CN106791692B - A kind of video monitoring apparatus for unmanned plane - Google Patents
A kind of video monitoring apparatus for unmanned plane Download PDFInfo
- Publication number
- CN106791692B CN106791692B CN201710005767.7A CN201710005767A CN106791692B CN 106791692 B CN106791692 B CN 106791692B CN 201710005767 A CN201710005767 A CN 201710005767A CN 106791692 B CN106791692 B CN 106791692B
- Authority
- CN
- China
- Prior art keywords
- box body
- box
- unmanned plane
- monitoring apparatus
- support frame
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
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Classifications
-
- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04N—PICTORIAL COMMUNICATION, e.g. TELEVISION
- H04N7/00—Television systems
- H04N7/18—Closed-circuit television [CCTV] systems, i.e. systems in which the video signal is not broadcast
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2101/00—UAVs specially adapted for particular uses or applications
- B64U2101/30—UAVs specially adapted for particular uses or applications for imaging, photography or videography
Abstract
A kind of video monitoring apparatus for unmanned plane, including box body, the bottom of box body is installed by box cover, support frame is equipped in box body, the lower end of support frame is equipped with the water pocket of annular, two groups of separation nets are installed on the middle part of support frame and top, non-woven bag is placed in every group of separation net, exothermic mixture is filled in non-woven bag, it is storage facilities chamber between separation net, the inside of water pocket is equipped with chock plug, and the end of chock plug is fixedly connected by pull rod with the inner wall of box cover, storage facilities is intracavitary to be equipped with video storage device, and video storage device connects the camera on unmanned plane.Box cover end is upward in the present invention, when opening the lid, pull rod can be pulled up together, chock plug is pulled out simultaneously, water in water pocket can flow downward on non-woven bag and storage facilities, and the exothermic mixture in non-woven bag meets water and starts fever and water is become steam, and steam and high temperature, which can heat the electronic product in storage facilities, to be burnt, it is destroyed to store electronic bits of data, enemy is avoided to utilize the data.
Description
Technical field
The invention belongs to unmanned plane device field, specifically a kind of video monitoring apparatus for unmanned plane.
Background technique
With the application of unmanned plane, video capture device is carried by unmanned plane and carries out video data collection, led in military affairs
Using more and more extensive in domain.But after there is accident or is shot down in unmanned plane, the electronic bits of data meeting of carrying in unmanned plane
It is stolen by enemy, to cause information leakage.
Summary of the invention
The present invention provides a kind of video monitoring apparatus for unmanned plane, to solve defect in the prior art.
The present invention is achieved by the following technical programs:
A kind of video monitoring apparatus for unmanned plane, including box body, the bottom of box body install box cover, are equipped with branch in box body
Support, the lower end of support frame are equipped with the water pocket of annular, and the top peace of one group of separation net and support frame is installed at the middle part of support frame
Fill one group of separation net, non-woven bag placed in every group of separation net, fills exothermic mixture (such as quick lime) in non-woven bag, two groups every
It is storage facilities chamber between off-network, the inside of water pocket is equipped with chock plug, and the end of chock plug connects by the way that the inner wall of pull rod and box cover is fixed
It connects, storage facilities is intracavitary to be equipped with video storage device, and video storage device connects the camera on unmanned plane.
A kind of video monitoring apparatus for unmanned plane as described above, the two sides of the box body open up inner cavity, inner cavity
End fasten installation cavity cover, air bag is filled in inner cavity, gas generator is installed in box body, gas generator can be to air bag
Interior inflation.
A kind of video monitoring apparatus for unmanned plane as described above, the air bag are full of the top and bottom after gas
The distance between be greater than the length of box body, the width of air bag is greater than the width of box body.
A kind of video monitoring apparatus for unmanned plane as described above, the gas generator pass through igniting driving mould
Block is started, and igniting drive module connects time delay module, and time delay module connects pressure sensor, is equipped in box body to each mould
The power supply of block power supply, pressure sensor are installed in a triggering box to be multiple, and the periphery for triggering the inner wall of box is respectively mounted pressure
Force snesor, triggering box is interior to be equipped with a heavy ball.
