CN201553298U - Floating platform for mooring hot airship - Google Patents
Floating platform for mooring hot airship Download PDFInfo
- Publication number
- CN201553298U CN201553298U CN2009202989037U CN200920298903U CN201553298U CN 201553298 U CN201553298 U CN 201553298U CN 2009202989037 U CN2009202989037 U CN 2009202989037U CN 200920298903 U CN200920298903 U CN 200920298903U CN 201553298 U CN201553298 U CN 201553298U
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- mooring
- utricule
- control system
- gondola
- hot air
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Abstract
The utility model relates to a floating platform for a mooring hot airship, which comprises a bag body, a hanging cabin, an anchoring vehicle, a control system, and ground equipment. The bag body is connected with the hanging cabin by a hanging rope, and a mooring rope which is connected on the intersecting point at the lower end of the hanging rope is arranged on the anchoring vehicle. The mooring rope is wound on a hydraulic winch by a guide disc. The guide disc and the hydraulic winch are fixed on the anchoring vehicle. The floating platform adopts the operating method of remote control to release a mooring hot air balloon in the sky as high as 2,000m for carrying a communication base station, and can carry out quick deployment in a certain zone so as to ensure smooth communication signals under emergency conditions. Moreover, the floating platform has the functions of monitoring and investigating, and has the advantages of simple operation as well as maintenance, low using cost, high safety, good reliability and the like.
Description
Technical field
The utility model relates to a kind of floating hollow panel, is specifically a kind ofly to be implemented in emergency communication under the major natural disasters situation, to utilize the fix a point lift-off and control the floating hollow panel of its height hot air dirigible airship of mooring hawser.
Background technology
China suffered the double blow of especially big snow disaster and Wenchuan special violent earthquake in 2008, the disaster area communication is interrupted fully, the obstructed execution and the scheduling that has had a strong impact on the disaster relief of information, reflect China and aspect emergency communication, lack actv. prediction scheme and measure, therefore, how to be implemented in the emergency communication under the major natural disasters situation, to become a urgent problem.If set up an emergent floating hollow panel during disaster, it is aerial that small-sized communication relay base station is brought to 2000m, can improve rescue efficiency greatly like this, greatly reduces people's property damage, retrieves countless life.
The measure that realizes at present emergency communication is exactly the height that communication base station is raised to requirement, and the most effective and feasible way utilizes aerostatics as floating hollow panel exactly, reaches communication base station is suspended in certain altitude carries out work.Because some characteristic of aerostatics, comparatively high-end technology is to adopt helium dirigible aerostatics to realize emergency communication at present, but its complicated operation, maintenances is loaded down with trivial details, operating costs is high, and difficulty or ease are popularized, only application in high-end military affairs investigation.As the communication calibration package, market presses for the floating hollow panel that a kind of Operation and Maintenance is simple, operating costs is cheap, so that timely communication when the disaster rescue and relief work takes place.
Summary of the invention
In order to overcome the above-mentioned deficiency of prior art, the utility model provides the mooring hot air dirigible airship that a kind of Operation and Maintenance is simple, operating costs is cheap, safe and reliable floating hollow panel.
The technical scheme that its technical matters that solves the utility model adopts comprises utricule, gondola, anchoring car, control system, wayside equipment; Utricule is connected with gondola through hanging rope, and the mooring hawser is connected on the joint of hanging rope lower end, and the mooring hawser is loaded on the anchoring car.
Said mooring hawser is wrapped on the hydraulic windlass by positioning disk, and positioning disk and hydraulic windlass are fixed on the anchoring car.
Communication base station equipment and generating set are arranged in the said gondola; Liquefied gas bottle is installed on the gondola both sides, is symmetrically distributed.
Hanging rope in said utricule both sides distribute is connected with the utricule top on the interior hanging rope, is connected with hanger down, and the booster fan of powering by the generating set on the gondola and the temperature booster by the liquefied gas bottle air feed on the gondola are installed on the hanger.
The utility model utricule is fleetline utricule and Y type tail, and aloft the utricule head facings the wind all the time, keeps the attitude of utricule basic horizontal, can keep very little resistance and very strong stability during mooring aloft.
