CN202848019U - Small air floating device of unmanned operation - Google Patents
Small air floating device of unmanned operation Download PDFInfo
- Publication number
- CN202848019U CN202848019U CN 201220553001 CN201220553001U CN202848019U CN 202848019 U CN202848019 U CN 202848019U CN 201220553001 CN201220553001 CN 201220553001 CN 201220553001 U CN201220553001 U CN 201220553001U CN 202848019 U CN202848019 U CN 202848019U
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- assembly
- air
- air floating
- floating
- floating empty
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Abstract
The utility model discloses a small air floating device of unmanned operation. The small air floating device is characterized by being formed by an air floating assembly and a landing assembly which are arranged in split mode. The air floating assembly is provided with an air floating air bag and working loads. The landing assembly is provided with an air storage unit and a control unit. Under the control of the control unit, the air storage bag in the air storage unit inflates air to the air floating air bag through a stop switch, a reducing valve and a check valve timely. After inflation, the air floating assembly lifts off and the landing assembly lands, and the air floating assembly is connected with the landing assembly through ropes. The small air floating device is good in maneuverability and convenient to carry and throw and does not require manual intervention after being started by outer triggering signals to work. The small air floating device is light in weight and small in size, can be thrown to sea surfaces or mountain areas with complex terrains through various platforms fast so as to meet requirements of monitoring, communication and the like under the emergency conditions of earthquake relief work, frontier defense and counterterrorism and the like.
Description
Technical field
The utility model relates to a kind of can carrying to be thrown in and operatorless small-sized floating empty device, belongs to field of aircraft.
Background technology
The application platform of the equipment such as aerial observation, target acquisition and communication repeating that use in specific region except satellite, aircraft, also can be selected dirigible, captive balloon etc.The aircraft fuel consumption is large, airborne period short, is not suitable for continuously long-term the use; Satellite can use for a long time, but track is high, and accuracy of observation is out of reach often, and the two operating cost is all higher; Therefore, for the lasting monitoring in certain specific region and the special time period or other application that continues, dirigible or captive balloon are good selections.
Dirigible is filled with unreactable gas, such as helium, be the buoyancy lift-off that relies on unreactable gas, utilize simultaneously self-contained engine installation to overcome windage, because its wind loading rating is limited, often be subjected to the impact of meteorological conditions when using in the low latitude, when use in the high-altitude more than 10000m, owing to rarefaction of air, add the weight of power and fuel, so that the volume of dirigible must be very huge, so that cost is high; And when low-to-medium altitude was used, captive balloon was a kind of application platform that does not need the environmental protection of power, and balloon (on-load) wafts in the high-altitude, and hawser and ground by a Gent system are that loading is connected.But, captive balloon has manoevreability unlike aircraft or dirigible, need many people's operations when adding balloon inflation, if on the sea or mountain area with a varied topography use, then often inconvenient, particularly at some special occasions such as earthquake relief work or anti-terrorism, system offer the time long, speed of response is slower.
The utility model content
The utility model provides a kind of mobility strong, be easy to carry input, by the unattended small-sized floating empty device that need not manpower intervention after the external world contact give a signal startup work, it is lightweight, volume is little, can enough kinds of platform render to rapidly sea or mountain area with a varied topography, to satisfy the needs such as monitoring under the emergency conditions such as earthquake relief work, frontier defense warning and anti-terrorism, communication.
The utility model is that the technical solution problem adopts following scheme:
The constructional feature of the unattended small-sized floating empty device of the utility model is by the floating empty assembly of split setting and the module composition that lands.
The structure of described floating empty assembly is set to:
One can be filled with unreactable gas so that the floating skyborne floating air bag of empty component suspension in good time, the check valve that is provided for stoping unreactable gas to be overflowed by the inflation inlet of floating air bag at the inflation inlet of described floating air bag;
One working load is fixedly installed on the described floating air bag, is used for finishing the setting task.
Described structure setting of landing assembly comprises:
One gas storage unit, to store unreactable gas with storage tank, outlet pipe at described storage tank sets gradually the T-pipe joint that can be connected with outside inflatable appliance, the cutoff switch that can turn-off or open outlet pipe, reducing valve for reducing inflation pressure, and the appendix that connects described cutoff switch and reducing valve, the delivery port of described reducing valve is connected with described check valve by gas ducting; Described floating empty assembly is to be fixedly installed on by described gas ducting to land on the assembly;
One control unit, to respond to starter gear to receive external start signal, open cutoff switch by firer's thrust unit by time sequence control device in good time, and after opening cutoff switch, cut off gas ducting through starting firer's cutter sweep behind the time delays that sets in advance;
One reel is that the wheel carrier that winds the line is fixedly installed on and lands in the assembly, and cotton rope one end in the reel is fixed on the coiling wheel carrier, and the other end is connected on the floating empty assembly.
