CN104670480A - Electric power routing inspection unmanned plane undercarriage - Google Patents
Electric power routing inspection unmanned plane undercarriage Download PDFInfo
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- CN104670480A CN104670480A CN201310606534.4A CN201310606534A CN104670480A CN 104670480 A CN104670480 A CN 104670480A CN 201310606534 A CN201310606534 A CN 201310606534A CN 104670480 A CN104670480 A CN 104670480A
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- gas
- unmanned plane
- alighting gear
- unmanned machine
- patrol unmanned
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Abstract
The invention discloses an electric power routing inspection unmanned plane undercarriage including a undercarriage body, and is characterized in that a buffer gas bag system is fixed in the undercarriage body and includes an inflatable gas bag in a vacuum state; the inflatable gas bag is internally provided with a micro gas bottle device which can release a large amount of gas to make the inflatable gas bag filled with the gas when an electric power routing inspection unmanned plane is crashed. The electric power routing inspection unmanned plane undercarriage has the beneficial effects that when the unmanned plane is crashed, the micro gas bottle device can instantly rapidly release the compressed gas, so as to make the inflatable gas bag originally in the vacuum state popped out and filled with the gas in short a few seconds, original crashing hard landing is changed into soft landing, and the unmanned plane and a loading device thereof are effectively protected.
Description
Technical field
The present invention relates to unmanned plane field, particularly the power patrol unmanned machine alighting gear of one.
Background technology
In recent years, the sustained and rapid development of Chinese national economy proposes more and more higher requirement to China's power industry.China has formed North China, northeast, East China, Central China, northwest and south electric network totally 6 transprovincially district's electrical networks at present, by more than the 110 kilovolts transmission lines of electricity in the whole nation in 2012 more than 700,000 kilometers.At present, the domestic people's of having helicopter and unmanned plane Power Line Inspection System grow up gradually, and wherein manned helicopter routing inspection also exists some problems: as expensive in helicopter and maintenance cost thereof, safety problem is outstanding.
It is flexible that unmanned plane has landing, and the plurality of advantages such as can freely to hover, has huge development prospect.But at present, power patrol unmanned machine performs and patrols and examines in process carrying task device, if there is unexpected air crash, unmanned plane can only be cushioned by the alighting gear hard landing of below, final result often machine is ruined equipment and is died, and causes serious consequence.
Summary of the invention
For the problems referred to above, the object of the present invention is to provide a kind of unmanned plane when there is unexpected air crash, the power patrol unmanned machine alighting gear of device damage that effectively can prevent unmanned plane and carry.
For achieving the above object, technical scheme proposed by the invention is: a kind of power patrol unmanned machine alighting gear, comprise alighting gear body, it is characterized in that: described alighting gear body internal fixtion has buffer air bag system, described buffer air bag system comprises the inflatable airbag that is in vacuum state, be provided with one in described inflatable airbag when power patrol unmanned machine falls, a large amount of gas can be discharged and make the gassiness miniature gas bottle device of inflatable airbag.
Preferably, in described miniature gas bottle device, be filled with pressure gas, be provided with one in miniature gas bottle device when patrol unmanned machine falls, the gas cylinder lancing device that miniature gas bottle device discharges gas can be punctured.
Further, described gas cylinder lancing device comprises 2 irony punctures nail, power supply, remote switchs, fixed by bracing wire between the head of a nail of 2 described irony puncture nails, and between the head of a nail, be provided with the spring being in tensioned state, coil is wound with between two described irony puncture nails, described coil is connected with power supply, remote switch, and described remote switch is connected with the long-range microcontroller of unmanned plane.
Preferably, described pressure gas is carbon dioxide.
Adopt technique scheme; power patrol unmanned machine alighting gear of the present invention; the beneficial effect had is; when the moment that unmanned plane falls; miniature gas bottle device can discharge rapidly the gas of compression moment; originally the inflatable airbag being in vacuum state is ejected within of short duration several seconds and aerification, become soft landing from the hard landing of original air crash, actv. protects unmanned plane and load equipment thereof.
Accompanying drawing explanation
Fig. 1 is power patrol unmanned machine landing gear structure schematic diagram of the present invention;
Fig. 2 is described buffer air bag system architecture schematic diagram;
Fig. 3 is described miniature gas bottle device structural representation;
Fig. 4 is described gas cylinder lancing device structural representation;
Fig. 5 is irony puncture nail effect schematic diagram after described wire breakage;
Fig. 6 is power patrol unmanned machine alighting gear buffer air bag system aerification schematic diagram.
Detailed description of the invention
Below in conjunction with the drawings and specific embodiments, the present invention will be further described.
As shown in Figure 1 and Figure 2, power patrol unmanned machine alighting gear, comprise alighting gear body 1, buffer air bag system 2 is fixed with by anchor fitting 11 in alighting gear body 1, buffer air bag system 2 comprises the inflatable airbag 21 that is in vacuum state, be provided with one in inflatable airbag 21 when power patrol unmanned machine falls, a large amount of gas can be discharged and make the gassiness miniature gas bottle device 20 of inflatable airbag.
As optimal way of the present invention, as shown in Figure 3, pressure gas 201 is filled with, as carbon dioxide in miniature gas bottle device 20; Be provided with one in miniature gas bottle device 20 when patrol unmanned machine falls, the gas cylinder lancing device 3 that miniature gas bottle device 20 discharges gas can be punctured.Preferably, as shown in Figure 4, gas cylinder lancing device 3 comprises the first puncture of irony puncture nail 31, second irony nail 32, power supply 35, remote switch 36, fixed by bracing wire 33 between the head of a nail of the first irony puncture nail 31, second irony puncture nail 32, and between the head of a nail, be provided with the spring 34 being in tensioned state, coil 37 is wound with between the first irony puncture nail 31, second irony puncture nail 32, coil 37 is connected with power supply 35, remote switch 36, and described remote switch 36 is connected with the long-range microcontroller of unmanned plane.
During concrete use, when the moment that unmanned plane falls, unmanned plane sends a signal to remote switch 36 by long-range microcontroller, Circuits System switch in buffer air bag system 2 is closed, electric current is by being wrapped in the coil 37 on the first irony puncture nail 31, second irony puncture nail 32, make puncture nail become a N-S pole magnet, two magnets are with being respectively N-S, S-N.Therefore lasting pulling force can be produced, and under the combined action of spring 34 elastic force of tensioned state, break being fixed on the bracing wire 33 nailed on of puncturing, add the elastic force of the spring 34 tightened, puncture is allowed to follow closely the broken miniature gas bottle device 20(of puncture as shown in Figure 5), miniature gas bottle device 20 discharges rapidly the CO of compression instantaneously
2gas, makes the inflatable airbag being originally in vacuum packed eject within of short duration several seconds and be full of CO
2gas (as shown in Figure 6), and then become soft landing from the hard landing of original air crash, actv. protects unmanned plane and load equipment thereof.
Although specifically show in conjunction with preferred embodiment and describe the present invention; but those skilled in the art should be understood that; not departing from the spirit and scope of the present invention that appended claims limits; in the form and details the present invention is made a variety of changes, be protection scope of the present invention.
Claims (4)
1. a power patrol unmanned machine alighting gear, comprise alighting gear body, it is characterized in that: described alighting gear body internal fixtion has buffer air bag system, described buffer air bag system comprises the inflatable airbag that is in vacuum state, be provided with one in described inflatable airbag when power patrol unmanned machine falls, a large amount of gas can be discharged and make the gassiness miniature gas bottle device of inflatable airbag.
2. the power patrol unmanned machine alighting gear of one according to claim 1, it is characterized in that: in described miniature gas bottle device, be filled with pressure gas, be provided with one in miniature gas bottle device when patrol unmanned machine falls, the gas cylinder lancing device that miniature gas bottle device discharges gas can be punctured.
3. the power patrol unmanned machine alighting gear of one according to claim 2, it is characterized in that: described gas cylinder lancing device comprises 2 irony punctures nail, power supply, remote switchs, fixed by bracing wire between the head of a nail of 2 described irony puncture nails, and between the head of a nail, be provided with the spring being in tensioned state, coil is wound with between two described irony puncture nails, described coil is connected with power supply, remote switch, and described remote switch is connected with the long-range microcontroller of unmanned plane.
4. the power patrol unmanned machine alighting gear of one according to claim 1, is characterized in that: described pressure gas is carbon dioxide.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201310606534.4A CN104670480A (en) | 2013-11-27 | 2013-11-27 | Electric power routing inspection unmanned plane undercarriage |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201310606534.4A CN104670480A (en) | 2013-11-27 | 2013-11-27 | Electric power routing inspection unmanned plane undercarriage |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN104670480A true CN104670480A (en) | 2015-06-03 |
Family
ID=53306192
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201310606534.4A Pending CN104670480A (en) | 2013-11-27 | 2013-11-27 | Electric power routing inspection unmanned plane undercarriage |
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| Country | Link |
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| CN (1) | CN104670480A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114537687A (en) * | 2022-04-27 | 2022-05-27 | 济南市勘察测绘研究院 | Geographic information survey and drawing unmanned aerial vehicle equipment |
| US11368002B2 (en) | 2016-11-22 | 2022-06-21 | Hydro-Quebec | Unmanned aerial vehicle for monitoring an electrical line |
| US12097956B2 (en) | 2021-04-30 | 2024-09-24 | Hydro-Quebec | Drone with tool positioning system |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN1843843A (en) * | 2006-04-25 | 2006-10-11 | 刘纯生 | Safety air bag for airplane |
| CN200995783Y (en) * | 2006-06-01 | 2007-12-26 | 肖忠渊 | Helicopter of carbon-fibre composite material with amphibious landing and takeoff functions |
| US20100206983A1 (en) * | 2007-10-22 | 2010-08-19 | Cheng-Ho Tho | Crash Attenuation System for Aircraft |
| CN201587535U (en) * | 2009-12-22 | 2010-09-22 | 航宇救生装备有限公司 | Landing cushioning airbag |
| CN201712786U (en) * | 2010-06-02 | 2011-01-19 | 林松 | Amphibious buoy-skid type collapsible undercarriage used for helicopters |
-
2013
- 2013-11-27 CN CN201310606534.4A patent/CN104670480A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN1843843A (en) * | 2006-04-25 | 2006-10-11 | 刘纯生 | Safety air bag for airplane |
| CN200995783Y (en) * | 2006-06-01 | 2007-12-26 | 肖忠渊 | Helicopter of carbon-fibre composite material with amphibious landing and takeoff functions |
| US20100206983A1 (en) * | 2007-10-22 | 2010-08-19 | Cheng-Ho Tho | Crash Attenuation System for Aircraft |
| CN201587535U (en) * | 2009-12-22 | 2010-09-22 | 航宇救生装备有限公司 | Landing cushioning airbag |
| CN201712786U (en) * | 2010-06-02 | 2011-01-19 | 林松 | Amphibious buoy-skid type collapsible undercarriage used for helicopters |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US11368002B2 (en) | 2016-11-22 | 2022-06-21 | Hydro-Quebec | Unmanned aerial vehicle for monitoring an electrical line |
| US12097956B2 (en) | 2021-04-30 | 2024-09-24 | Hydro-Quebec | Drone with tool positioning system |
| CN114537687A (en) * | 2022-04-27 | 2022-05-27 | 济南市勘察测绘研究院 | Geographic information survey and drawing unmanned aerial vehicle equipment |
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| C02 | Deemed withdrawal of patent application after publication (patent law 2001) | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20150603 |