CN110697021A - Unmanned aerial vehicle is folded in lightweight - Google Patents
Unmanned aerial vehicle is folded in lightweight Download PDFInfo
- Publication number
- CN110697021A CN110697021A CN201911017620.5A CN201911017620A CN110697021A CN 110697021 A CN110697021 A CN 110697021A CN 201911017620 A CN201911017620 A CN 201911017620A CN 110697021 A CN110697021 A CN 110697021A
- Authority
- CN
- China
- Prior art keywords
- plate
- horn
- hangers
- curb plate
- bottom plate
- 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.)
- Pending
Links
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/30—Parts of fuselage relatively movable to reduce overall dimensions of aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Remote Sensing (AREA)
- Road Signs Or Road Markings (AREA)
Abstract
The invention provides a light-weight folding unmanned aerial vehicle which comprises a central body and a horn, wherein the horn is detachably connected with the central body, the horn is uniformly arranged along the circumference of the central body, the horn can be folded, the central body comprises an upper plate and a bottom plate, the upper plate and the bottom plate are rectangular, the upper plate and the bottom plate are fixedly connected through aluminum columns, a plurality of side plates are arranged between the upper plate and the bottom plate, the side plates are respectively inserted with the upper plate and the bottom plate, and the upper plate is provided with an upper limiting block inserted with the horn and protrudes outwards. The central body passes through the horn and connects undercarriage and motor, and holistic atress situation has effectively been improved to boxlike central body, has increased under the condition of few weight, very big increase the intensity of structure, folding horn simple structure, the convenience that opens and shuts has wholly alleviateed whole unmanned aerial vehicle's weight to unmanned aerial vehicle's duration has been improved.
Description
Technical Field
The invention relates to the field of unmanned aerial vehicles, in particular to a lightweight folding unmanned aerial vehicle.
Background
The unmanned aerial vehicle is an unmanned aerial vehicle operated by using a wireless remote control device and a self-contained program control device. Unmanned aerial vehicles are in fact a general term for unmanned aerial vehicles, and can be defined from a technical perspective as follows: unmanned fixed wing aircraft, unmanned VTOL aircraft, unmanned airship, unmanned helicopter, unmanned multi-rotor aircraft, etc. Unmanned planes tend to be more suitable for tasks that are too "fool, dirty, or dangerous" than manned planes. Unmanned aerial vehicles can be classified into military and civilian applications according to the application field. For military use, unmanned aerial vehicles divide into reconnaissance aircraft and target drone. In the civil aspect, the application of the unmanned aerial vehicle industry is really just needed by the unmanned aerial vehicle; at present, the unmanned aerial vehicle is applied to the fields of aerial photography, agriculture, plant protection, miniature self-timer, express transportation, disaster relief, wild animal observation, infectious disease monitoring, surveying and mapping, news reporting, power inspection, disaster relief, film and television shooting and the like, the application of the unmanned aerial vehicle is greatly expanded, and developed countries actively expand industrial application and develop unmanned aerial vehicle technology.
In recent years, with the development of the unmanned aerial vehicle market, the multi-rotor unmanned aerial vehicle rapidly gains attention of the broad consumer groups with the advantages of excellent control performance, convenience in vertical take-off and landing and the like, and becomes the most popular product so far. The weight of the whole organism of current many rotor unmanned aerial vehicle is too big, has restricted unmanned aerial vehicle's load and continuation of the journey to make unmanned aerial vehicle's cost and weight increase substantially. In order to make more convenient transportation and storage of unmanned aerial vehicle, folding research and development and use have been carried out to the unmanned aerial vehicle horn, and the durability and the weight problem of folding unmanned aerial vehicle horn become the technical problem that the urgent need was solved.
Disclosure of Invention
The invention aims to overcome the defects of the traditional technology and provide a light-weight folding unmanned aerial vehicle.
The aim of the invention is achieved by the following technical measures: the utility model provides a folding unmanned aerial vehicle of lightweight, includes central body and horn, the horn with the connection can be dismantled to the central body, the horn is followed the circumference of central body evenly sets up, the collapsible setting of horn, its characterized in that: the central body includes upper plate and bottom plate, upper plate and bottom plate are the rectangle, through aluminium post fixed connection between upper plate and the bottom plate, still be equipped with a plurality of curb plates between upper plate and the bottom plate, it is a plurality of the curb plate respectively with upper plate and bottom plate are pegged graft, and are a plurality of the curb plate sets up four limits departments at the upper plate of rectangle and bottom plate, the upper plate be equipped with the last spacing piece that the horn was pegged graft, go up the setting of spacing piece in four angle departments of upper plate, and outside outstanding setting.