Said control system comprises that ground control system and aerial control system and one are used to send the telecommand of ground artificial maneuvering device, receive the communication radio station of aerial platform monitor data; Ground control system comprises manual handling, display equipment; Aerial control system comprises the monitored control system that the temperature sensor, anemoscope, baroceptor, the GPS orientator that are loaded on the utricule are constituted, aerial control system also comprises the telecommand, the collection monitoring system information that receive the ground artificial maneuvering device, carries out the A/D conversion, gps data receives, and sends signal that the control burner master valve opens and closes, sends the central controller of control command to booster fan control setup, blowdown valve control setup to the burner section control circuit.
The utility model adopts the mode of utricule internal-combustion device heating to produce lift and drives hanger and gondola rising, utilize booster fan to keep intraluminal pressure, the external form that keeps fairing when making utricule work, and guaranteeing to make the resistance minimum of its generation, gondola to adopt and the utricule suspension that stands away, gondola directly is suspended on the hanging rope, mooring hawser and hanging rope direct connection, the power transmission helps alleviating the weight of gondola not by gondola, increases system performance.Ground anchoring facility speed as required discharges and recovery mooring hawser.
The utility model work mode adopts ground remote control, the situation of stronghold surface state monitoring, by central controller burner section, booster fan and blowdown valve parts are controlled, make it carry communication base station and be suspended to certain altitude aloft, change according to the size of wind-force and to add heat and guarantee to have enough surplus buoyancies, open communication base station then, task engine work provides the information communication service.
The utility model adopts the mode of remote manipulation, the mooring fire balloon is released into about 2000m aerial, is used to carry communication base station, can dispose fast in certain region, makes to guarantee that under emergency communication signal is unimpeded, and has the function of the investigation of monitoring.
The utility model with the beneficial effect that the mooring helium balloon is compared is: a) productive costs is low.The cost of producing a mooring fire balloon is 1/10th to 1/20th of a mooring helium balloon; B) use and maintenance cost is low.The each operating costs of mooring fire balloon has only some working expenseies, combustion gas expense and personal expenditures, and the mooring helium balloon of equal rank size uses once, and light helium expense is just in 1,000,000; C) material, source of the gas are unrestricted.The used textile material of fire balloon all is domestic production, and what combustion gas was used is the common petroleum blue gas, and resource can be sought everywhere, and the used material of mooring helium dirigible needs external import mostly, and helium substantially also by import, is easy to be restricted in case situation occurs; D) simple to operation, launch fast, but fast construction, lift-off fast.Mooring helium dirigible is a huge system, needs personnel many (20～30 people), setup time also very long (minimum 5 hours).And minimum needs operator 5 people of mooring fire balloon prepare and layout time the shortest need 20min, are suitable for very much quick deployment in emergency circumstances; E) system is simple, and crossing ability is good, is convenient to transportation.The mooring helium balloon needs full size vehiclees such as supporting helium car, anchoring car, generator car, control car, can only be by road transport more than 3 grades, under hazardous condition, be difficult to arrive disaster-stricken on-the-spot, and the mooring fire balloon only needs a light truck can load armamentarium, in emergency circumstances even can decompose transportation, a deeply disaster-stricken line better plays a role; F) the mooring helium balloon requires than higher personnel, need to keep the operation troop of some at ordinary times, and implement to train, could under emergency condition, play a role, and the mooring fire balloon requires very low to personnel, only need possess 2～3 core technology personnel through training, other staff need not professional training, have reduced spending at ordinary times; G) the huge spheroid of mooring helium balloon can be piled up thick and heavy accumulated snow when snowing, and can't clear up at all, therefore, snowy day, helium balloon was can not be gas filed, more can not go up to the air, and mooring fire balloon temperature height (temperature is up to 100 ℃ in the capsule), snowflake drops on the spheroid and can melt at once, can not increase utricule weight, can use, the non-icing successfully record of fire balloon safe flight in the sleet cloud is abroad arranged in the sky in slight snow.
Description of drawings
Below in conjunction with drawings and Examples the utility model is further specified.
Fig. 1 is a structural representation of the present utility model.Fig. 2 is the utility model utricule part lateral plan.Fig. 3 is the utility model gondola part-structure scheme drawing.Fig. 4 is the utility model ground anchoring facility.Fig. 5 is the utility model control system.
