CN106585988A - Explosive-removing unmanned aerial vehicle - Google Patents
Explosive-removing unmanned aerial vehicle Download PDFInfo
- Publication number
- CN106585988A CN106585988A CN201710026716.2A CN201710026716A CN106585988A CN 106585988 A CN106585988 A CN 106585988A CN 201710026716 A CN201710026716 A CN 201710026716A CN 106585988 A CN106585988 A CN 106585988A
- Authority
- CN
- China
- Prior art keywords
- servomotor
- explosive
- electric cylinders
- expansion link
- power component
- 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.)
- Granted
Links
- 239000002360 explosive Substances 0.000 claims abstract description 30
- 229910000831 Steel Inorganic materials 0.000 claims abstract description 11
- 239000010959 steel Substances 0.000 claims abstract description 11
- 238000005553 drilling Methods 0.000 claims abstract 2
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims description 24
- 239000003721 gunpowder Substances 0.000 claims description 9
- 230000009194 climbing Effects 0.000 claims description 4
- 230000005611 electricity Effects 0.000 claims description 3
- 238000009434 installation Methods 0.000 claims description 3
- 230000000712 assembly Effects 0.000 abstract 3
- 238000000429 assembly Methods 0.000 abstract 3
- 238000004880 explosion Methods 0.000 description 5
- 230000015572 biosynthetic process Effects 0.000 description 2
- 238000005474 detonation Methods 0.000 description 2
- 239000012634 fragment Substances 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000034994 death Effects 0.000 description 1
- 231100000517 death Toxicity 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000007599 discharging Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 230000007704 transition Effects 0.000 description 1
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/02—Aircraft not otherwise provided for characterised by special use
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B25—HAND TOOLS; PORTABLE POWER-DRIVEN TOOLS; MANIPULATORS
- B25J—MANIPULATORS; CHAMBERS PROVIDED WITH MANIPULATION DEVICES
- B25J11/00—Manipulators not otherwise provided for
- B25J11/002—Manipulators for defensive or military tasks
- B25J11/0025—Manipulators for defensive or military tasks handling explosives, bombs or hazardous objects
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D1/00—Dropping, ejecting, releasing, or receiving articles, liquids, or the like, in flight
- B64D1/22—Taking-up articles from earth's surface
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U50/00—Propulsion; Power supply
- B64U50/10—Propulsion
- B64U50/19—Propulsion using electrically powered motors
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Robotics (AREA)
- Remote Sensing (AREA)
- Disintegrating Or Milling (AREA)
- Working Measures On Existing Buildindgs (AREA)
Abstract
The invention provides an explosive-removing unmanned aerial vehicle comprising a vehicle body, two first square sleeves, two first telescopic rods, three power assemblies, a steel wire rope and the like. The explosive-removing unmanned aerial vehicle is characterized in that the vehicle body is of a cuboid structure; the head of the vehicle is in a point-end shape; the square sleeves are mounted on the left side and the right side of the vehicle body correspondingly; each first telescopic rod is slidably mounted in the corresponding square sleeve; two power assemblies are mounted on the upper portions of the outer end portions of the first telescopic rods correspondingly; and another power assembly is arranged on the rear portion of the vehicle body; and is mounted on the rear portion of the vehicle body through a rear portion mounting seat. The unmanned aerial vehicle can be flexibly controlled to rise up and go forward through the three power assemblies, explosive can be flexibly captured through arrangement of a mechanical arm, and drilling on the ground can be conducted through a cone-shaped spiral drill head on a pneumatic clamping jaw.
Description
Technical field
The present invention relates to extraordinary unmanned air vehicle technique field, more particularly to a kind of explosive unmanned plane.
Background technology
With running down for global anti-terror explosive removing situation, increasing soldier is because during explosive is excluded
Injures and deaths, it is development trend in the future that explosive is excluded using equipment special, and traditional explosive equipment such as explosive-removal robot etc. is deposited
The speed of travel it is slow, walk dangerous big shortcoming in urban district after explosive is got, with unmanned air vehicle technique increasingly into
It is ripe, unmanned plane can be adopted as the carrier of explosive device, unmanned plane has the characteristics of translational speed is fast, landing is flexible,
With unmanned plane shift explosive when due to being to transport in the air, so little to the menace in urban district.