The central body passes through the horn and connects undercarriage and motor, and holistic atress situation has effectively been improved to boxlike central body, has increased under the condition of few weight, very big increase the intensity of structure, folding horn simple structure, the convenience that opens and shuts has wholly alleviateed whole unmanned aerial vehicle's weight to unmanned aerial vehicle's duration has been improved.
As a preferred scheme, the upper plate is provided with a plurality of upper connecting holes, the side plate is provided with an upper connecting block connected with the upper connecting holes, the bottom plate is provided with a plurality of lower connecting holes, the side plate is provided with a lower connecting block connected with the lower connecting holes, and the upper connecting block and the lower connecting block are both provided with a plurality of connecting holes.
As a preferred scheme, the lateral plate comprises two transverse supporting rods and two longitudinal supporting rods, two ends of each longitudinal supporting rod are fixed to the two transverse supporting rods respectively, and the longitudinal supporting rods and the transverse supporting rods form a lateral plate ventilation frame.
As a preferred scheme, the upper plate, the bottom plate and the side plates form a circuit bin in a surrounding mode, the upper plate is provided with a circuit mounting opening, the circuit mounting opening is formed in the middle of the upper plate, the bottom plate is provided with a plurality of bottom plate ventilation areas, and the circuit bin is communicated with the outside through the bottom plate ventilation areas.
As a preferred scheme, the horn includes first organism curb plate, second organism curb plate, first horn curb plate, second horn curb plate and side pipe, first organism curb plate and second organism curb plate size equals, and the shape is the same, first horn curb plate equals with the second horn curb plate size, and the shape is the same, first organism curb plate, second organism curb plate with first horn curb plate, second horn curb plate rotatable coupling, side pipe with first horn curb plate and second horn curb plate fixed connection.
As a preferred scheme, the first machine body side plate and the second machine body side plate are both provided with an upper machine body connecting block and a lower machine body connecting block, the upper plate is provided with an upper connecting hole corresponding to the upper machine body connecting block, the bottom plate is provided with a lower connecting hole corresponding to the lower machine body connecting block, the upper machine body connecting block is inserted in the upper connecting hole, and the lower machine body connecting block is inserted in the lower connecting hole.
As a preferred scheme, the first machine arm side plate and the second machine arm side plate are arranged between the first machine body side plate and the second machine body side plate, and the upper parts of the first machine arm side plate and the second machine arm side plate are provided with limit grooves corresponding to the upper limit blocks.
As a preferred scheme, first organism curb plate is equipped with first hangers, second organism curb plate is equipped with the second hangers, first horn curb plate is equipped with the third hangers, the second horn curb plate is equipped with the fourth hangers, first hangers and third hangers correspond the setting, second hangers and fourth hangers correspond the setting.
As a preferred scheme, first hangers sets up the outside lower part of first organism curb plate, first hangers is equipped with first hangers connecting hole, the second hangers sets up the outside lower part of second organism curb plate, the second hangers is equipped with the second hangers connecting hole, the third hangers sets up the outside lower part of first horn curb plate, the third hangers is equipped with the third hangers connecting hole, the fourth hangers sets up the outside lower part of second horn curb plate, the fourth hangers is equipped with the fourth hangers connecting hole, first hangers connecting hole, second hangers connecting hole, third hangers connecting hole and fourth hangers connecting hole are connected through the hinge.
As a preferred scheme, be equipped with horn upper plate and horn bottom plate between first horn curb plate and the second horn curb plate, the both sides that the horn upper plate is relative are equipped with first horn upper plate connecting block and second horn upper plate connecting block respectively, the both sides that the horn bottom plate is relative are equipped with first horn bottom plate connecting block and second horn bottom plate connecting block respectively, first horn curb plate be equipped with the first horn side plate connecting hole that first horn upper plate connecting block corresponds, first horn curb plate be equipped with the second horn curb plate connecting hole that second horn upper plate connecting block corresponds, the second horn curb plate be equipped with the first horn side plate connecting hole that first horn bottom plate connecting block corresponds, the second horn curb plate be equipped with the second horn side plate connecting hole that second horn bottom plate connecting block corresponds.
