CN106741889A - A kind of band catches the pouch-type aircraft of playing function - Google Patents
A kind of band catches the pouch-type aircraft of playing function Download PDFInfo
- Publication number
- CN106741889A CN106741889A CN201611065794.5A CN201611065794A CN106741889A CN 106741889 A CN106741889 A CN 106741889A CN 201611065794 A CN201611065794 A CN 201611065794A CN 106741889 A CN106741889 A CN 106741889A
- Authority
- CN
- China
- Prior art keywords
- aircraft
- target
- propeller
- support member
- connection support
- 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
- 229920000049 Carbon (fiber) Polymers 0.000 claims description 13
- 239000004917 carbon fiber Substances 0.000 claims description 13
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 claims description 13
- 239000000463 material Substances 0.000 claims description 12
- 229910000838 Al alloy Inorganic materials 0.000 claims description 5
- 230000005540 biological transmission Effects 0.000 claims description 5
- RZVHIXYEVGDQDX-UHFFFAOYSA-N 9,10-anthraquinone Chemical compound C1=CC=C2C(=O)C3=CC=CC=C3C(=O)C2=C1 RZVHIXYEVGDQDX-UHFFFAOYSA-N 0.000 description 4
- 238000010586 diagram Methods 0.000 description 3
- 238000009434 installation Methods 0.000 description 3
- 238000000034 method Methods 0.000 description 3
- 239000011120 plywood Substances 0.000 description 3
- 230000007797 corrosion Effects 0.000 description 2
- 238000005260 corrosion Methods 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 238000005728 strengthening Methods 0.000 description 2
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 1
- 235000006508 Nelumbo nucifera Nutrition 0.000 description 1
- 240000002853 Nelumbo nucifera Species 0.000 description 1
- 235000006510 Nelumbo pentapetala Nutrition 0.000 description 1
- 239000000956 alloy Substances 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 229910052799 carbon Inorganic materials 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000005484 gravity Effects 0.000 description 1
- 230000000977 initiatory effect Effects 0.000 description 1
- 229910052752 metalloid Inorganic materials 0.000 description 1
- 150000002738 metalloids Chemical class 0.000 description 1
- 238000003801 milling Methods 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/08—Helicopters with two or more rotors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C15/00—Attitude, flight direction, or altitude control by jet reaction
- B64C15/02—Attitude, flight direction, or altitude control by jet reaction the jets being propulsion jets
-
- 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
-
- 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
- B64D1/02—Dropping, ejecting, or releasing articles
- B64D1/08—Dropping, ejecting, or releasing articles the articles being load-carrying devices
- B64D1/12—Releasing
-
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2201/00—UAVs characterised by their flight controls
- B64U2201/10—UAVs characterised by their flight controls autonomous, i.e. by navigating independently from ground or air stations, e.g. by using inertial navigation systems [INS]
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2201/00—UAVs characterised by their flight controls
- B64U2201/20—Remote controls
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Toys (AREA)
Abstract
The present invention provides the pouch-type aircraft that a kind of band catches playing function, including propeller, propeller installing component, head connector, connection support member, catches and put part and sensor mounting block, and propeller installing component is used to install fixed propeller；Propeller installing component is used to be fixedly connected support member；It is bag structure that multiple connection support member constitutes closed polygon structure by multiple propeller installing component head and the tail closures；Head connector is fixed on connection support member；Sensor mounting block is used to install fixed various kinds of sensors, and sensor mounting block is fixed on connection support member；Catch the center that part is fixed on the connection support member for constituting each side of polygonized structure and is located at aircraft of putting.Using the manual aircraft of the present invention of remote control, aircraft vertical take off after fast approaching target, and make target drag for catching for aircraft by fuselage mode of toppling to put in part；Operation aircraft makes a return voyage, so as to captured target is taken back into ground together.
Description
Technical field
The present invention relates to unmanned air vehicle technique field, in particular it relates to a kind of band catches the pouch-type aircraft of playing function.
Background technology
In recent years, with the popularization of unmanned air vehicle technique, increasing unmanned plane is appeared in daily life.So
And because unmanned plane lacks effective Supervision Measures, in the case of being often able to appear in without permission, unmanned plane flies into correlation
The situation in region, work or daily life to relevant department bring influence.So needing exist for one kind can
The device captured to unmanned plane.
Through retrieval, multi-rotor aerocraft and its closure open frame (201510833372.7), it is many invention provides one kind
The closure open frame of rotor craft, can control rotor lift by changing pitch；Closed type multi-rotor aerocraft
(201420329869.6), the invention provides a kind of closed type multi-rotor aerocraft, invention focuses on strengthening the steady of frame
Gu degree and antitorque dynamic property.
Both the above closed type aircraft mainly puts forth effort on solution aircraft produced problem in flight course in itself.
The content of the invention
For defect of the prior art, it is an object of the invention to provide the pouch-type aircraft that a kind of band catches playing function,
Can be with high-speed flight, using the structure of the pocket open formula of shape aircraft, it is possible to achieve the capture and dispensing of target.
To realize object above, the present invention provides the pouch-type aircraft that a kind of band catches playing function, including：Propeller, push away
Enter device installing component, head connector, connect support member, catch and put part and sensor mounting block, wherein：
The propeller installing component is used to install fixed propeller and be fixedly connected support member；
Multiple connection support members pass through the polygonized structure that multiple propeller installing component head and the tail closures constitute closure,
Form bag structure；
The head connector is located at the connection support member on polygonized structure one side；
The sensor mounting block is used to install fixed various kinds of sensors, and sensor mounting block is fixed on connection support
On part；
It is described catch put part be fixed on the connection support member for constituting each side of polygonized structure and be located at the flight
The center of device.
Preferably, the propeller is duct or rotor power device.
Preferably, when the propeller is duct, propeller is located at the inner or outer side of propeller installing component, its
In：Inner side refer to aircraft closed polygon structure within direction, outside refers to beyond the closed polygon structure of aircraft
Direction.
Preferably, when the propeller be rotor power device when, propeller be located at propeller installing component top or
Lower section, wherein：Top refer to the closed polygon structural plan of aircraft vertically upward, lower section refers to the closure of aircraft
Polygonized structure plane vertical downward direction.
Preferably, the head connector is loaded with flying control device, GPS and data transmission module.
Preferably, the sensor includes ultrasonic wave, light stream, infrared, barometer, vision sensor.
Preferably, the connection support member material is carbon fiber or aluminium alloy.Carbon fiber is a kind of novel metalloid material,
It has the small excellent specific property of high specific strength, high ratio modulus, corrosion-resistant and thermal coefficient of expansion, is suitable as structural material and carries negative
Lotus, meeting the equal of above characteristic requirements can be used as the type selecting material of fuselage.Certainly, aluminum alloy materials can also be applicable.
Preferably, remote control is manual by setting for the aircraft, or the winged control device carried by aircraft itself
Realize automatically controlling with sensor：
When the manual aircraft capture target, approached by setting after aircraft vertical takes off described in remote control control
Target, and target is dragged for into catching for the aircraft put in part, then controls the aircraft to make a return voyage, target that will be captured
Ground is taken back together；When the aircraft is automatically controlled, the carry-on sensor sensing and after capturing target, by
Fly control device autonomous control and close to target, by target acquistion and take back ground；
When target is delivered, it would be desirable to which the target of dispensing is placed in catching and putting part, and the aircraft is with target
Destination is moved to after taking off vertically, target is slowly landed with the aircraft by way of vertical landing, target is removed
After being moved away from the aircraft, the aircraft is controlled to make a return voyage.
Further, polygonized structure of the present invention can be sandwich construction, and polygonized structure is in vertical direction described in multilayer
On connect to form with certain depth, layer stereo structure by connection support bar, it is possible to increase the mechanical strength of aircraft.
Aircraft of the present invention includes but is not limited to unmanned plane capture on application scenario, also can operate with and flies to aerial
Row thing (such as birds) is captured, or is carried out short distance, light goods and materials using the pouch-type aircraft that band catches playing function and put into operation
Occasion.The present invention includes but is not limited to realize arresting multiple unmanned plane targets.
Compared with prior art, the present invention has following beneficial effect：
1st, it is different from traditional multi-rotor unmanned aerial vehicle in structure：Show traditional multi-rotor unmanned aerial vehicle flight control system in center of gravity
Position, and the system for flight control computer, on the connection support member of pouch-type aircraft, center slot milling is caught for placement and is put
Part and the target of capture/dispensing.
2nd, it is safe and reliable in capture means：Compared to the mode of shooting down, it can prevent from shooting down capture unmanned plane and fall initiation
Security incident, farthest saves captured unmanned plane from damage；Compared to multiple unmanned planes collaboration linked network capture unmanned plane mode, this
Invention only need to manipulate a unmanned plane and be capable of achieving to arrest, it is easy to control and high-performance cruise.
The present invention catches net to capture the unmanned plane of illegal flight using installation in the middle of pouch-type aircraft, i.e., using pouch-type
The structure of the open formula of aircraft, in centre, net is caught in installation, can be used to capture unmanned plane；While aircraft of the present invention was both
Rotor can be used, duct can be also used.
Brief description of the drawings
The detailed description made to non-limiting example with reference to the following drawings by reading, further feature of the invention,
Objects and advantages will become more apparent upon：
Fig. 1 is the planar structure schematic diagram of the embodiment of the present invention；
Fig. 2 is the dimensional structure diagram of the embodiment of the present invention 1；
Fig. 3 is the dimensional structure diagram of the embodiment of the present invention 2；
In figure：Propeller 1, propeller installing component 2, head connector 3, sensor mounting block 4, connection support member 5,
Catch and put part 6.
Specific embodiment
With reference to specific embodiment, the present invention is described in detail.Following examples will be helpful to the technology of this area
Personnel further understand the present invention, but the invention is not limited in any way.It should be pointed out that to the ordinary skill of this area
For personnel, without departing from the inventive concept of the premise, various modifications and improvements can be made.These belong to the present invention
Protection domain.
Embodiment 1
As depicted in figs. 1 and 2, a kind of band catches the pouch-type aircraft of playing function, the capture for realizing UAV targets；
Including：Propeller 1, propeller installing component 2, head connector 3, sensor mounting block 4, connection support member 5, catch and put part
6, it is necessary to what is illustrated is：Propeller 1 at this is duct motor, and propeller installing component 2 is duct motor mounting plate, connection branch
Support member 5 is carbon fiber bar, catches and puts part 6 and catch net；Wherein：
The duct motor mounting plate 2 is divided into upper and lower two installing plates, for fixing duct motor 1 and carbon fiber bar 5, its
In：Circular arc portion is provided with duct motor mounting plate 2, for placing duct motor 1 and fixing；
The carbon fiber bar 5 is fine through carbon by pipe clamp by the head and the tail connection composition polygonized structure of duct motor mounting plate 2
Tie up the hole on plate 5 to be fixedly clamped, so as to form the main frame of heretofore described " pouch-type " aircraft；
The two ends of the head connector 3 are fixed by pipe clamp with the carbon fiber bar 5 on polygonized structure one side；Head connects
Fitting 3 is used for fixed winged control device, GPS and data transmission module；
The sensor installing plate 4 is fixed on carbon fiber bar 5 and (polygon positioned at the position relative with head connector 3
On two sides relative in shape structure)；
It is described to catch the center that net 6 is fixed on the carbon fiber bar 5 for constituting each side of polygonized structure and is located at the aircraft.
Used as preferred embodiment, 3 points of the head connector is top plate and lower plywood, top plate and lower plywood
There are multiple mounting holes the left and right sides respectively, for being fixed on carbon fiber bar 5 by pipe clamp；Top plate top is for installing GPS
The rest of receiver, top plate and lower plywood is used to install flight control system and data transmission module.In other embodiment,
Any rigid position of the aircraft can be used as the installation position of flight control system, GPS and data transmission module.
Further, used as a kind of mechanical component, material can be carbon fiber or aluminium alloy to the pipe clamp, play connection and
Fixed effect；Specifically, on the one hand pipe clamp is used to connect duct motor mounting part part and carbon fiber bar, on the other hand for even
Pick a connector and carbon fiber bar.
Used as preferred embodiment, the sensor includes ultrasonic wave, light stream, infrared, barometer, vision sensor.
Used as preferred embodiment, the aircraft be able to can both be led to again by setting the manual aircraft of remote control
The winged control device and sensor for crossing itself carrying are realized automatically controlling.
When the manual aircraft capture target, approached by setting after aircraft vertical takes off described in remote control control
Target, and target is dragged for into the catching in net 6 of the aircraft, then controls the aircraft to make a return voyage, target one that will be captured
Rise and take back ground；When the aircraft is automatically controlled, the carry-on sensor sensing and after capturing target, by flying
Control device autonomous control and close to target, by target acquistion and takes back ground.In certain preferred embodiments, the aircraft
When close to UAV targets, target can be dragged for by fuselage mode of verting and caught in net 6.
When target is delivered, it would be desirable to which the target of dispensing is placed in catching net 6, and the aircraft is with target vertical
Destination is moved to after taking off, target is slowly landed with the aircraft by way of vertical landing, target moved from
After driving the aircraft, the aircraft is controlled to make a return voyage.
Embodiment 2
As shown in figures 1 and 3, a kind of band catches the pouch-type aircraft of playing function, and wherein propeller 1 is filled using rotor power
Put, be a kind of pouch-type aircraft using rotor as power set.
To improve the mechanical strength of the aircraft, double-decker is employed on the basis of embodiment 1, level here
Structure refers to multiple connection support members and constitutes closed polygon structure, two-layer by multiple propeller installing components head and the tail closures
Structure as having two-layer in vertical direction is referred to, Fig. 3 is seen.
Rotor power device is located above or below propeller installing component 2, wherein：Top refers to the aircraft and closes
Close polygonized structure plane vertically upward, lower section is the aircraft polygon closing structure plane vertical downward direction.
The pouch-type flying instrument of the rotor power device is for thrust is big, mobility strong the characteristics of.
It is the mechanical strength for further improving fuselage on the premise of thrust meets requirement, aluminium alloy equally can be used as machine
Body mechanical material, it has the characteristics of processing characteristics is splendid, material is slim and graceful, corrosion resistance is strong, therefore flies as described in this instance
The fuselage material of row device.
Embodiment 3
To improve the capture ability of the aircraft, ultrasonic sensor is carried on sensor installing plate 4 or vision is passed
Sensor, for perceiving landform and object around the aircraft.As shown in Fig. 2 only giving a side senser installing plate 4；
Multiple sensor installing plates 4 can be set on each side of polygonized structure and are used to carry multiple according to demand in specific implementation process
Ultrasonic sensor or vision sensor, the ability for strengthening sensor senses periphery.
Determine ability for realize the aircraft, baroceptor can also be carried on the sensor installing plate 4.
Embodiment 4
In interim and emergent demand, the aircraft can also be used for non-unmanned plane object, and such as birds implement to arrest.Institute
Aircraft is stated through operating hand control to take off vertically, the sensor close to after target by being mounted on sensor installing plate 4 determines
With seizure target, object is caught interior into net is caught.
Embodiment 5
The application scenario of the aircraft captures except said one or multiple unmanned planes, to airflight thing (such as birds)
Outside being captured, can also be put into operation using short distance, light goods and materials is carried out.
Goods and materials dispensing is carried out using aircraft described in embodiment 1, the control of the aircraft is carried out by remote control, this
When, it would be desirable to the target of dispensing is placed in catching and putting part 6, catch put part 6 can also be using catching net；The aircraft is with throwing
Put after target vertical takes off and be moved to destination, target is slowly landed with the aircraft by way of vertical landing.Mesh
Mark is moved after leaving the aircraft, controls the aircraft to make a return voyage.
Specific embodiment of the invention is described above.It is to be appreciated that the invention is not limited in above-mentioned
Particular implementation, those skilled in the art can within the scope of the claims make various deformations or amendments, this not shadow
Sound substance of the invention.
Claims (5)
1. a kind of band catches the pouch-type aircraft of playing function, it is characterised in that including：Propeller, propeller installing component, head
Connector, connection support member, catch and put part and sensor mounting block, wherein：
The propeller installing component is used to install fixed propeller and be fixedly connected support member；
Multiple connection support members pass through the polygonized structure that multiple propeller installing component head and the tail closures constitute closure, i.e. shape
Into bag structure；
The head connector is located at the connection support member on polygonized structure one side；
The sensor mounting block is used to install fixed various kinds of sensors, and sensor mounting block is fixed on connection support member
On；
Described catching is put part and is fixed on the connection support member for constituting each side of polygonized structure and positioned at the aircraft
Center.
2. a kind of band according to claim 1 catches the pouch-type aircraft of playing function, it is characterised in that the propeller is
Duct or rotor power device.
3. a kind of band according to claim 1 catches the pouch-type aircraft of playing function, it is characterised in that the head connection
Part is loaded with flying control device, GPS and data transmission module.
4. a kind of band according to claim 1 catches the pouch-type aircraft of playing function, it is characterised in that the connection support
Part material is carbon fiber or aluminium alloy.