The content of the invention
For the problems referred to above, the present invention provides a kind of explosive unmanned plane, and the present invention, can be with by arranging three Power Components
Flexible control unmanned plane rises and advances；Explosive can flexibly be captured by arranging mechanical arm, by Pneumatic clamping jaw
Tapered twist drill can drill on the ground；Small-sized gunpowder demolition set can be prevented outside in explosion time by Bell jar
Release fragment, to protect the safety of people around.
Technical scheme used in the present invention is：A kind of explosive unmanned plane, including body, two the first square sockets, two
First expansion link, three Power Components, steel wire rope, the first servomotor, Bell jar, the second square socket, the second expansion link, second
Servomotor, swing arm, the 3rd servomotor, Pneumatic clamping jaw, direct current generator, tapered twist drill, rear portion mounting seat, elevator
Machine, water under high pressure demolition set, it is characterised in that：Described body is rectangular structure, and prow is pointed shape, in body or so
Both sides are respectively provided with first square socket, and first expansion link is slidably fitted with each first square socket, and first stretches
Power Component is installed above the outer end of bar, the rear portion of body also is provided with a Power Component, and the Power Component passes through rear portion
Mounting seat is arranged on After-Body；One hoist engine is installed in internal body, hoist engine is lifted first and watched by steel wire rope
Take motor and Bell jar, described steel wire rope bottom and the connection of the first servomotor bottom, the motor shaft of the first servomotor
Be fixedly connected with Bell jar top, a mechanical arm be installed on the right side of Bell jar, described mechanical arm include the second square socket,
Two expansion links, the second servomotor, swing arm, the 3rd servomotor, Pneumatic clamping jaw, direct current generator, tapered twist drill, it is described
The second square socket be fixedly mounted on the right side of bell cover outer wall, be provided with the second square socket can stretch second stretch
Bar, is provided with the second servomotor, motor shaft ends and the swing arm side of the second servomotor in the second expansion link outer end
Back-end location is fixedly connected, and swing arm front end is provided with the 3rd servomotor, the motor shaft and Pneumatic clamping jaw of the 3rd servomotor
Bottom is fixedly connected, Pneumatic clamping jaw front end have two can be with the jaw of parallelly opening-and-closing, jaw is used to clamp explosive, in pneumatic clamps
Pawl side is provided with direct current generator, and the motor shaft ends of direct current generator are provided with tapered twist drill, and tapered twist drill is used for
Drill on the ground；One spherical water under high pressure demolition set is installed inside Bell jar；
Described Power Component include lower disc, six electric cylinders, upper disk, brushless electric machine, propellers, lower disc and upper disk it
Between be provided with six electric cylinders, described electric cylinders include electric cylinders cylinder part and electric cylinders piston rod portion, and six electric cylinders are divided into three groups
And be connected with upper disk and lower disc by ball pivot, the electric cylinders cylinder part bottom of each group of two electric cylinders is close together, electricity
Cylinder piston rod part front end separates, and is provided with brushless electric machine, is provided with spiral on the motor shaft of brushless electric machine above upper disk
Oar, drives propeller rotation by brushless electric machine, controls the attitude of brushless electric machine, three power packages by six electric cylinders linkages
In part, the Power Component of body both sides is provided and climbing power controls organism balance, and the Power Component of After-Body provides pushing away forward
Power.
Further, the first described expansion link and the second expansion link are extended and retracted by hydraulic cylinder control.
Further, described water under high pressure demolition set includes spherical shell, water layer and small-sized gunpowder demolition set, and spherical shell is divided into
Two-layer, is dispersed with water layer between inside and outside spherical shell, and small-sized gunpowder demolition set is internally provided with spherical shell.
Beneficial effect of the present invention：
1. the present invention can flexibly control unmanned plane and rise and advance by arranging three Power Components.