Due to the adoption of the technical scheme, compared with the prior art, the invention has the advantages that: the invention provides a lightweight folding unmanned aerial vehicle, which is characterized in that a combined box-shaped central body and a combined arm are arranged, so that the weight of the unmanned aerial vehicle is reduced to a great extent, the strength of the whole unmanned aerial vehicle is ensured, the whole weight of the unmanned aerial vehicle is reduced, and the load carrying capacity and the cruising capacity of the unmanned aerial vehicle are greatly improved.
The invention is further described with reference to the following figures and detailed description.
Drawings
Fig. 1 is a schematic structural diagram of a central body and a horn of a lightweight folding unmanned aerial vehicle according to the invention.
Fig. 2 is a schematic structural diagram of a boom of a lightweight folding unmanned aerial vehicle according to the present invention.
Fig. 3 is a schematic structural diagram of a first body side plate of the lightweight folding unmanned aerial vehicle.
Fig. 4 is a schematic structural view of a first arm side plate and a second arm side plate of the lightweight folding unmanned aerial vehicle.
Fig. 5 is a schematic diagram of an upper plate structure of a lightweight folding unmanned aerial vehicle according to the invention.
Fig. 6 is a schematic structural diagram of a bottom plate of the lightweight folding unmanned aerial vehicle.
Fig. 7 is a side plate structure schematic diagram of the lightweight folding unmanned aerial vehicle.
Detailed Description
Example (b): as shown in fig. 1-7, a folding unmanned aerial vehicle of lightweight, including central body and horn 2, horn 2 with the connection can be dismantled to the central body, horn 2 follows the circumference of central body evenly sets up, the collapsible setting of horn 2, its characterized in that: the central body includes upper plate 11 and bottom plate 12, upper plate 11 and bottom plate 12 are the rectangle, through aluminium column fixed connection between upper plate 11 and the bottom plate 12, still be equipped with a plurality of curb plates 14 between upper plate 11 and the bottom plate 12, it is a plurality of curb plate 14 respectively with upper plate 11 and bottom plate 12 are pegged graft, and are a plurality of curb plate 14 sets up four limits departments at the upper plate 11 of rectangle and bottom plate 12, upper plate 11 be equipped with last spacing piece 113 that horn 2 was pegged graft, go up spacing piece 113 setting in four corners departments of upper plate 11, and outside outstanding setting. The central body passes through the horn and connects undercarriage and motor, and holistic atress situation has effectively been improved to boxlike central body, has increased under the condition of few weight, very big increase the intensity of structure, folding horn simple structure, the convenience that opens and shuts has wholly alleviateed whole unmanned aerial vehicle's weight to unmanned aerial vehicle's duration has been improved. Holistic upper plate 11, box-like structure is constituteed to bottom plate 12 and curb plate 14, connection between upper plate 11 and the bottom plate 12 introduces curb plate 14 and strengthens, make whole mechanism become a confined cube, compare in the central body structure that does not have the curb plate before, holistic atress condition can effectively be improved to the confined cube, few weight has been increased, promptly under the condition of curb plate weight, very big increase the intensity of structure, use the aluminium columnar connection between upper plate and the bottom plate, make the connection between curb plate and upper plate and the bottom plate can not loosen and take off, whole formation is reliable enclosed construction.
As shown in fig. 4, 5 and 6, the upper plate 11 is provided with a plurality of upper connection holes 111, the side plate 14 is provided with an upper connection block 141 connected to the upper connection holes 111, the bottom plate 12 is provided with a plurality of lower connection holes 121, the side plate 14 is provided with a lower connection block 142 connected to the lower connection holes 121, and the upper connection block 141 and the lower connection block 142 are provided in plurality. The upper plate 11 and the side plate 14 are connected by the connection of the plurality of upper connection holes 111 and the upper connection blocks 141, and the bottom plate 12 and the side plate 14 are connected by the connection of the plurality of lower connection holes 121 and the lower connection blocks 142, reducing the use of connection members. Upper plate 11 still is equipped with aluminium post connecting hole 115, and bottom plate 12 is equipped with down aluminium post connecting hole 124, and the aluminium post is equipped with internal screw thread aluminium system connecting rod for both ends, puts the aluminium post between upper plate 11 and bottom plate 12, sees through the upper end of aluminium post connecting hole 115 and aluminium post through the screw and is connected, and the screw sees through down aluminium post connecting hole 124 and is connected with the lower extreme of aluminium post, realizes the fixed connection of aluminium post and upper plate 11 and bottom plate 12.