The specific embodiment
In Fig. 1, the utility model comprises utricule 1, gondola 3, mooring hawser 4, anchoring car 7, control system, ground handling equipment etc.Utricule 1 is connected with gondola 3 by hanging rope 2,2 one-tenth fan-shaped distributions of hanging rope, directly distance is next fixed with hanging rope 2 according to utricule 1 for distribution angle, mooring hawser 4 is received on the joint of hanging rope 2, then by positioning disk 5 be wrapped on the hydraulic windlass 6, positioning disk 5 and hydraulic windlass 6 are fixed on the anchoring car 7.Utricule 1 obtains the lift rising owing to the in-to-in temperature booster produces hot air, and hydraulic windlass 6 is by operating altitude, lift-off and the recovery speed of hawser 4 control mooring hot air dirigible airships.Adorn rotary connector between the joint of mooring hawser 4 and hanging rope 2.
Among Fig. 2,8 one-tenth fan-shaped array of interior hanging rope are distributed in the both sides (Fig. 2 is a lateral plan, the opposite side symmetry) of utricule.Be connected with the utricule top on the interior hanging rope 8, be connected with hanger 9 down, interior hanging rope 8 bears hanger 9 and goes up the booster fan 10 of installation and the weight of temperature booster 11, the weight of also bearing the exterior gondola of utricule.Booster fan 10 guarantees that by the power supply of the generating set on the gondola utricule keeps certain interior pressure, and the temperature booster 11 main heats that produce are by the liquefied gas bottle air feed on the gondola.
Among Fig. 3, pod framework 12 directly is suspended on the hanging rope 2, and mooring hawser 4 is connected on the joint of hanging rope 2, and communication base station and task device 13, pipeline system, power equipment supply, liquefied gas bottle 14 are installed on pod framework 12 inside.Liquefied gas bottle 14 be mounted to symmetrical distribution.
Among Fig. 4, ground anchoring facility comprises the hydraulic drum 6 that discharges and reclaim the mooring hawser, in order to discharge in needs and to reclaim the mooring hawser, changes operating altitude, lift-off and the recovery of mooring hot air dirigible airship.Hanging rope is through utricule, hanger, gondola, and final stress point concentrates on the mooring hawser 4.Mooring hawser 4 enters tension force releasing mechanism 15 more earlier by positioning disk 5, is wound at last on the hydraulic drum 6.Tension force releasing mechanism 15 mainly is the tension force that discharges the mutual extruding that produces when mooring hawser 4 is wrapped on the hydraulic drum 6, prevents to damage when mooring hawser 4 from twining.Positioning disk as a whole can be in the deflection of hydraulic windlass plane, all enters hydraulic windlass with horizontal direction after making hawser that any direction enters by positioning disk.7 are the anchoring car.
Figure 5 shows that the control system figure of the floating hollow panel of whole mooring hot air dirigible airship, control system comprises ground control system 16 and aerial control system 17.Ground control system 16 mainly includes artificial manipulation device, display equipment.Communication radio station sends telecommand, the reception aerial platform monitor data of wayside equipment.Aerial control system 17 comprises the monitored control system that the temperature sensor, anemoscope, baroceptor, the GPS orientator that are loaded on the utricule are constituted; Comprise and receive telecommand, collection monitoring system information, A/D conversion, gps data reception central controller.Central controller can send control signal that the control burner master valve opens and closes, send control signal (control command) to booster fan control setup and blowdown valve control setup to the burner section control circuit.Ground control system 16 sends the burner section firepower control that flying platform is handled in instruction for aerial control system 17 by communication radio station, temperature in the control capsule, the lift that keeps flying platform, simultaneously, status information to flying platform: storage pressure, generator voltage, generator oil tank oil mass, capsule head temperature, bag pressure, platform height of living in, GPS position, wind speed etc. are monitored, pass under the monitor message by communication radio station, be convenient to the ground staff and control in real time, guarantee finishing smoothly of task.
Ground handling equipment mainly provides fire balloon utricule working service necessary installations and facilities.Mainly comprise blowing engine, electrical generator, tool box, electric oil pump etc.Blowing engine is that fire balloon uses when taking off, and electrical generator provides power supply for the anchoring car.
Claims (6)
1. the floating hollow panel of mooring hot air dirigible airship is characterized in that: comprise utricule, gondola, anchoring car, control system; Utricule is connected with gondola through hanging rope, and the mooring hawser is connected on the joint of hanging rope lower end, and the mooring hawser is loaded on the anchoring car.
2. mooring hot air dirigible airship according to claim 1 floats hollow panel, it is characterized in that: said mooring hawser is wrapped on the hydraulic windlass by positioning disk, and positioning disk and hydraulic windlass are fixed on the anchoring car.