The end of a kind of video monitoring apparatus for unmanned plane as described above, the box body is installed by medicine box, medicine box
Upper end be tubbiness, medicine box is sleeved on the end of box body, and the end connection installation parachute of box body, parachute, which is compacted, to be embedded in
The tubbiness region of medicine box, medicine box is interior to fill gunpowder, and the periphery of box body is equipped with sleeve, and the bottom of sleeve is equipped with pulse igniter, arteries and veins
The firing tip for rushing igniter is located in medicine box, and pulse igniter connects unmanned electromechanical source.
The invention has the advantages that it is intracavitary that storage device is mounted on storage facilities in the present invention.When unmanned plane or box body
After falling into enemy's hand.According to general inertial thinking, box cover end upward, can be upward together by pull rod when opening the lid
It pulls, while chock plug being pulled out, the water in water pocket can flow downward on non-woven bag and storage facilities, the hair in non-woven bag
Thermit powder meets water and starts fever and water is become steam, and steam and high temperature, which can heat the electronic product in storage facilities, to be burnt, from
And electronic bits of data is stored and is destroyed, avoid enemy from utilizing the data.Our personnel can be beaten in such a way that inversion prevents
It opens, facilitates and take out relevant device.
Detailed description of the invention
In order to more clearly explain the embodiment of the invention or the technical proposal in the existing technology, to embodiment or will show below
There is attached drawing needed in technical description to be briefly described, it should be apparent that, the accompanying drawings in the following description is this hair
Bright some embodiments for those of ordinary skill in the art without any creative labor, can be with
It obtains other drawings based on these drawings.
Fig. 1 is structural schematic diagram of the invention；Fig. 2 is I partial enlargement structural representation of Fig. 1；Fig. 3 is of the invention makes
With status architecture schematic diagram；Fig. 4 is module connection block diagram of the invention.
Appended drawing reference: 1 box body, 2 box cover, 3 support frame, 4 water pocket, 5 separation net, 6 non-woven bag, 7 storage facilities chamber 8 plug
13 gas generator 14 of first 9 pull rod, 10 inner cavity 11 cavity cover, 12 air bag igniting 15 time delay module of drive module, 16 pressure
Sensor 17 triggers 18 heavy ball of box, 19 sleeve, 20 pulse igniter, 21 power supply, 22 medicine box, 23 parachute.
Specific embodiment
It in order to make the object, technical scheme and advantages of the embodiment of the invention clearer, below will be in the embodiment of the present invention
Technical solution be clearly and completely described, it is clear that described embodiments are some of the embodiments of the present invention, rather than
Whole embodiments.Based on the embodiments of the present invention, those of ordinary skill in the art are not making creative work premise
Under every other embodiment obtained, shall fall within the protection scope of the present invention.
A kind of video monitoring apparatus for unmanned plane, as shown, including box body 1, box cover 2 is installed in the bottom of box body 1,
Support frame 3 is equipped in box body 1, the lower end of support frame 3 is equipped with the water pocket 4 of annular, and one group of separation net 5 is installed at the middle part of support frame 3
And one group of separation net 5 is installed on the top of support frame 3, and non-woven bag 6 is placed in every group of separation net 5, filling hair in non-woven bag 6
Thermit powder (such as quick lime), is storage facilities chamber 7 between two groups of separation nets 5, and the inside of water pocket 4 is equipped with chock plug 8, the end of chock plug 8
Portion is fixedly connected by pull rod 9 with the inner wall of box cover 2, and video storage device is equipped in storage facilities chamber 7, and video storage device connects
Connect the camera on unmanned plane.In the present invention, storage device is mounted in storage facilities chamber 7.When unmanned plane or box body 1 are fallen
After entering in enemy's hand.According to general inertial thinking, 2 end of box cover upward, open the lid 2 when, can be by pull rod 9 together upwards
It pulls, while chock plug 8 being pulled out, the water in water pocket 4 can flow downward on non-woven bag 6 and storage facilities, in non-woven bag 6
Exothermic mixture meet water and start fever and water is become into steam, the electronic product in storage facilities can be heated and be burnt by steam and high temperature
It ruins, is destroyed so that electronic bits of data be stored, enemy is avoided to utilize the data.The side that our personnel can be prevented using inversion
Formula is opened, and is facilitated and is taken out relevant device.