As shown in fig. 7, the side panel 14 includes two transverse support bars 143 and two longitudinal support bars 144, two ends of the two transverse support bars 143 are respectively fixed to the two transverse support bars 144, and the longitudinal support bars 144 and the transverse support bars 143 form a side panel ventilation frame 145. The side panel ventilation frame 145 is used for heat dissipation and ventilation. The lateral support bar 143 and the longitudinal support bar 144 constitute the side panel 14, so that the side panel 14 can provide effective support while maximally reducing its weight.
As shown in fig. 1, the upper plate 11, the bottom plate 12 and the side plates 14 enclose a circuit cabin 13, and the circuit cabin 13 is used for accommodating a circuit used by the unmanned aerial vehicle. The upper plate 11 is provided with a circuit mounting port 114, and the circuit mounting port 114 is arranged in the middle of the upper plate 11. As shown in fig. 6, the bottom plate 12 is provided with a plurality of bottom plate ventilation areas 123, and the circuit compartment 13 is communicated with the outside by the bottom plate ventilation areas 123. The bottom plate ventilation area 123 is used for heat dissipation and ventilation of the circuit. The bottom plate 11 still is equipped with launcher connecting hole 125, and launcher connecting hole 125 sets up and is equipped with two sets ofly, sets up respectively in the relative both sides of bottom plate 12, and a set of launcher that is used for fixed connection unmanned aerial vehicle, another group are used for fixed connection unmanned aerial vehicle's acceptance device.
As shown in fig. 1 and 2, the boom 2 includes a first boom side plate 21, a second boom side plate 22, a first boom side plate 23, a second boom side plate 24, and a square pipe 27, the first boom side plate 21 and the second boom side plate 22 have the same size and the same shape, the first boom side plate 23 and the second boom side plate 24 have the same size and the same shape, the first boom side plate 21, the second boom side plate 22, the first boom side plate 23 and the second boom side plate 24 are rotatably connected, and the square pipe 27 is fixedly connected to the first boom side plate 23 and the second boom side plate 24. Both ends of square pipe 27 are equipped with curb plate connecting hole and undercarriage connecting hole 271 respectively, and the curb plate connecting hole is used for connecting first horn curb plate 23 and second horn curb plate 24, and through bolt fixed connection, undercarriage connecting hole 271 is used for connecting the undercarriage, also is through bolt fixed connection. By adopting the combined folding horn, a large space is reserved inside the whole horn, so that materials used for the horn can be saved on the basis of convenient adjustment, and the weight of the whole unmanned aerial vehicle is reduced. In this embodiment, the horn is equipped with four groups, sets up respectively in the adjacent department that supports four strongest curb plates for the horn is more firm.
As shown in fig. 3 and 5 and 6, the first body side plate 21 and the second body side plate 22 are both provided with an upper body connecting block 213 and a lower body connecting block 212, the upper plate 11 is provided with an upper connecting hole 111 corresponding to the upper body connecting block 213, the bottom plate 12 is provided with a lower connecting hole 121 corresponding to the lower body connecting block 212, the upper body connecting block 213 is inserted into the upper connecting hole 111, and the lower body connecting block 212 is inserted into the lower connecting hole 121. Through connecting block 213 and last connecting hole 111 on the organism of mutually supporting, connecting block 212 and lower connecting hole 121 under the organism for first horn curb plate 23 and second horn curb plate 24 and upper plate 11 and bottom plate 12 fixed connection, it is convenient, firm to connect, have reduced the use of connecting piece, play the supporting role to whole structure again simultaneously, can increase whole unmanned aerial vehicle's atress.
As shown in fig. 2 and 4, the first arm side plate 23 and the second arm side plate 24 are disposed between the first body side plate 21 and the second body side plate 22, and the upper portions of the first arm side plate 23 and the second arm side plate 24 are provided with a stopper groove 28 corresponding to the upper stopper 113. As shown in fig. 1 and fig. 2, the upper limiting block 113 is provided with a protective plate mounting hole 116 for mounting a protective plate, after the whole unmanned aerial vehicle is mounted, the protective plate is protected to be mounted on the outer side of the upper plate through the protective plate mounting hole and a knob matched with the protective plate, the upper limiting block 113 is mounted at one end of the limiting groove 28, so that the first arm side plate 23 and the second arm side plate 24 can rotate, and the mounting and the use of the protective plate mounted on the upper limiting block 113 cannot be influenced.
As shown in fig. 2, 3 and 4, the first body side plate 21 is provided with a first hanging lug 211, the second body side plate 22 is provided with a second hanging lug, the first arm side plate 23 is provided with a third hanging lug 231, the second arm side plate 24 is provided with a fourth hanging lug, the first hanging lug 211 and the third hanging lug 231 are correspondingly arranged, and the second hanging lug and the fourth hanging lug are correspondingly arranged. First hangers 211 sets up the outside lower part of first organism curb plate 21, first hangers 211 is equipped with first hangers connecting hole 214, the second hangers sets up the outside lower part of second organism curb plate, the second hangers is equipped with the second hangers connecting hole, third hangers 231 sets up the outside lower part of first horn curb plate 23, third hangers 231 is equipped with third hangers connecting hole 232, the fourth hangers sets up the outside lower part of second horn curb plate, the fourth hangers is equipped with the fourth hangers connecting hole, first hangers connecting hole, second hangers connecting hole, third hangers connecting hole and fourth hangers connecting hole are connected through hinge 3. First hangers and second hangers set up on fixed first organism curb plate and second organism curb plate, consequently also fixed the setting, and third hangers and fourth hangers set up on first horn curb plate and second horn curb plate, and four hangers pass through hinge 2 and connect, and consequently third hangers and fourth hangers can be followed hinge 3 and rotated.
As shown in fig. 3, first organism curb plate 21 still is equipped with inward recess 216 in the one end that is close to the central body, and the middle part of first organism curb plate 21 still is equipped with two first through-holes 215, because of whole unmanned aerial vehicle's the bearing that hangs is mainly born by the central body, consequently first organism curb plate 21 only regards as the connection use, it can satisfy the demand to need not too big intensity, recess and first through-hole have reduced the material of first organism curb plate on the basis of having guaranteed first organism curb plate basis function, whole unmanned aerial vehicle's weight has alleviateed promptly, provide very big help for continuation of the journey and load, relative second organism curb plate also has the same setting, give unnecessary details. As shown in fig. 4, the first arm side plate 23 has a second through hole 233 at the middle thereof, and the second through hole acts on the first through hole in the same manner, which is not described again.
As shown in fig. 2 and 4, an upper boom plate 25 and a lower boom plate 26 are arranged between the first boom side plate 23 and the second boom side plate 24, two opposite sides of the upper boom plate 24 are respectively provided with a first upper boom plate connecting block and a second upper boom plate connecting block, two opposite sides of the lower boom plate are respectively provided with a first lower boom plate connecting block and a second lower boom plate connecting block, the first boom side plate is provided with a first boom side plate connecting hole corresponding to the first upper boom plate connecting block, the first boom side plate is provided with a second boom side plate connecting hole corresponding to the second upper boom plate connecting block, the second boom side plate is provided with a first boom side plate connecting hole corresponding to the first boom plate connecting block, and the second boom side plate is provided with a second boom side plate connecting hole corresponding to the second boom plate connecting block. The upper arm plate 25 and the lower arm plate 26 make the entire arm structure more stable. A folding buckle 251 is further disposed on the upper plate 25, a folding buckle gasket 252 is further disposed outside the folding buckle 251, and the folding buckle 251 is used for enabling the whole boom 2 to be folded. The folding buckle gasket 252 is used for protecting the folding buckle 251, and the folding buckle 251 and the folding buckle gasket 252 are connected to the first boom side plate 23 and the second boom side plate 24 in an inserting manner, specifically, refer to a method for connecting the boom upper plate and the boom base plate to the first boom side plate and the second boom side plate.