After system received extraneous signal and starts and automatically finish inflation, floating empty assembly go up to the air, is landed assembly and fallen earthward, and floated empty assembly and was connected assembly and connects by cotton rope.Compared with the prior art, the utility model beneficial effect is embodied in:
1, the mooring ball in the prior art, storage tank and ventilating control equipment all separate, and on the sea or mountain area with a varied topography inconvenient operation when using, also are not easy to carry and throw in; The floating empty assembly of split setting and to land assembly be to be connected by gas ducting in the utility model, compact overall structure, volume are little, lightweight, are convenient to transportation, can throw in the mountain area and use on the sea, not limited by topographic condition.
2 compare with common mooring ball, a series of processes such as inflation and control all are automatically to carry out afterwards in input in the utility model, this device is after receiving extraneous energizing signal, start-up course need not personnel operation and control, degree of automation is high, is fit to the rapidly occasion of reaction of the needs such as earthquake relief work or anti-terrorism.
Description of drawings
Fig. 1 is the utility model structured flowchart;
Fig. 1 label: 1 floating empty assembly; 2 land assembly; 11 floating air bags; 12 working loads; 13 check valves; 21 induction starter gears; 22 time sequence control devices; 23 firer's thrust units; 24 firer's cutter sweeps; 25 cutoff switches; 26 reducing valves; 27 appendixs; 28 T-pipe joints; 29 storage tanks; 31 gas ductings; 32 cotton ropes; 210 reels.
The specific embodiment
Referring to Fig. 1, the floating empty assembly 1 that unattended small-sized floating empty device is the split setting in the present embodiment and the assembly 2 that lands consist of;
As shown in Figure 1, the structure of floating empty assembly 1 is set to:
One can be filled with unreactable gas so that float the skyborne floating air bag 11 of empty assembly 1 suspension in good time, is provided for the check valve 13 that stops unreactable gas to be overflowed by the inflation inlet that floats air bag 11 at the inflation inlet that floats air bag 11;
One working load 12 is fixedly installed on the floating air bag 11, is used for finishing the setting task, and working load 12 can be signal monitoring device or Communications Relay Set etc.
As shown in Figure 1, landing the structure setting of assembly 2 comprises:
One gas storage unit, to store unreactable gas with storage tank 29, outlet pipe at storage tank 29 sets gradually the T-pipe joint 28 that can be connected with outside inflatable appliance, the cutoff switch 25 that can turn-off or open outlet pipe, reducing valve 26 for reducing inflation pressure, and the appendix 27 that connects cutoff switch 25 and reducing valve 26, the delivery port of reducing valve 26 is connected with check valve 13 by gas ducting 31, forms filling channel.Floating empty assembly 1 is to be fixedly installed on by gas ducting 31 to land on the assembly 2.
One control unit, to respond to starter gear 21 to receive external start signal, open cutoff switch 25 by time sequence control device 22 by firer's thrust unit 23, beginning is inflated to floating air bag by storage tank, after finishing inflation, start firer's cutter sweep 24 and cut off gas ducting 31, make floating empty assembly 1 and land assembly 2 and separate, floating empty assembly 1 is gone up to the air; In the implementation, time sequence control device 22 produces respectively the trigger current of igniting firer's thrust unit 23 and firer's cutter sweep 24 by the sequential of setting.
One reel 210 is that the wheel carrier that winds the line is fixedly installed on and lands in the assembly 2, and cotton rope 32 1 ends in the reel 210 are fixed on the coiling wheel carrier, and the other end is connected on the floating empty assembly 1; After floating empty assembly 1 lift-off, still be connected to by cotton rope and land assembly 2, prevent that floating empty assembly 1 from being blown away by aerial air-flow.
Working process:
The preparation process is to be inflated to storage tank 29 by the external high pressure inflatable appliance by T-pipe joint 28, can use helium, finishes this inflation port of sealing T-pipe joint 28 after the inflation.
