and mission payload is stayed to be controlled.Described earth station can be integrated in ground anchor system 4, can also pass through channel radio
News means, remote control is carried out by the smart machine that can be networked.
Claims (11)
1. the scheme of kite balloon airship in sky when a kind of long, including hull 1, drag-line 2, gondola 3, ground anchor system 4 and earth station.
2. the scheme of kite balloon airship in sky when as claimed in claim 1 a kind of long, it is characterised in that the entirety of described hull 1
Profile is lower resistance ship shape, can improve kite balloon airship wind loading rating, and hull 1 is made using Lightweight high-strength composite material, can be with
Obtain higher superpressure performance and relatively low slip.
3. the scheme of kite balloon airship in sky when as claimed in claim 2 a kind of long, it is characterised in that described discharge charge gas port 11
Positioned at the bottom, head or side of hull 1, for letting fly away before charge operation and gas reclaimer operation.Described valve
Device 12 is located at the top or head of hull 1, can realize bleed air operation in emergency circumstances by ground control.Described
Empennage 13 is located at hull rear portion, can increase the transverse direction and directional static stability of kite balloon airship.
4. the scheme of kite balloon airship in sky when as claimed in claim 1 a kind of long, it is characterised in that described drag-line 2 includes ship
Boundling on body draws in the net 21 and mooring guy 23.
5. the scheme of kite balloon airship in sky when as claimed in claim 4 a kind of long, it is characterised in that described boundling draws in the net 21 use
Converged at a bit in by the buoyancy of hull 1, by the connection of rotatable device 22 and gondola 3, buoyancy is transferred to gondola 3.Hang
The bottom in cabin 3 is connected by rotatable device 22 with mooring guy 23, and hull 1 and gondola 3 are anchored at into designated flying zone.Described can
Rotating device 22, by the particular design of itself, can separate the rotary motion for connecting two ends, it is ensured that when wind-engaging rotates
Will not make boundling draw in the net 21 and mooring guy 23 knot.
6. the scheme of kite balloon airship in sky when as claimed in claim 1 a kind of long, it is characterised in that described gondola 3 includes hanging
Cabin shell 31, gondola frame 32 and load 33.
7. the scheme of kite balloon airship in sky when as claimed in claim 6 a kind of long, it is characterised in that described bird shell 31 is stream
Line style housing, the whole encapsulated by structures of gondola 3 is got up, the overall frontal resistance of reduction gondola.Described gondola frame 32 is used to connect
Boundling draws in the net 21 and mooring guy 23, by taking General design, can provide structural support for different mission payloads, make to hang
Cabin possesses interchangeability.Described load 33 include hull information gathering and control system, communication transmission system, energy resource system and
Mission payload, mission payload is required according to different task, can be emergency communication equipment, earth observation equipment or early warning radar
Deng.
8. the scheme of kite balloon airship in sky when as claimed in claim 7 a kind of long, it is characterised in that described solar array
The quantity of row 34, is arranged according to the difference of mission payload, and solar battery array 34 is received in gondola 3 when letting fly away, to finger
Surely after degree in outage, stretched out by motion outside gondola 3, daytime, solar battery array 34 absorbed solar energy, maintained load
33 energy resource supply in the daytime, and by unnecessary energy storage into energy-storage battery, it is ensured that the night energy resource supply of load 33.Energy storage
Battery remains to maintain the operation for several days of load 33 to tens of days in the case of no supplement of solar energy in the daytime.
9. the scheme of kite balloon airship in sky when as claimed in claim 1 a kind of long, it is characterised in that described ground anchor system
4 include shelter 41, mooring mast 42, aerating device 43, gas storage and retracting device 44, wrap-up 45 and counterweight 46.
10. ground anchor system 4 as claimed in claim 9, it is characterised in that described shelter 41 is integrated special to be set
Meter, for storing hull 1 and drag-line 2 before letting fly away etc., and is integrated with the other equipment of ground anchor system 4, makes entirely to be tethered at
Dirigible can be integrated within a shelter 41.Shelter 41 meets highway and air transport requirement, is easy to transhipment to dispose, whole system
System can realize the Flexible deployment of dirigible by haulage truck 5.Described mooring mast 42 is Collapsible structure, is placed in shelter 41
Portion, when kite balloon airship is let fly away, mooring mast 42 is holded up, for fixing kite balloon airship.Described aerating device 43, which can be integrated in, is
Stay on tower 42, for being inflated to kite balloon airship.Described gas storage and retracting device 44 are located inside shelter 41, for storing
With recovery helium.Described wrap-up 45 is located inside shelter 41, for letting and reclaiming hull 1 fly away, and controls kite balloon airship
Resident height.Described counterweight 46 is that ground anchor system 4 provides additional weight, improves the stability of ground anchor system 4,
Counterweight 46 can be the fixed weight carried with shelter 41 or water, sandstone or the soil of letting scene supplement fly away
Etc. interim counterweight.