Claims (10)
1. The utility model provides a folding unmanned aerial vehicle of lightweight, includes central body and horn, the horn with the connection can be dismantled to the central body, the horn is followed the circumference of central body evenly sets up, the collapsible setting of horn, its characterized in that: the central body includes upper plate and bottom plate, upper plate and bottom plate are the rectangle, through aluminium post fixed connection between upper plate and the bottom plate, still be equipped with a plurality of curb plates between upper plate and the bottom plate, it is a plurality of the curb plate respectively with upper plate and bottom plate are pegged graft, and are a plurality of the curb plate sets up four limits departments at the upper plate of rectangle and bottom plate, the upper plate be equipped with the last spacing piece that the horn was pegged graft, go up the setting of spacing piece in four angle departments of upper plate, and outside outstanding setting.
2. The folding unmanned aerial vehicle of lightweight of claim 1, characterized in that: the upper plate is provided with a plurality of upper connecting holes, the side plate is provided with an upper connecting block connected with the upper connecting holes, the bottom plate is provided with a plurality of lower connecting holes, the side plate is provided with a lower connecting block connected with the lower connecting holes, and the upper connecting block and the lower connecting block are both provided with a plurality of connecting holes.
3. The folding unmanned aerial vehicle of claim 2, characterized in that: the lateral plate comprises two transverse supporting rods and two longitudinal supporting rods, the two ends of each longitudinal supporting rod are fixed to the two transverse supporting rods respectively, and the longitudinal supporting rods and the transverse supporting rods form a lateral plate ventilation frame.
4. The folding unmanned aerial vehicle of one of claims 1 to 3, characterized in that: the circuit bin is defined by the upper plate, the bottom plate and the side plates, the circuit bin is formed by the upper plate, the bottom plate and the side plates in a surrounding mode, the circuit mounting port is formed in the middle of the upper plate, the bottom plate is provided with a plurality of bottom plate ventilation areas, and the circuit bin is communicated with the outside through the bottom plate ventilation areas.
5. The folding unmanned aerial vehicle of lightweight of claim 1, characterized in that: the horn includes first organism curb plate, second organism curb plate, first horn curb plate, second horn curb plate and side pipe, first organism curb plate and second organism curb plate size equals, and the shape is the same, first horn curb plate and second horn curb plate size equals, and the shape is the same, first organism curb plate, second organism curb plate with first horn curb plate, second horn curb plate rotatable coupling, side pipe with first horn curb plate and second horn curb plate fixed connection.
6. The folding unmanned aerial vehicle of lightweight of claim 5, characterized in that: the first machine body side plate and the second machine body side plate are both provided with a machine body upper connecting block and a machine body lower connecting block, the upper plate is provided with an upper connecting hole corresponding to the machine body upper connecting block, the bottom plate is provided with a lower connecting hole corresponding to the machine body lower connecting block, the machine body upper connecting block is inserted into the upper connecting hole, and the machine body lower connecting block is inserted into the lower connecting hole.
7. The folding unmanned aerial vehicle of claim 6, characterized in that: the first machine arm side plate and the second machine arm side plate are arranged between the first machine body side plate and the second machine body side plate, and limiting grooves corresponding to the upper limiting blocks are formed in the upper portions of the first machine arm side plate and the second machine arm side plate.
8. The folding unmanned aerial vehicle of lightweight of claim 7, characterized in that: first organism curb plate is equipped with first hangers, second organism curb plate is equipped with the second hangers, first arm curb plate is equipped with the third hangers, the second horn curb plate is equipped with the fourth hangers, first hangers and third hangers correspond the setting, second hangers and fourth hangers correspond the setting.
9. The folding unmanned aerial vehicle of claim 8, characterized in that: first hangers sets up the outside lower part of first organism curb plate, first hangers is equipped with first hangers connecting hole, the second hangers sets up the outside lower part of second organism curb plate, the second hangers is equipped with the second hangers connecting hole, the third hangers sets up the outside lower part of first horn curb plate, the third hangers is equipped with the third hangers connecting hole, the fourth hangers sets up the outside lower part of second horn curb plate, the fourth hangers is equipped with the fourth hangers connecting hole, first hangers connecting hole, second hangers connecting hole, third hangers connecting hole and fourth hangers connecting hole pass through the hinge and connect.
10. The folding unmanned aerial vehicle of one of claims 5-9, characterized in that: be equipped with horn upper plate and horn bottom plate between first horn curb plate and the second horn curb plate, the both sides that the horn upper plate is relative are equipped with first horn upper plate connecting block and second horn upper plate connecting block respectively, the both sides that the horn bottom plate is relative are equipped with first horn bottom plate connecting block and second horn bottom plate connecting block respectively, first horn curb plate be equipped with the first horn side plate connecting hole that first horn upper plate connecting block corresponds, first horn side plate be equipped with the second horn curb plate connecting hole that second horn upper plate connecting block corresponds, the second horn curb plate be equipped with the first horn side plate connecting hole that first horn bottom plate connecting block corresponds, the second horn curb plate be equipped with the second horn side plate connecting hole that second horn bottom plate connecting block corresponds.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201911017620.5A CN110697021A (en) | 2019-10-24 | 2019-10-24 | Unmanned aerial vehicle is folded in lightweight |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201911017620.5A CN110697021A (en) | 2019-10-24 | 2019-10-24 | Unmanned aerial vehicle is folded in lightweight |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN110697021A true CN110697021A (en) | 2020-01-17 |
Family
ID=69201143
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201911017620.5A Pending CN110697021A (en) | 2019-10-24 | 2019-10-24 | Unmanned aerial vehicle is folded in lightweight |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN110697021A (en) |
Citations (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN205022844U (en) * | 2015-09-30 | 2016-02-10 | 湖南云顶智能科技有限公司 | Unmanned aerial vehicle horn folding mechanism and unmanned aerial vehicle |
| CN107521685A (en) * | 2017-09-20 | 2017-12-29 | 首航国翼（武汉）科技有限公司 | Foldable multiaxis unmanned plane |
-
2019
- 2019-10-24 CN CN201911017620.5A patent/CN110697021A/en active Pending
Patent Citations (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN205022844U (en) * | 2015-09-30 | 2016-02-10 | 湖南云顶智能科技有限公司 | Unmanned aerial vehicle horn folding mechanism and unmanned aerial vehicle |
| CN107521685A (en) * | 2017-09-20 | 2017-12-29 | 首航国翼（武汉）科技有限公司 | Foldable multiaxis unmanned plane |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US20170291677A1 (en) | Folding heavy-lift unmanned aerial vehicle frame | |
| CN111619783A (en) | Unmanned aerial vehicle with collapsible unmanned aerial vehicle support piece | |
| US20220227485A1 (en) | Unmanned aerial vehicle folding landing gear | |
| CN206446791U (en) | A kind of police unmanned plane of many rotors | |
| CN209097009U (en) | A kind of damping device of unmanned plane during flying device | |
| CN110733649A (en) | anti-interference lightweight unmanned aerial vehicle | |
| CN110697020A (en) | Unmanned aerial vehicle lightweight folding frame | |
| CN111703575B (en) | Multifunctional unmanned aerial vehicle | |
| CN110697021A (en) | Unmanned aerial vehicle is folded in lightweight | |
| CN207482211U (en) | A kind of unmanned plane landing stage apparatus | |
| CN216834262U (en) | Big load foldable six-rotor unmanned aerial vehicle | |
| CN106428549A (en) | Carrying device for unmanned aerial vehicle | |
| CN217199501U (en) | Box storage and transportation device of unmanned aerial vehicle | |
| CN206218217U (en) | A kind of eight rotor electric power unwrapping wire unmanned planes | |
| CN209889129U (en) | Scalable comprehensive protection device of unmanned aerial vehicle | |
| CN111806692B (en) | Commodity circulation transportation unmanned aerial vehicle | |
| CN211032987U (en) | Many rotor unmanned aerial vehicle centrum of lightweight | |
| CN213735537U (en) | Scalable horn and scalable unmanned aerial vehicle of horn | |
| CN211568295U (en) | Unmanned aerial vehicle with distribution function | |
| CN108528741A (en) | A kind of drop-proof Aerial photography unmanned plane | |
| CN210503909U (en) | Convenient portable unmanned aerial vehicle anticollision shock attenuation transport case | |
| CN216509162U (en) | Unmanned aerial vehicle platform that takes off and land for hydraulic engineering | |
| CN206307271U (en) | A kind of unmanned plane uses carrying device | |
| CN206087285U (en) | Long -range delivery of goods unmanned aerial vehicle | |
| CN214729757U (en) | Remote control's intelligent unmanned aerial vehicle machine nest |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20200117 |
|
| RJ01 | Rejection of invention patent application after publication |