The utility model device is transported to the sky of specifying the region by shipping platform, after the input, namely started by induction starter gear 21 by outward sign and land assembly 2 and devote oneself to work, at first be to open cutoff switch 25 by time sequence control device 22 by firer's thrust unit 23, inflated to floating air bag 11 by storage tank 29, after finishing inflation, start firer's cutter sweep 24 and cut off gas ductings 31, make floating empty assembly 1 and land assembly 2 and separate, float empty assembly 1 and gone up to the air; Land assembly 2 free fallings to ground; At this moment, cotton rope 32 keeps floating empty assembly 1 and the interconnecting between the assembly 2 of landing, and prevents that floating empty assembly 1 is blown away.
Floating empty assembly 1 lift-off is to the setting regions that is subjected to the cotton rope limitation of length, and working load 12 drops into self work.
Claims (2)
1. a unattended small-sized floating empty device is characterized in that the floating empty assembly (1) that is arranged by split and the assembly (2) that lands consist of;
The structure of described floating empty assembly (1) is set to:
The one skyborne floating air bag (11) that can in good time be filled with unreactable gas so that floating empty assembly (1) suspends, the check valve (13) that is provided for stoping unreactable gas to be overflowed by the inflation inlet of floating air bag (11) at the inflation inlet of described floating air bag (11);
One working load (12) is fixedly installed on the described floating air bag (11), is used for finishing the setting task;
Described structure setting of landing assembly (2) comprising:
One gas storage unit, to store unreactable gas with storage tank (29), outlet pipe at described storage tank (29) sets gradually the T-pipe joint (28) that can be connected with outside inflatable appliance, can turn-off or open the cutoff switch (25) of outlet pipe, reducing valve (26) for reducing inflation pressure, and the appendix (27) that connects described cutoff switch (25) and reducing valve (26), the delivery port of described reducing valve (26) is connected with described check valve (13) by gas ducting (31); Described floating empty assembly (1) is to be fixedly installed on by described gas ducting (31) to land on the assembly (2);
One control unit, to respond to starter gear (21) to receive external start signal, open cutoff switch (25) by firer's thrust unit (23) by time sequence control device (22) in good time, and opening cutoff switch (25) afterwards through starting firer's cutter sweep (24) cut-out gas ducting (31) behind the time delays that sets in advance.
2. unattended small-sized floating empty device according to claim 1, it is characterized in that a reel (210) being set described landing in the assembly, that the wheel carrier that winds the line is fixedly installed on and lands in the assembly (2), cotton rope (32) one ends in the reel (210) are fixed on the coiling wheel carrier, and the other end is connected on the floating empty assembly (1).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201220553001 CN202848019U (en) | 2012-10-26 | 2012-10-26 | Small air floating device of unmanned operation |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201220553001 CN202848019U (en) | 2012-10-26 | 2012-10-26 | Small air floating device of unmanned operation |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN202848019U true CN202848019U (en) | 2013-04-03 |
Family
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 201220553001 Expired - Fee Related CN202848019U (en) | 2012-10-26 | 2012-10-26 | Small air floating device of unmanned operation |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN202848019U (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102897310A (en) * | 2012-10-26 | 2013-01-30 | 安徽神剑鹏升科技有限公司 | Unmanned small-size floating device |
| CN103231806A (en) * | 2013-05-17 | 2013-08-07 | 上海大学 | Air droppable automatic launch mooring platform |
| CN105799908A (en) * | 2016-05-04 | 2016-07-27 | 北方民族大学 | Unmanned aerial vehicle device working on heavy load condition and control method |
| CN105857611A (en) * | 2016-05-03 | 2016-08-17 | 北方民族大学 | Unmanned aerial vehicle device capable of prolonging flight time and implementation method |
-
2012
- 2012-10-26 CN CN 201220553001 patent/CN202848019U/en not_active Expired - Fee Related
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102897310A (en) * | 2012-10-26 | 2013-01-30 | 安徽神剑鹏升科技有限公司 | Unmanned small-size floating device |
| CN102897310B (en) * | 2012-10-26 | 2015-03-25 | 安徽神剑鹏升科技有限公司 | Unmanned small-size floating device |
| CN103231806A (en) * | 2013-05-17 | 2013-08-07 | 上海大学 | Air droppable automatic launch mooring platform |
| CN105857611A (en) * | 2016-05-03 | 2016-08-17 | 北方民族大学 | Unmanned aerial vehicle device capable of prolonging flight time and implementation method |
| CN105799908A (en) * | 2016-05-04 | 2016-07-27 | 北方民族大学 | Unmanned aerial vehicle device working on heavy load condition and control method |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20130403 Termination date: 20181026 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |