CN206160834U - Unmanned aerial vehicle trapper - Google Patents
Unmanned aerial vehicle trapper Download PDFInfo
- Publication number
- CN206160834U CN206160834U CN201621121159.XU CN201621121159U CN206160834U CN 206160834 U CN206160834 U CN 206160834U CN 201621121159 U CN201621121159 U CN 201621121159U CN 206160834 U CN206160834 U CN 206160834U
- Authority
- CN
- China
- Prior art keywords
- garnishment
- steering wheel
- steel wire
- discharger
- net
- 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.)
- Active
Links
- 230000007246 mechanism Effects 0.000 claims abstract description 36
- 229910000831 Steel Inorganic materials 0.000 claims abstract description 33
- 239000010959 steel Substances 0.000 claims abstract description 33
- 230000005540 biological transmission Effects 0.000 claims description 11
- 238000010304 firing Methods 0.000 claims description 6
- 238000003780 insertion Methods 0.000 claims description 6
- 230000037431 insertion Effects 0.000 claims description 6
- 239000002390 adhesive tape Substances 0.000 claims description 3
- 238000005516 engineering process Methods 0.000 abstract description 4
- 238000013461 design Methods 0.000 description 11
- 238000010586 diagram Methods 0.000 description 4
- 230000033001 locomotion Effects 0.000 description 4
- 238000000034 method Methods 0.000 description 4
- 238000002347 injection Methods 0.000 description 3
- 239000007924 injection Substances 0.000 description 3
- 230000000149 penetrating effect Effects 0.000 description 3
- 230000032683 aging Effects 0.000 description 2
- 230000008859 change Effects 0.000 description 2
- 238000013016 damping Methods 0.000 description 2
- 239000007789 gas Substances 0.000 description 2
- 238000009527 percussion Methods 0.000 description 2
- 230000008569 process Effects 0.000 description 2
- 230000035945 sensitivity Effects 0.000 description 2
- 239000000243 solution Substances 0.000 description 2
- 208000027418 Wounds and injury Diseases 0.000 description 1
- 230000006378 damage Effects 0.000 description 1
- 238000005034 decoration Methods 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 230000018109 developmental process Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 239000002360 explosive Substances 0.000 description 1
- 230000010006 flight Effects 0.000 description 1
- 230000006872 improvement Effects 0.000 description 1
- 208000014674 injury Diseases 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
Landscapes
- Manipulator (AREA)
Abstract
The utility model discloses an unmanned aerial vehicle trapper belongs to the unmanned aerial vehicle capturing technology field, including triangle -shaped support and emitter mounting bracket, the triangle -shaped support links together through triangle -shaped support pipe, the emitter mounting bracket links together through horizontal pole and standpipe, install the steel wire isolator between triangle -shaped support and the emitter mounting bracket, install the kickoff mechanism in the arbitrary triangle -shaped support, install range unit on two horizontal poles in two emitter mounting brackets, the range unit top is connected with moving camera, the range unit bottom is connected with the picture and passes equipment, arbitrary emitter mounting bracket middle part is connected with the launch pad, install emitter on the launch pad, install in the emitter and grab the net. The utility model discloses the utilization is penetrated the net and is caught target unmanned aerial vehicle to it lets unmanned aerial vehicle fall in safe region again to fly, and supporting moreover have the picture to pass equipment, on convenient definite opportunity of arresting, has improved security and accuracy greatly.
Description
Technical field
This utility model belongs to unmanned plane capturing technology field, and in particular to a kind of unmanned plane catcher.
Background technology
The common principle of unmanned plane catcher has two kinds：One kind is to utilize Electromagnetic Interference, causes UAV targets to work
Failure；Another kind is to cause UAV targets' job failure using object contact target unmanned plane, such as using guided missile or grab net
Destroy unmanned plane.During initial development, the country has no forming technique to two kinds of unmanned plane capturing technologies.The former most profit
With pickaback formula interference unit, interference success rate is high, but carries heavy, and does not adapt to intricately shape, and operating radius receives people institute energy
The range effects of arrival.The latter's high cost, it is dangerous larger.For the purpose of both seizure schemes are to shoot down unmanned plane, it is impossible to keep away
Exempt from ground of falling after UAV targets' failure potentially to threaten.If UAV targets carry explosive, after unmanned plane falls
The secondary injury caused to ground installation is just into urgent problem.
Utility model content
This utility model purpose is：A kind of unmanned plane catcher is aimed to provide, is caught UAV targets using net is penetrated, and
Fly to safety zone and allow unmanned plane to fall again, and be configured with Image transmission equipment, facilitate determination to arrest opportunity, substantially increase
Safety and accuracy.
To realize above-mentioned technical purpose, the technical solution adopted in the utility model is as follows：
A kind of unmanned plane catcher, including two triangular supports and two discharger installing racks, described two triangles
Shape support is linked together by triangular supports pipe, and described two discharger installing racks are perpendicular by two cross bars and two
Pipe links together, and steel wire vibration isolator is provided between described two triangular supports and two discharger installing racks, described
Two triangular supports and two discharger installing racks are connected by steel wire vibration isolator, in described any one triangular supports
Kickoff mechanism is installed, range unit, the range finding are installed between two discharger installing racks on described two cross bars
Device top is connected with moving camera, and the range unit bottom is connected with Image transmission equipment, described any one discharger peace
Shelve middle part and be connected with transmitting station, discharger is installed on the transmitting station, be provided with the discharger and grab net.
Using the utility model of the technical program, on main aircraft, main aircraft can be as needed for the catcher carry
Change different aircraft.Discharger installing rack is linked together by steel wire vibration isolator and triangular supports, triangle
Frame links together with main aircraft, and the recoil for penetrating network process generation is absorbed completely by steel wire vibration isolator.Moving camera and figure
Image information is sent in real time biography equipment ground screen, and ground judges UAV targets position, Ran Houtong by range unit
Remote controller operation discharger is crossed, injection is grabbed net, entirely grabs net and wrap after UAV targets, when main aircraft flight is to safety
During region, ground will be grabbed net and freed by remote controller operation kickoff mechanism, discharge UAV targets.Such structure design, profit
UAV targets are caught with net is penetrated, and is flown to safety zone and is allowed unmanned plane to fall again, and be configured with Image transmission equipment, side
Just determine and arrest opportunity, substantially increase safety and accuracy.
Further limit, the discharger includes ejecting gun, the ejecting gun gun barrel is connected with air chamber, the ejecting gun
On be provided with switch knob, firing pin and trigger, the ejecting gun gun barrel lower section is provided with axle sleeve, steel wire disk, rotary shaft, garnishment mechanism
With garnishment steering wheel, the garnishment steering wheel is connected with transmitting station, and the steel wire disk is connected on garnishment steering wheel, the steel wire disk
Be arranged with steel wire rope, the steel wire rope bypasses axle sleeve and free end is connected with one end of garnishment mechanism, the garnishment mechanism it is another
One end is connected with trigger, and the rotary shaft is arranged on garnishment mechanism middle part, and the garnishment mechanism is turned by rotary shaft with transmitting station
Dynamic connection.Such structure design, is rotated by controlling garnishment steering wheel, drives steel wire disk to rotate, and steel wire rope pulls garnishment machine
One end of structure, garnishment mechanism rotates around rotary shaft, the other end cocking of garnishment mechanism when rotating, and rebound switch knob, firing pin
After percussion sub-warhead, gases at high pressure will grab net and project by air chamber, to reach the purpose that net is grabbed in transmitting.
Further limit, the kickoff mechanism includes connection sheet, latch, lock frame, steering wheel and steering wheel disk, the steering wheel disk connects
It is connected on steering wheel, the steering wheel disk is connected with latch by connection sheet, inside the latch insertion lock frame.Such structure sets
Meter, servo driving steering wheel disk is rotated, and steering wheel disk drives connection sheet and latch motion, latch motion realization in the hole of lock frame to open
Close, to reach the purpose for grabbing net is freed.
Further limit, the net of grabbing is provided with four guide heads, in the pilot hole of four guide heads insertion air chamber,
Described grabbing be provided with a head rope after net, and the end of the head rope is provided with annular ring, and annular ring is enclosed within latch.So
Structure design, air chamber projects guide head, makes entirely to grab net and wraps UAV targets, when main aircraft flight is to safety zone
Afterwards, latch is opened, and annular ring departs from from kickoff mechanism, and realization is entirely grabbed net and separated with the catcher.
Further limit, the range unit is radar range finding sensor.Such structure design, with small volume, spirit
The advantages of sensitivity is high.
Further limit, the moving camera and Image transmission equipment are bonding with range unit by sponge double faced adhesive tape.It is such
Structure design, fire resistance is good, ageing-resistant, rub resistance, moreover it is possible to play a part of temperature resistance damping.
Description of the drawings
The nonlimiting examples that this utility model can be given by accompanying drawing are further illustrated；
Fig. 1 is a kind of dimensional structure diagram of unmanned plane catcher embodiment of this utility model；
Fig. 2 is a kind of right side structural representation of unmanned plane catcher embodiment of this utility model；
Fig. 3 is the mplifying structure schematic diagram of discharger in Fig. 1；
Fig. 4 is the mplifying structure schematic diagram of kickoff mechanism closure state in Fig. 1；
Fig. 5 is the mplifying structure schematic diagram of kickoff mechanism opening in Fig. 1；
Main element symbol description is as follows：
1st, moving camera；2nd, discharger；21st, ejecting gun；22nd, air chamber；23rd, switch knob；24th, firing pin；25th, trigger；26th, axle
Set；27th, steel wire rope；28th, steel wire disk；29th, rotary shaft；210th, garnishment mechanism；211st, garnishment steering wheel；3rd, kickoff mechanism；31st, even
Contact pin；32nd, latch；33rd, frame is locked；34th, steering wheel；35th, steering wheel disk；4th, triangular supports；5th, discharger installing rack；6th, steel wire every
Shake device；7th, Image transmission equipment；8th, range unit.
Specific embodiment
In order that those skilled in the art may be better understood this utility model, it is right with reference to the accompanying drawings and examples
Technical solutions of the utility model are further illustrated.
As depicted in figs. 1 and 2, a kind of unmanned plane catcher of the present utility model, including two triangular supports 4 and two
Discharger installing rack 5, two triangular supports 4 are linked together by triangular supports pipe, and two dischargers are installed
Frame 5 is linked together by two cross bars and two vertical tubes, between two triangular supports 4 and two discharger installing racks 5
Steel wire vibration isolator 6 is installed, two triangular supports 4 and two discharger installing racks 5 are connected by steel wire vibration isolator 6, appoints
Kickoff mechanism 3 is installed in one triangular supports 4 of meaning, survey is installed in two discharger installing racks 5 on two cross bars
Away from device 8, the top of range unit 8 is connected with moving camera 1, and the bottom of range unit 8 is connected with Image transmission equipment 7, and any one is sent out
The middle part of injection device installing rack 5 is connected with transmitting station, is provided with to be provided with discharger 2, discharger 2 on transmitting station and grabs net.
In the present embodiment, on main aircraft, main aircraft can as needed change different flights to the catcher carry
Device.Discharger installing rack 5 is linked together by steel wire vibration isolator 6 with triangular supports 4, triangular supports 4 and main flight
Device links together, and the recoil for penetrating network process generation is absorbed completely by steel wire vibration isolator 6.Moving camera 1 and Image transmission equipment 7 will
Image information is sent in real time ground screen, and ground judges UAV targets position by range unit 8, then by remote control
Operation discharger 2, injection is grabbed net, entirely grabs net and wrap after UAV targets, when main aircraft flight is to safety zone,
Ground will be grabbed net 3 and freed by remote controller operation kickoff mechanism 3, discharge UAV targets.Such structure design, using penetrating
Net catches UAV targets, and flies to safety zone and allow unmanned plane to fall again, and is configured with Image transmission equipment, convenient true
Surely arrest opportunity, substantially increase safety and accuracy.
As shown in figure 3, preferred emission device 2 includes ejecting gun 21, the gun barrel of ejecting gun 21 is connected with air chamber 22, ejecting gun 21
On be provided with switch knob 23, firing pin 24 and trigger 25, the gun barrel of ejecting gun 21 lower section is provided with axle sleeve 26, steel wire disk 28, rotary shaft
29th, garnishment mechanism 210 and garnishment steering wheel 211, garnishment steering wheel 211 is connected with transmitting station, and steel wire disk 28 is connected to garnishment steering wheel
On 211, steel wire disk 28 is arranged with steel wire rope 27, and steel wire rope 27 bypasses axle sleeve 26 and one end of free end and garnishment mechanism 210
Connection, the other end of garnishment mechanism 210 is connected with trigger 25, and rotary shaft 29 is arranged on the middle part of garnishment mechanism 210, garnishment mechanism
210 are connected by rotary shaft 29 with transmitting station rotation.Such structure design, is rotated by controlling garnishment steering wheel 211, drives steel
Cord disk 28 is rotated, and steel wire rope 27 pulls one end of garnishment mechanism 210, garnishment mechanism 210 to rotate around rotary shaft 29, when rotating
The other end cocking 25 of garnishment mechanism 210, rebound switch knob 23, and after the percussion sub-warhead of firing pin 24, gases at high pressure pass through air chamber
22 will grab net projects, to reach the purpose that net is grabbed in transmitting.In fact, discharger 2 can also specifically be considered as the case may be
Structure.
As shown in Figure 4 and Figure 5, preferred kickoff mechanism 3 includes connection sheet 31, latch 32, lock frame 33, steering wheel 34 and steering wheel disk
35, steering wheel disk 35 is connected on steering wheel 34, and steering wheel disk 35 is connected with latch 32 by connection sheet 31, in the insertion lock frame 33 of latch 32
Portion.Such structure design, steering wheel 34 drives steering wheel disk 35 to rotate, and steering wheel disk 35 drives connection sheet 31 and latch 32 to move, and inserts
Folding is realized in the motion in the hole of lock frame 33 of pin 32, and to reach the purpose for grabbing net is freed.In fact, can also be as the case may be
The concrete structure for considering kickoff mechanism 3.
It is preferred that grabbing net is provided with four guide heads, in the pilot hole of four guide head insertion air chambers 22, grabs and be provided with after net
A piece head rope, the end of the head rope is provided with annular ring, and annular ring is enclosed within latch 32.Such structure design, air chamber 22 is projected
Guide head, makes entirely to grab net and wraps UAV targets, and after main aircraft flight is to safety zone, latch 32 is opened, annular
Circle departs from from kickoff mechanism 3, and realization is entirely grabbed net and separated with the catcher.In fact, can also be concrete as the case may be
The structure of net is grabbed in consideration.
It is preferred that range unit 8 is radar range finding sensor.Such structure design, it is excellent with small volume, sensitivity height etc.
Point.In fact, the species of other range units 8 can also be selected as the case may be.
Preferred movement camera 1 and Image transmission equipment 7 are by sponge double faced adhesive tape and the bonding connection of range unit 8.Such structure
Design, fire resistance is good, ageing-resistant, rub resistance, moreover it is possible to play a part of temperature resistance damping.In fact, can also be according to concrete feelings
Condition selects the connected mode of other moving cameras 1 and Image transmission equipment 7 and range unit 8.
A kind of unmanned plane catcher that this utility model is provided is described in detail above.The explanation of specific embodiment
It is only intended to help and understands method of the present utility model and its core concept.It should be pointed out that for the common skill of the art
For art personnel, on the premise of without departing from this utility model principle, some improvement can also be carried out to this utility model and is repaiied
Decorations, these are improved and modification is also fallen in this utility model scope of the claims.
Claims (6)
1. a kind of unmanned plane catcher, it is characterised in that：Including two triangular supports (4) and two discharger installing racks
(5), described two triangular supports (4) are linked together by pipe, and described two discharger installing racks (5) are by two
Cross bar and two vertical tubes link together, and install between described two triangular supports (4) and two discharger installing racks (5)
There is steel wire vibration isolator (6), described two triangular supports (4) and two discharger installing racks (5) are by steel wire vibration isolator (6)
Kickoff mechanism (3) is installed in connection, described any one triangular supports (4), in two transmitting dresses on described two cross bars
Put and be provided between installing rack (5) range unit (8), range unit (8) top is connected with moving camera (1), the survey
Image transmission equipment (7) is connected with away from device (8) bottom, described any one discharger installing rack (5) middle part is connected with transmitting station,
It is provided with to be provided with discharger (2), the discharger (2) on the transmitting station and grabs net.
2. a kind of unmanned plane catcher according to claim 1, it is characterised in that：The discharger (2) is including transmitting
Rifle (21), ejecting gun (21) gun barrel is connected with air chamber (22), and on the ejecting gun (21) switch knob (23), firing pin are provided with
(24) and trigger (25), ejecting gun (21) the gun barrel lower section be provided with axle sleeve (26), steel wire disk (28), rotary shaft (29),
Garnishment mechanism (210) and garnishment steering wheel (211), the garnishment steering wheel (211) is connected with transmitting station, and the steel wire disk (28) is even
It is connected on garnishment steering wheel (211), the steel wire disk (28) is arranged with steel wire rope (27), the steel wire rope (27) bypasses axle sleeve
(26) and free end is connected with one end of garnishment mechanism (210), the other end of the garnishment mechanism (210) is with trigger (25) even
Connect, installed in garnishment mechanism (210) middle part, the garnishment mechanism (210) is by rotary shaft (29) and sends out for the rotary shaft (29)
Penetrate platform and rotate connection.
3. a kind of unmanned plane catcher according to claim 2, it is characterised in that：The kickoff mechanism (3) is including connection
Piece (31), latch (32), lock frame (33), steering wheel (34) and steering wheel disk (35), the steering wheel disk (35) is connected on steering wheel (34),
The steering wheel disk (35) is connected with latch (32) by connection sheet (31), and the latch (32) insertion lock frame (33) is internal.
4. a kind of unmanned plane catcher according to claim 3, it is characterised in that：The net of grabbing is provided with four guiding
Head, in the pilot hole of four guide heads insertion air chamber (22), described grabbing be provided with a head rope, the end of the head rope after net
End is provided with annular ring, and annular ring is enclosed within latch (32).
5. a kind of unmanned plane catcher according to claim 4, it is characterised in that：The range unit (8) is radar survey
Away from sensor.
6. a kind of unmanned plane catcher according to claim 5, it is characterised in that：The moving camera (1) and figure biography set
Standby (7) are bonding with range unit (8) by sponge double faced adhesive tape.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621121159.XU CN206160834U (en) | 2016-10-13 | 2016-10-13 | Unmanned aerial vehicle trapper |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621121159.XU CN206160834U (en) | 2016-10-13 | 2016-10-13 | Unmanned aerial vehicle trapper |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206160834U true CN206160834U (en) | 2017-05-10 |
Family
ID=58654011
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201621121159.XU Active CN206160834U (en) | 2016-10-13 | 2016-10-13 | Unmanned aerial vehicle trapper |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206160834U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109782793A (en) * | 2018-11-28 | 2019-05-21 | 北京汉能光伏投资有限公司 | Unmanned plane rescue mode and system |
| CN112902757A (en) * | 2021-01-19 | 2021-06-04 | 卫国英 | Improve unmanned aerial vehicle trapper of catching effect |
-
2016
- 2016-10-13 CN CN201621121159.XU patent/CN206160834U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109782793A (en) * | 2018-11-28 | 2019-05-21 | 北京汉能光伏投资有限公司 | Unmanned plane rescue mode and system |
| CN112902757A (en) * | 2021-01-19 | 2021-06-04 | 卫国英 | Improve unmanned aerial vehicle trapper of catching effect |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US10871353B2 (en) | System for deploying a first object for capturing, immobilising or disabling a second object | |
| CN104590562B (en) | A kind of Anti-collision fixed point fire-fighting unmanned plane | |
| EP3540364B1 (en) | Drone interceptor system, and methods and computer program products useful in conjunction therewith | |
| KR101664618B1 (en) | The capture device is equipped with unmanned flight system and Capture method using the same | |
| CN106679507B (en) | One kind is soft to injure ammunition | |
| KR102114337B1 (en) | Capture equipment of drone | |
| CN106581906A (en) | High-rise building fire extinguishing apparatus based on unmanned aerial vehicle | |