3. mooring hot air dirigible airship according to claim 1 floats hollow panel, it is characterized in that: communication base station equipment and generating set are arranged in the said gondola; Liquefied gas bottle is installed on the gondola both sides, is symmetrically distributed.
4. mooring hot air dirigible airship according to claim 1 floats hollow panel, it is characterized in that: hanging rope in both sides distribute in the said utricule, be connected with the utricule top on the interior hanging rope, and be connected with hanger down; Booster fan by the generating set on gondola power supply and the temperature booster by the liquefied gas bottle air feed on the gondola are installed on the hanger.
5. mooring hot air dirigible airship according to claim 1 floats hollow panel, it is characterized in that: utricule is fleetline utricule and Y type tail.
6. mooring hot air dirigible airship according to claim 1 floats hollow panel, it is characterized in that: said control system comprises that ground control system and aerial control system and one are used to send the telecommand of ground artificial maneuvering device, receive the communication radio station of aerial platform monitor data; Ground control system comprises manual handling, display equipment; Aerial control system comprises the monitored control system that the temperature sensor, anemoscope, baroceptor, the GPS orientator that are loaded on the utricule are constituted, aerial control system also comprises the telecommand, the collection monitoring system information that receive the ground artificial maneuvering device, carries out the A/D conversion, gps data receives, and sends signal that the control burner master valve opens and closes, sends the central controller of control command to booster fan control setup, blowdown valve control setup to the burner section control circuit.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2009202989037U CN201553298U (en) | 2009-12-12 | 2009-12-12 | Floating platform for mooring hot airship |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2009202989037U CN201553298U (en) | 2009-12-12 | 2009-12-12 | Floating platform for mooring hot airship |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN201553298U true CN201553298U (en) | 2010-08-18 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2009202989037U Expired - Lifetime CN201553298U (en) | 2009-12-12 | 2009-12-12 | Floating platform for mooring hot airship |
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Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102092471A (en) * | 2009-12-12 | 2011-06-15 | 襄樊宏伟航空器有限责任公司 | Floating platform for mooring hot air airship |
| CN102874402A (en) * | 2012-09-25 | 2013-01-16 | 襄阳宏伟航空器有限责任公司 | Airtight pressure-charged hot-gas floating platform |
| CN107682885A (en) * | 2017-07-13 | 2018-02-09 | 国网浙江省电力公司嘉兴供电公司 | A kind of LTE230 micro-base stations |
| CN109677627A (en) * | 2019-01-11 | 2019-04-26 | 苏州全波通信技术股份有限公司 | It is tethered at unmanned plane precision approach control system and method |
| CN109760817A (en) * | 2018-12-26 | 2019-05-17 | 中国电子科技集团公司第三十八研究所 | A kind of small-sized high motor driven captive balloon platform system |
-
2009
- 2009-12-12 CN CN2009202989037U patent/CN201553298U/en not_active Expired - Lifetime
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102092471A (en) * | 2009-12-12 | 2011-06-15 | 襄樊宏伟航空器有限责任公司 | Floating platform for mooring hot air airship |
| CN102092471B (en) * | 2009-12-12 | 2013-12-11 | 襄樊宏伟航空器有限责任公司 | Floating platform for mooring hot air airship |
| CN102874402A (en) * | 2012-09-25 | 2013-01-16 | 襄阳宏伟航空器有限责任公司 | Airtight pressure-charged hot-gas floating platform |
| CN102874402B (en) * | 2012-09-25 | 2015-06-03 | 襄阳宏伟航空器有限责任公司 | Airtight pressure-charged hot-gas floating platform |
| CN107682885A (en) * | 2017-07-13 | 2018-02-09 | 国网浙江省电力公司嘉兴供电公司 | A kind of LTE230 micro-base stations |
| CN107682885B (en) * | 2017-07-13 | 2020-10-20 | 国网浙江省电力公司嘉兴供电公司 | LTE230 micro base station |
| CN109760817A (en) * | 2018-12-26 | 2019-05-17 | 中国电子科技集团公司第三十八研究所 | A kind of small-sized high motor driven captive balloon platform system |
| CN109677627A (en) * | 2019-01-11 | 2019-04-26 | 苏州全波通信技术股份有限公司 | It is tethered at unmanned plane precision approach control system and method |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| AV01 | Patent right actively abandoned |
Granted publication date: 20100818 Effective date of abandoning: 20091212 |
|
| RGAV | Abandon patent right to avoid regrant |