11. the scheme of kite balloon airship in sky when as claimed in claim 1 a kind of long, it is characterised in that described earth station includes
Communication apparatus, display device and control device etc..The communication that described communication apparatus is used between equipment compartment, transmits hull phase
Information and mission payload data are closed, and are shown on the display device, and kite balloon airship and mission payload are entered according to mission requirements
Row control.Described earth station can be integrated in ground anchor system 4, also can be by wireless telecommunications means, by that can network
Smart machine carry out remote control.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710401339.6A CN107054610A (en) | 2017-06-01 | 2017-06-01 | The scheme of kite balloon airship in sky when a kind of long |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710401339.6A CN107054610A (en) | 2017-06-01 | 2017-06-01 | The scheme of kite balloon airship in sky when a kind of long |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN107054610A true CN107054610A (en) | 2017-08-18 |
Family
ID=59616145
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710401339.6A Pending CN107054610A (en) | 2017-06-01 | 2017-06-01 | The scheme of kite balloon airship in sky when a kind of long |
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Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107628222A (en) * | 2017-08-23 | 2018-01-26 | 中国人民解放军63653部队 | A kind of method that Large Airship is let fly away using the transhipment of integral truss-like device |
| CN107697263A (en) * | 2017-08-23 | 2018-02-16 | 中国人民解放军63653部队 | Platform is let in a kind of Large Airship transhipment fly away |
| CN108860557A (en) * | 2018-06-08 | 2018-11-23 | 重庆交通职业学院 | The work system of more unmanned hot air dirigible airships of rotor |
| CN109515678A (en) * | 2018-10-17 | 2019-03-26 | 中国特种飞行器研究所 | Platform and method of deploying is unfolded in the small-sized automatic fast aeration of spindle spheric captive balloon |
| CN112078775A (en) * | 2019-06-14 | 2020-12-15 | 天津天航智远科技有限公司 | Unmanned aerial vehicle logistics system taking carrying airship as center |
| CN114325876A (en) * | 2021-12-22 | 2022-04-12 | 四创电子股份有限公司 | Multifunctional aerostat weather guarantee equipment |
-
2017
- 2017-06-01 CN CN201710401339.6A patent/CN107054610A/en active Pending
Cited By (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107628222A (en) * | 2017-08-23 | 2018-01-26 | 中国人民解放军63653部队 | A kind of method that Large Airship is let fly away using the transhipment of integral truss-like device |
| CN107697263A (en) * | 2017-08-23 | 2018-02-16 | 中国人民解放军63653部队 | Platform is let in a kind of Large Airship transhipment fly away |
| CN107628222B (en) * | 2017-08-23 | 2020-04-24 | 中国人民解放军63653部队 | Method for transferring and flying large airship by adopting integrated truss type device |
| CN107697263B (en) * | 2017-08-23 | 2020-07-07 | 中国人民解放军63653部队 | Large airship transferring and flying platform |
| CN108860557A (en) * | 2018-06-08 | 2018-11-23 | 重庆交通职业学院 | The work system of more unmanned hot air dirigible airships of rotor |
| CN109515678A (en) * | 2018-10-17 | 2019-03-26 | 中国特种飞行器研究所 | Platform and method of deploying is unfolded in the small-sized automatic fast aeration of spindle spheric captive balloon |
| CN109515678B (en) * | 2018-10-17 | 2022-04-19 | 中国特种飞行器研究所 | Automatic quick inflation and deployment platform and deployment method for small spindle-shaped captive balloon |
| CN112078775A (en) * | 2019-06-14 | 2020-12-15 | 天津天航智远科技有限公司 | Unmanned aerial vehicle logistics system taking carrying airship as center |
| CN114325876A (en) * | 2021-12-22 | 2022-04-12 | 四创电子股份有限公司 | Multifunctional aerostat weather guarantee equipment |
| CN114325876B (en) * | 2021-12-22 | 2024-04-26 | 四创电子股份有限公司 | Multifunctional aerostat weather protection equipment |
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Application publication date: 20170818 |
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