Specifically, will cause 1 hard landing of box body when unmanned plane breaks down sometimes, landing to reduce the present invention
When impact force, the two sides of effective protection box body 1 and its internal unit, box body 1 described in the present embodiment open up inner cavity 10, inner cavity
10 end fastens installation cavity cover 11, and air bag 12 is filled in inner cavity 10, gas generator 13 is installed in box body 1, gas occurs
Device 13 can be inflated into air bag 12.Fuel in gas generator 13 is sodium azide, can quickly be occurred on triggering anti-
A large amount of nitrogen should be generated, gas generator 13 starts in drop event of the present invention, and gas, gas are quickly filled with into air bag 12
Press it is larger cavity cover 11 can be opened, thus box body 1 two sides formed protection air bag 12.
Specifically, air bag 12 described in the present embodiment is greater than box body 1 full of the distance between the top and bottom after gas
Length, the width of air bag 12 are greater than the width of box body 1.12 volume of air bag after inflation is larger, the whole length for being greater than box body 1 and
Width is integrally that air bag 12 preferentially lands when landing, is capable of the damage of effective protection box body 1 received.
Further, in order to realize that the automatic inflating of air bag 12, gas generator 13 described in the present embodiment pass through igniting
Drive module 14 is started, and igniting drive module 14 connects time delay module 15, and time delay module 15 connects pressure sensor 16, box
The power supply 21 powered to modules is equipped in body 1, pressure sensor 16 is installed in a triggering box 17 to be multiple, is triggered
The periphery of the inner wall of box 17 is respectively mounted pressure sensor 16, is equipped with a heavy ball 18 in triggering box 17.In general flight course, weight
Ball 18 is at least contacted with a pressure sensor 16 always, keep 16 signal of pressure sensor output, when occur falling situation when,
Heavy ball 18 is state of weightlessness within a certain period of time, no longer gives 16 signal of pressure sensor, when time delay module 15 is triggered, delay one
After section time (such as 3-5 seconds), starting ignition drive module 14, which starts gas generator 13, is inflated.
Further, medicine box 22 is installed in the end of box body 1 described in the present embodiment, and the upper end of medicine box 22 is tubbiness, medicine
Box 22 is sleeved on the end of box body 1, and the end connection installation parachute 23 of box body 1, parachute 23, which is compacted, is embedded in medicine box 22
Tubbiness region, gunpowder is filled in medicine box 22, the periphery of box body 1 is equipped with sleeve 19, and the bottom of sleeve 19 is equipped with pulse igniter
20, the firing tip of pulse igniter 20 is located in medicine box 22, and pulse igniter 20 connects unmanned electromechanical source.By remotely controlling
Mode driving pulse igniter 20 makes 22 combustion explosion of medicine box, so that 1 overall emission of box body is gone out, the transmitting of box body 1 to highest
It is begun to decline after point, while parachute 23 is opened under the action of air flows, and reduces the speed of landing, enables box body 1
Grease it in.
Finally, it should be noted that the above embodiments are merely illustrative of the technical solutions of the present invention, rather than its limitations；Although
Present invention has been described in detail with reference to the aforementioned embodiments, those skilled in the art should understand that: it still may be used
To modify the technical solutions described in the foregoing embodiments or equivalent replacement of some of the technical features；
And these are modified or replaceed, technical solution of various embodiments of the present invention that it does not separate the essence of the corresponding technical solution spirit and
Range.
Claims (5)
1. a kind of video monitoring apparatus for unmanned plane, it is characterised in that: including box body (1), the bottom mounting box of box body (1)
It covers (2), is equipped with support frame (3) in box body (1), the lower end of support frame (3) is equipped with the water pocket (4) of annular, the middle part of support frame (3)
One group of separation net (5) is installed on the top for installing one group of separation net (5) and support frame (3), places nonwoven in every group of separation net (5)
Cloth bag (6) fills exothermic mixture in non-woven bag (6), is between two groups of separation nets (5) storage facilities chamber (7), water pocket (4) it is interior
Side is equipped with chock plug (8), and the end of chock plug (8) is fixedly connected by pull rod (9) with the inner wall of box cover (2), in storage facilities chamber (7)
Equipped with video storage device, video storage device connects the camera on unmanned plane.
2. a kind of video monitoring apparatus for unmanned plane according to claim 1, it is characterised in that: the box body
(1) two sides open up inner cavity (10), and the end of inner cavity (10) fastens installation cavity cover (11), fill in air bag in inner cavity (10)
(12), gas generator (13) are installed in box body (1), gas generator (13) being capable of the inflation into air bag (12).