2. explosive can flexibly be captured by arranging mechanical arm, can be with by the tapered twist drill on Pneumatic clamping jaw
Drill on the ground.
3. can prevent small-sized gunpowder demolition set from outwards discharging fragment in explosion time by Bell jar, to protect people around
Safety.
4. explosive is destroyed using water under high pressure demolition set, because there is the presence of water, it is possible to avoid spark
Formation, and the temperature at blast can be reduced, will not set off an explosion thing induced detonation.
Description of the drawings
Fig. 1 is the overall structure diagram of the present invention.
Fig. 2 is the hoist engine scheme of installation of the present invention.
Fig. 3 is the water under high pressure demolition set scheme of installation of the present invention.
Fig. 4 is the Power Component structural representation of the present invention.
Fig. 5 is the water under high pressure demolition set structural representation of the present invention.
Drawing reference numeral：1- bodies；The first square sockets of 2-；The first expansion links of 3-；4- Power Components；5- steel wire ropes；6- first
Servomotor；7- Bell jars；The second square sockets of 8-；The second expansion links of 9-；The second servomotors of 10-；11- swing arms；12- the 3rd
Servomotor；13- Pneumatic clamping jaws；14- direct current generators；15- tapered twist drills；16- rear portions mounting seat；17- hoist engines；18-
Water under high pressure demolition set；401- lower discs；402- electric cylinders cylinder parts；403- electric cylinders piston rod portions；The upper disks of 404-；405-
Brushless electric machine；406- propellers；1801- spherical shells；1802- water layers；The small-sized gunpowder demolition sets of 1803-.
Specific embodiment
Below by embodiment, and accompanying drawing is combined, technical scheme is described in further detail.
Embodiment
As shown in Figure 1, Figure 2, shown in Fig. 3, Fig. 4, Fig. 5, a kind of explosive unmanned plane, including the first square socket 2, two of body 1, two
One Power Component 4 of expansion link 3, three, steel wire rope 5, the first servomotor 6, Bell jar 7, the second square socket 8, the second expansion link
9th, the second servomotor 10, swing arm 11, the 3rd servomotor 12, Pneumatic clamping jaw 13, direct current generator 14, tapered twist drill
15th, rear portion mounting seat 16, hoist engine 17, water under high pressure demolition set 18, it is characterised in that：Described body 1 is rectangular structure,
Prow is pointed shape, is each side provided with first square socket 2 in body 1, peace of sliding in each first square socket 2
Equipped with first expansion link 3, Power Component 4 is installed above the outer end of the first expansion link 3, the rear portion of body 1 also is provided with
One Power Component 4, the Power Component 4 are arranged on 1 rear portion of body by rear portion mounting seat 16；One is provided with inside body 1
Individual hoist engine 17, hoist engine 17 lift the first servomotor 6 and Bell jar 7, described 5 lower end of steel wire rope by steel wire rope 5
Portion and the connection of 6 bottom of the first servomotor, the motor shaft of the first servomotor 6 are fixedly connected with 7 top of Bell jar, Bell jar 7
Right side is provided with a mechanical arm, described mechanical arm include the second square socket 8, the second expansion link 9, the second servomotor 10,
Swing arm 11, the 3rd servomotor 12, Pneumatic clamping jaw 13, direct current generator 14, tapered twist drill 15, the second described square socket
8 are fixedly mounted on the right side of 7 outer wall of Bell jar, are provided with the second expansion link 9 that can be stretched, second in the second square socket 8
9 outer end of expansion link is provided with the second servomotor 10, after the motor shaft ends of the second servomotor 10 and 11 side of swing arm
End position is fixedly connected, and 11 front end of swing arm is provided with the 3rd servomotor 12, the motor shaft of the 3rd servomotor 12 with it is pneumatic
13 bottom of jaw is fixedly connected, 13 front end of Pneumatic clamping jaw have two can be with the jaw of parallelly opening-and-closing, jaw is used to clamp explosive,
Direct current generator 14 is installed in 13 side of Pneumatic clamping jaw, the motor shaft ends of direct current generator 14 are provided with tapered twist drill 15,
Tapered twist drill 15 is used to drill on the ground；One spherical water under high pressure demolition set 18 is installed inside Bell jar 7；
Described Power Component 4 includes lower disc 401, six electric cylinders, upper disk 404, brushless electric machine 405, propellers 406, under
Six electric cylinders are provided between disk 401 and upper disk 404, described electric cylinders include electric cylinders cylinder part 402 and electric cylinders piston rod
Part 403, six electric cylinders are divided into three groups and are connected with upper disk 404 and lower disc 401 by ball pivot, and two of each group are electric
402 bottom of electric cylinders cylinder part of cylinder is close together, and 403 front end of electric cylinders piston rod portion separates, and installs above upper disk 404
There is brushless electric machine 405, propeller 406 is installed on the motor shaft of brushless electric machine 405, propeller is driven by brushless electric machine 405
406 rotations, control the attitude of brushless electric machine 405 by six electric cylinders linkages, and in three Power Components 4,1 both sides of body is dynamic
Power component 4 provides climbing power and controls body 1 and balances, and the Power Component 4 at 1 rear portion of body provides motive force forward.