5. a kind of band according to claim any one of 1-4 catches the pouch-type aircraft of playing function, it is characterised in that described
Remote control is manual by setting for aircraft, or the winged control device by aircraft itself carrying and the automatic control of sensor realization
System：
When manual aircraft capture target, by setting after aircraft vertical takes off described in remote control control close to mesh
Mark, and target is dragged for into catching for the aircraft and put in part, then control the aircraft to make a return voyage, the target one that will be captured
Rise and take back ground；When the aircraft is automatically controlled, the carry-on sensor sensing and after capturing target, by flying
Control device autonomous control and close to target, by target acquistion and takes back ground；
When target is delivered, it would be desirable to which the target of dispensing is placed in catching and putting part, and the aircraft is with target vertical
Destination is moved to after taking off, target is slowly landed with the aircraft by way of vertical landing, target moved from
After driving the aircraft, the aircraft is controlled to make a return voyage.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201611065794.5A CN106741889B (en) | 2016-11-28 | 2016-11-28 | Pocket type aircraft with catching and releasing functions |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201611065794.5A CN106741889B (en) | 2016-11-28 | 2016-11-28 | Pocket type aircraft with catching and releasing functions |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN106741889A true CN106741889A (en) | 2017-05-31 |
| CN106741889B CN106741889B (en) | 2020-07-14 |
Family
ID=58902034
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201611065794.5A Active CN106741889B (en) | 2016-11-28 | 2016-11-28 | Pocket type aircraft with catching and releasing functions |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106741889B (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108502176A (en) * | 2018-03-25 | 2018-09-07 | 景遥（上海）信息技术有限公司 | A kind of Intelligent unattended machine catching bird system |
| CN108674628A (en) * | 2018-04-18 | 2018-10-19 | 佛山世寰智能科技有限公司 | A kind of loop configuration tailstock formula vertical take-off and landing unmanned aerial vehicle |
| CN110182390A (en) * | 2019-05-05 | 2019-08-30 | 北京空间飞行器总体设计部 | A kind of reusable space junk flexibility arrests pocket device and arrests method |
| EP3967600A1 (en) * | 2020-09-15 | 2022-03-16 | Livelink Aerospace Ltd | Aerial drone |
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| JP2000199699A (en) * | 1999-01-04 | 2000-07-18 | Yoshio Abe | Flying body catcher employing several sheets of net |
| CN204548516U (en) * | 2015-04-24 | 2015-08-12 | 马鞍山市赛迪智能科技有限公司 | A kind of fixed point air-drop unmanned vehicle system |
| CN105314112A (en) * | 2015-05-13 | 2016-02-10 | 安徽中森管理咨询有限公司 | A multifunctional unmanned aerial vehicle used for fishery |
| CN105501436A (en) * | 2016-03-10 | 2016-04-20 | 上海仪耐新材料科技有限公司 | Portable intelligent anti-unmanned aerial vehicle interception net system |
| DE102015003323A1 (en) * | 2015-03-17 | 2016-09-22 | Bunolma GmbH & Co. KG | Device for catching a flying unmanned aerial vehicle |
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Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2000199699A (en) * | 1999-01-04 | 2000-07-18 | Yoshio Abe | Flying body catcher employing several sheets of net |
| DE102015003323A1 (en) * | 2015-03-17 | 2016-09-22 | Bunolma GmbH & Co. KG | Device for catching a flying unmanned aerial vehicle |
| CN204548516U (en) * | 2015-04-24 | 2015-08-12 | 马鞍山市赛迪智能科技有限公司 | A kind of fixed point air-drop unmanned vehicle system |
| CN105314112A (en) * | 2015-05-13 | 2016-02-10 | 安徽中森管理咨询有限公司 | A multifunctional unmanned aerial vehicle used for fishery |
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Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108502176A (en) * | 2018-03-25 | 2018-09-07 | 景遥（上海）信息技术有限公司 | A kind of Intelligent unattended machine catching bird system |
| CN108674628A (en) * | 2018-04-18 | 2018-10-19 | 佛山世寰智能科技有限公司 | A kind of loop configuration tailstock formula vertical take-off and landing unmanned aerial vehicle |
| CN108674628B (en) * | 2018-04-18 | 2021-07-23 | 佛山世寰智能科技有限公司 | Annular structure tailstock type vertical take-off and landing unmanned aerial vehicle |
| CN110182390A (en) * | 2019-05-05 | 2019-08-30 | 北京空间飞行器总体设计部 | A kind of reusable space junk flexibility arrests pocket device and arrests method |
| EP3967600A1 (en) * | 2020-09-15 | 2022-03-16 | Livelink Aerospace Ltd | Aerial drone |
| GB2598796A (en) * | 2020-09-15 | 2022-03-16 | Livelink Aerospace Ltd | Aerial drone |
| GB2598796B (en) * | 2020-09-15 | 2023-07-26 | Livelink Aerospace Ltd | Aerial drone |
| US11794897B2 (en) | 2020-09-15 | 2023-10-24 | Livelink Aerospace Ltd | Aerial drone |
Also Published As
| Publication number | Publication date |
|---|---|
| CN106741889B (en) | 2020-07-14 |
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