| CN103935522B (en) | A kind of rotary wind type unmanned plane falling protecting device out of control and guard method | |
| CN106767172A (en) | A kind of pickaback portable anti-unmanned aerial vehicle ejecting is soft to injure retracting device | |
| CN206160834U (en) | Unmanned aerial vehicle trapper | |
| CN205327431U (en) | Novel unmanned aerial vehicle | |
| CN204822085U (en) | Unmanned aerial vehicle with arrest ware | |
| CN106995059A (en) | A kind of unmanned aerial vehicle onboard net gun apparatus | |
| CN102384702A (en) | Method for intercepting aircrafts without collateral damage in unmanned way | |
| CN110806147A (en) | Unmanned aerial vehicle catches and recovery unit | |
| CN107684677A (en) | A kind of winged jaw arrangement for high-rise fire extinguishing system | |
| RU2490584C1 (en) | Fighter device for destruction of drones | |
| CN110465036A (en) | Controllable guidance fire extinguisher bomb, fire extinguishing system and extinguishing method | |
| CN205784877U (en) | Unmanned plane capture triggering system | |
| CN207540428U (en) | A kind of unmanned plane blocking apparatus | |
| KR102297796B1 (en) | Fire fighting unmanned vehicle, and fire fighting system and method using the same | |
| CN109850151A (en) | A kind of unmanned plane arrest net device and unmanned plane | |
| CN113074583A (en) | Unmanned aerial vehicle capture equipment | |
| CN108275275A (en) | Unmanned plane throwing mechanism, unmanned plane and the delivering method based on unmanned plane | |
| CN209092568U (en) | A kind of high building extinguishing device based on unmanned plane |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| PE01 | Entry into force of the registration of the contract for pledge of patent right |
Denomination of utility model: A UAV catcher Effective date of registration: 20200820 Granted publication date: 20170510 Pledgee: Beijing Yanhong Financing Guarantee Co.,Ltd. Pledgor: BEIJING HANGJING INNOVATION SCIENCE & TECHNOLOGY Co.,Ltd. Registration number: Y2020990001003 |
|
| PE01 | Entry into force of the registration of the contract for pledge of patent right | ||
| PC01 | Cancellation of the registration of the contract for pledge of patent right |
Date of cancellation: 20210824 Granted publication date: 20170510 Pledgee: Beijing Yanhong Financing Guarantee Co.,Ltd. Pledgor: BEIJING HANGJING INNOVATION SCIENCE & TECHNOLOGY Co.,Ltd. Registration number: Y2020990001003 |
|
| PC01 | Cancellation of the registration of the contract for pledge of patent right | ||
| PE01 | Entry into force of the registration of the contract for pledge of patent right | ||
| PE01 | Entry into force of the registration of the contract for pledge of patent right |
Denomination of utility model: A UAV catcher Effective date of registration: 20210924 Granted publication date: 20170510 Pledgee: Beijing Yanhong Financing Guarantee Co.,Ltd. Pledgor: BEIJING HANGJING INNOVATION SCIENCE & TECHNOLOGY Co.,Ltd. Registration number: Y2021990000876 |
|
| PC01 | Cancellation of the registration of the contract for pledge of patent right |
Date of cancellation: 20230105 Granted publication date: 20170510 Pledgee: Beijing Yanhong Financing Guarantee Co.,Ltd. Pledgor: BEIJING HANGJING INNOVATION SCIENCE & TECHNOLOGY CO.,LTD. Registration number: Y2021990000876 |
|
| PC01 | Cancellation of the registration of the contract for pledge of patent right | ||
| PE01 | Entry into force of the registration of the contract for pledge of patent right |
Denomination of utility model: A UAV catcher Effective date of registration: 20230214 Granted publication date: 20170510 Pledgee: Beijing Yanhong Financing Guarantee Co.,Ltd. Pledgor: BEIJING HANGJING INNOVATION SCIENCE & TECHNOLOGY CO.,LTD. Registration number: Y2023110000065 |
|
| PE01 | Entry into force of the registration of the contract for pledge of patent right | ||
| PC01 | Cancellation of the registration of the contract for pledge of patent right |
Granted publication date: 20170510 Pledgee: Beijing Yanhong Financing Guarantee Co.,Ltd. Pledgor: BEIJING HANGJING INNOVATION SCIENCE & TECHNOLOGY CO.,LTD. Registration number: Y2023110000065 |
|
| PC01 | Cancellation of the registration of the contract for pledge of patent right |