Further, the first described expansion link 3 and the second expansion link 9 are extended and retracted by hydraulic cylinder control.
Further, described water under high pressure demolition set 18 includes spherical shell 1801, water layer 1082 and small-sized gunpowder explosion dress
1803 are put, 1801 points of spherical shell is two-layer, is dispersed with water layer 1082, is internally provided with little in spherical shell 1801 between inside and outside spherical shell 1801
Type gunpowder demolition set 1803.
Operation principle of the present invention：
First expansion link 3 is stretched out first by the present invention when taking off, and is then provided by two Power Components 4 of 1 both sides of body
Climbing power simultaneously controls body 1 and balances, and the Power Component 4 at 1 rear portion of body provides motive force forward, in each Power Component 4
Brushless electric machine 405 and the attitude of propeller 406 controlled by the linkage of six electric cylinders；When unmanned plane is flown to above explosive
Bell jar 7 and mechanical arm are put down by hoist engine 17, Bell jar 7 is controlled by the first servomotor 6 above Bell jar 7
Rotation, mechanical arm is reached above explosive, then by mechanical arm capturing explosive, concrete grammar is：By hydraulic pressure
Cylinder controls the flexible of the second expansion link 9, controls the swing of swing arm 11 by the second servomotor 10, by the 3rd servomotor
The rotation of 12 control Pneumatic clamping jaws 13, controls the rotation of tapered twist drill 15 by direct current generator 14, by Pneumatic clamping jaw 13
The jaw of two parallelly opening-and-closings clamp explosive, then unmanned plane takes off and transition is to spacious unmanned area, and next step passes through
Bell jar 7 and mechanical arm are put down by hoist engine 17, and then Pneumatic clamping jaw 13 overturns 180 ° and makes tapered twist drill 15 down, then
Direct current generator 14 is opened and drives tapered twist drill 15 to rotate, and tapered twist drill 15 gets out one on the ground and can be put into
The conical pit of explosive, next step Pneumatic clamping jaw 13 overturn 180 ° again, and then Pneumatic clamping jaw 13 unclamps explosive, makes explosive
Fall in conical pit, Bell jar 7 is covered above conical pit afterwards, then ignite water under high pressure demolition set 18, produced by exploding
Explosive is destroyed by raw water under high pressure, because there is the presence of water, it is possible to is avoided the formation of spark, and can be reduced at blast
Temperature, will not set off an explosion thing induced detonation.