3. a kind of video monitoring apparatus for unmanned plane according to claim 2, it is characterised in that: the air bag
(12) it is greater than the length of box body (1) full of the distance between the top and bottom after gas, the width of air bag (12) is greater than box body (1)
Width.
4. a kind of video monitoring apparatus for unmanned plane according to claim 2, it is characterised in that: the gas hair
Raw device (13) are started by igniting drive module (14), igniting drive module (14) connection time delay module (15), and be delayed mould
Block (15) connects pressure sensor (16), and the power supply (21) powered to modules, pressure sensor (16) are equipped in box body (1)
It is installed in a triggering box (17) to be multiple, the periphery for triggering the inner wall of box (17) is respectively mounted pressure sensor (16), is touched
It sends out and is equipped with a heavy ball (18) in box (17).
5. a kind of video monitoring apparatus for unmanned plane according to claim 1, it is characterised in that: the box body
(1) medicine box (22) are installed in end, and the upper end of medicine box (22) is tubbiness, and medicine box (22) is sleeved on the end of box body (1), box body
(1) end connection installation parachute (23), parachute (23) are compacted the tubbiness region for being embedded in medicine box (22), medicine box (22)
The periphery of interior filling gunpowder, box body (1) is equipped with sleeve (19), and the bottom of sleeve (19) is equipped with pulse igniter (20), pulse point
The firing tip of firearm (20) is located in medicine box (22), and pulse igniter (20) connects unmanned electromechanical source.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710005767.7A CN106791692B (en) | 2017-01-05 | 2017-01-05 | A kind of video monitoring apparatus for unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710005767.7A CN106791692B (en) | 2017-01-05 | 2017-01-05 | A kind of video monitoring apparatus for unmanned plane |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN106791692A CN106791692A (en) | 2017-05-31 |
| CN106791692B true CN106791692B (en) | 2019-05-14 |
Family
ID=58950688
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710005767.7A Expired - Fee Related CN106791692B (en) | 2017-01-05 | 2017-01-05 | A kind of video monitoring apparatus for unmanned plane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106791692B (en) |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN1340019A (en) * | 1999-02-12 | 2002-03-13 | 热学发展有限公司 | Tamper evident closure |
| JP2009087504A (en) * | 2007-10-03 | 2009-04-23 | Tomoaki Ito | Information storage medium destruction device |
| CN101615235A (en) * | 2009-08-04 | 2009-12-30 | 青岛海信智能商用设备有限公司 | A kind of self-destruction system for memory data |
| CN204904279U (en) * | 2015-07-31 | 2015-12-23 | 珠海市一微半导体有限公司 | Storage device with data are from destroying mechanism |
| JP5875166B1 (en) * | 2014-12-04 | 2016-03-02 | 三央工業株式会社 | Combined destruction device |
| CN105552036A (en) * | 2015-12-16 | 2016-05-04 | 鸿秦（北京）科技有限公司 | Shape memory alloy based chip destroying device and method |
-
2017
- 2017-01-05 CN CN201710005767.7A patent/CN106791692B/en not_active Expired - Fee Related
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN1340019A (en) * | 1999-02-12 | 2002-03-13 | 热学发展有限公司 | Tamper evident closure |
| JP2009087504A (en) * | 2007-10-03 | 2009-04-23 | Tomoaki Ito | Information storage medium destruction device |
| CN101615235A (en) * | 2009-08-04 | 2009-12-30 | 青岛海信智能商用设备有限公司 | A kind of self-destruction system for memory data |
| JP5875166B1 (en) * | 2014-12-04 | 2016-03-02 | 三央工業株式会社 | Combined destruction device |
| CN204904279U (en) * | 2015-07-31 | 2015-12-23 | 珠海市一微半导体有限公司 | Storage device with data are from destroying mechanism |
| CN105552036A (en) * | 2015-12-16 | 2016-05-04 | 鸿秦（北京）科技有限公司 | Shape memory alloy based chip destroying device and method |
Also Published As
| Publication number | Publication date |
|---|---|
| CN106791692A (en) | 2017-05-31 |
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| SE01 | Entry into force of request for substantive examination | ||
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| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20190514 Termination date: 20210105 |