Claims (3)
1. a kind of explosive unmanned plane, including body（1）, two the first square sockets（2）, two the first expansion links（3）, three power
Component（4）, steel wire rope（5）, the first servomotor（6）, Bell jar（7）, the second square socket（8）, the second expansion link（9）, second
Servomotor（10）, swing arm（11）, the 3rd servomotor（12）, Pneumatic clamping jaw（13）, direct current generator（14）, cone-type spiral bore
Head（15）, rear portion mounting seat（16）, hoist engine（17）, water under high pressure demolition set（18）, it is characterised in that：Described body
（561）For rectangular structure, prow is pointed shape, in body（1）One square socket, each square set are each side installed
First expansion link is slidably fitted with cylinder（3）, the first expansion link（3）Outer end above Power Component is installed（4）, machine
Body（1）Rear portion also be provided with a Power Component（4）, the Power Component（4）By rear portion mounting seat（16）Installed in body（1）
Rear portion；In body（1）Inside is provided with a hoisting mechanism（17）, hoist engine（17）By steel wire rope（5）Watch to lift first
Take motor（6）And Bell jar（776）, described steel wire rope（5）Bottom and the first servomotor（96）Bottom connects, and first watches
Take motor（6）Motor shaft and Bell jar（7）Top is fixedly connected, Bell jar（7）Right side is provided with a mechanical arm, described
Mechanical arm includes the second square socket（8）, the second expansion link（9）, the second servomotor（10）, swing arm（11）, the 3rd servo electricity
Machine（12）, Pneumatic clamping jaw（13）, direct current generator（14）, tapered twist drill（15）, described the second square socket（8）Fixed installation
In Bell jar（7）On the right side of outer wall, in the second square socket（8）In the second expansion link that can be stretched is installed（9）, it is flexible second
Bar（9）Outer end is provided with the second servomotor（10）, the second servomotor（10）Motor shaft ends and swing arm（11）Side
Surface rear end position is fixedly connected, swing arm（11）Front end is provided with the 3rd servomotor（12）, the 3rd servomotor（12）Electricity
Arbor and Pneumatic clamping jaw（13）Bottom is fixedly connected, Pneumatic clamping jaw（13）Front end have two can be with the jaw of parallelly opening-and-closing, jaw
For clamping explosive, in Pneumatic clamping jaw pawl（13）Side is provided with direct current generator（14）, direct current generator（14）Motor shaft end
Portion is provided with tapered twist drill（15）, tapered twist drill（15）For drilling on the ground；In Bell jar（7）It is internal to install
There is a spherical water under high pressure demolition set（18）；
Described Power Component（4）Including lower disc（401）, six electric cylinders, upper disks（404）, brushless electric machine（405）, spiral
Oar（406）, lower disc（401）With upper disk（404）Between be provided with six electric cylinders, described electric cylinders include electric cylinders cylinder part
（402）With electric cylinders piston rod portion（403）, six electric cylinders are divided into three groups and by ball pivot and upper disk（404）And lower disc
（401）Connection, the electric cylinders cylinder part of each group of two electric cylinders（402）Bottom is close together, electric cylinders piston rod portion（403）
Front end separates, in upper disk（404）Top is provided with brushless electric machine（405）, brushless electric machine（405）Motor shaft on spiral shell is installed
Rotation oar（406）, by brushless electric machine（405）Drive propeller（406）Rotation, controls brushless electric machine by six electric cylinders linkages
（405）Attitude, three Power Components（4）Middle body（1）The Power Component of both sides（4）Climbing power is provided and body is controlled（1）
Balance, body（1）The Power Component at rear portion（4）Motive force forward is provided.
2. a kind of explosive unmanned plane according to claim 1, it is characterised in that：The first described expansion link（3）With second
Expansion link（9）Extend and retract by hydraulic cylinder control.
3. a kind of explosive unmanned plane according to claim 1, it is characterised in that：Described water under high pressure demolition set（18）Bag
Include spherical shell（1801）, water layer（1082）With small-sized gunpowder demolition set（1803）, spherical shell（1801）It is divided into two-layer, in inside and outside spherical shell
（1801）Between be dispersed with water layer（1082）, internally spherical shell（1801）In be provided with small-sized gunpowder demolition set（1803）.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710026716.2A CN106585988B (en) | 2017-01-14 | 2017-01-14 | A kind of explosive unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710026716.2A CN106585988B (en) | 2017-01-14 | 2017-01-14 | A kind of explosive unmanned plane |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN106585988A true CN106585988A (en) | 2017-04-26 |
| CN106585988B CN106585988B (en) | 2018-11-20 |
Family
ID=58585485
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710026716.2A Active CN106585988B (en) | 2017-01-14 | 2017-01-14 | A kind of explosive unmanned plane |
Country Status (1)
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| CN (1) | CN106585988B (en) |
Cited By (12)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107161331A (en) * | 2017-05-27 | 2017-09-15 | 徐秀娥 | A kind of automatic replacing fluorescent tube unmanned plane |
| CN107363848A (en) * | 2017-09-08 | 2017-11-21 | 韩朝锋 | A kind of land mine Mai Fang robots |
| CN107554771A (en) * | 2017-09-08 | 2018-01-09 | 孟庆仕 | It is a kind of to be used to bury the unmanned plane for putting land mine |
| CN108429216A (en) * | 2018-04-01 | 2018-08-21 | 周佰平 | A kind of high-tension line deicing unmanned plane |
| CN109323636A (en) * | 2018-12-14 | 2019-02-12 | 湖南华诺星空电子技术有限公司 | A kind of not quick-fried object removal system based on unmanned platform |
| CN110329507A (en) * | 2019-07-16 | 2019-10-15 | 韦礼东 | A kind of explosive equipment of Intelligent unattended machine |
| CN110406678A (en) * | 2019-08-07 | 2019-11-05 | 北京凌天世纪控股股份有限公司 | Explosion flying robot |
| CN111392040A (en) * | 2020-04-10 | 2020-07-10 | 赵文波 | Explosion-removing unmanned aerial vehicle and explosion-removing method |
| CN111452058A (en) * | 2020-04-10 | 2020-07-28 | 赵文波 | Unmanned aerial vehicle explosion removing device and using method thereof |
| CN114013660A (en) * | 2021-11-09 | 2022-02-08 | 江苏科技大学 | Amphibious flight device for recycling unmanned equipment on water |
| CN114348259A (en) * | 2021-12-28 | 2022-04-15 | 台州市公安局 | It is alert with unmanned aerial vehicle that ware is destroyed to loading has remote explosive |
| CN118372271A (en) * | 2024-06-24 | 2024-07-23 | 合肥德智航创科技有限公司 | Manipulator for explosive-handling unmanned aerial vehicle |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107161331A (en) * | 2017-05-27 | 2017-09-15 | 徐秀娥 | A kind of automatic replacing fluorescent tube unmanned plane |
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| CN110406678A (en) * | 2019-08-07 | 2019-11-05 | 北京凌天世纪控股股份有限公司 | Explosion flying robot |
| CN111392040A (en) * | 2020-04-10 | 2020-07-10 | 赵文波 | Explosion-removing unmanned aerial vehicle and explosion-removing method |
| CN111452058A (en) * | 2020-04-10 | 2020-07-28 | 赵文波 | Unmanned aerial vehicle explosion removing device and using method thereof |
| CN111392040B (en) * | 2020-04-10 | 2023-05-30 | 北京路遥科技有限公司 | Explosion-venting unmanned aerial vehicle and explosion-venting method |
| CN114013660A (en) * | 2021-11-09 | 2022-02-08 | 江苏科技大学 | Amphibious flight device for recycling unmanned equipment on water |
| CN114348259A (en) * | 2021-12-28 | 2022-04-15 | 台州市公安局 | It is alert with unmanned aerial vehicle that ware is destroyed to loading has remote explosive |
| CN114348259B (en) * | 2021-12-28 | 2024-06-04 | 台州市公安局 | Police unmanned aerial vehicle loaded with remote explosive destroying device |
| CN118372271A (en) * | 2024-06-24 | 2024-07-23 | 合肥德智航创科技有限公司 | Manipulator for explosive-handling unmanned aerial vehicle |
| CN118372271B (en) * | 2024-06-24 | 2024-08-16 | 合肥德智航创科技有限公司 | Manipulator for explosive-handling unmanned aerial vehicle |
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| CN106585988B (en) | 2018-11-20 |
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