CN206813295U - A kind of unmanned transporter of tower material - Google Patents
A kind of unmanned transporter of tower material Download PDFInfo
- Publication number
- CN206813295U CN206813295U CN201720673806.6U CN201720673806U CN206813295U CN 206813295 U CN206813295 U CN 206813295U CN 201720673806 U CN201720673806 U CN 201720673806U CN 206813295 U CN206813295 U CN 206813295U
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- casing
- gas port
- aileron
- panel
- tower material
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- 238000005452 bending Methods 0.000 claims abstract description 28
- 238000010276 construction Methods 0.000 claims abstract description 11
- 238000009423 ventilation Methods 0.000 abstract description 3
- 238000000034 method Methods 0.000 abstract description 2
- 230000015572 biosynthetic process Effects 0.000 description 4
- 230000006641 stabilisation Effects 0.000 description 4
- 238000011105 stabilization Methods 0.000 description 4
- 238000010586 diagram Methods 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 1
- 238000007789 sealing Methods 0.000 description 1
Abstract
The utility model belongs to unmanned air vehicle technique field, and in particular to a kind of unmanned transporter of tower material, including casing, six ailerons being symmetricly set on casing and the undercarriage being arranged on the downside of casing；Casing includes plate and lower panel above enclosed construction, the left panel and right panel and the front panel and rear board in three face bending structures that are respectively equipped with gas port, the top of left panel and right panel is obliquely installed multiple rows of gas port using its vertical center line as line of symmetry, gas port level height highest of the gas port close to vertical center line is often arranged, the air guide hole site on gas port and right panel on left panel corresponds.The unmanned transporter of tower material can make wind enter casing from side after again from the smooth discharge of other side, casing will not be impacted, and the front panel and rear board of casing are close to streamline construction, also impact of the cross-ventilation to casing can be reduced, make aircraft stabilized flight, smoothly transport article.
Description
Technical field
The utility model belongs to unmanned air vehicle technique field, and in particular to a kind of unmanned transporter of tower material.
Background technology
Unmanned transporter needs stable state of flight, just can guarantee that transport article is unlikely to the meaning for shaking, dropping
Outer situation, especially in the stronger environment of cross-ventilation, the structure of unmanned transporter has certainly to the stability of state of flight
Qualitatively act on.
Utility model content
In order to solve the above-mentioned technical problem, the utility model provides a kind of unmanned transporter of tower material, and it has stable
Flight structure.
The utility model is achieved in that a kind of unmanned transporter of tower material, including：Casing, it is symmetricly set on casing
Six ailerons and the undercarriage that is arranged on the downside of casing；
Wherein, casing include plate and lower panel above enclosed construction, the left panel for being respectively equipped with gas port and right panel,
And front panel and rear board in three face bending structures, the top of the left panel and right panel are symmetrical using its vertical center line
Line is obliquely installed multiple rows of gas port, often arranges gas port level height highest of the gas port close to vertical center line, leading on left panel
Stomata corresponds with the air guide hole site in right panel.
Further, in three face bending structures of the front panel and rear board, the angle between two adjacent surfaces is 110-
130°。
Further, the top of the left panel and right panel is obliquely installed two row's air guides by line of symmetry of its vertical center line
Hole.
Further, the number for often arranging gas port is 5.
Further, there are two stage casings for being symmetricly set on the face bending structure of front panel three in the aileron, there is four
The individual middle part for being symmetricly set on the left panel and right panel.
Further, upper and lower two fixed plates are fixedly installed on the casing, are rolled between two fixed plates by aileron
Overlapping piece connects aileron horn, and aileron folded piece includes two parallel fixed seats, and two fixed plates up and down are connected to by fixed seat
Between, parallel guide chute is set in two parallel fixed seats, bolt sliding bar is set in two guide chutes, at two
The rear side of the guide chute of parallel fixed seat is connected two fixed seats by a connecting rod with holes, position centered on the hole
Put, the bolt sliding bar vertical connection jackscrew, be inserted on the jackscrew after limit spring through the hole of connecting rod, aileron is set
Bar connecting seat is connected by rotating shaft with fixed seat, and semicircle limit fastener is set in connecting seat both sides, and when aileron deploys, bolt is slided
Lever blocks buckle, and carries out spacing.
Further, connection otic placode is set in the outer side-lower of two fixed seats, the aileron horn connecting seat is arranged to round
Barrel structure, the lower section both sides of cylinder have the connection otic placode of triangle, the connection otic placode of triangle and the connection otic placode of fixed seat
After a spiral shell axis connection, connecting seat and fixed seat axis connection are formed, axis and the plane where central plate of connecting seat cylinder have
There is the tilt angle of 3-5 degree.
Further, spacing preiection is set on the downside of the connection otic placode of the triangle, on the inside of the connection otic placode of fixed seat
It is raised spacing in groove when connecting seat folds when rotating with 90 degree of groove.
Further, bolt hole is set on the connecting seat cylinder, be connected by bolt with aileron connecting rod.
Further, the aileron connects propeller by aileron connecting rod, and connecting motor in the aileron connecting rod connects
Female connector, motor connection set are nested into the end of aileron connecting rod, motor connection set connection motor base, and motor is arranged on motor bottom
In seat, motor base sealed connection is nested into motor lower cover by being covered on motor, propeller is fixed on motor by steady pin
Outer rotor on.
Compared with prior art, the utility model has the advantage of the unmanned cargo carrier of tower material provided by the utility model
There is stable flight structure：The one-to-one gas port set on the left panel and right panel of casing, wind can be made from side
Enter after casing again from the smooth discharge of other side, casing will not be impacted, and being bent in three faces for casing is tied
The front panel and rear board of structure can also reduce impact of the cross-ventilation to casing, make aircraft is stable to fly close to streamline construction
OK, article is smoothly transported.
Brief description of the drawings
Fig. 1 is the unmanned conveyor designs schematic diagram of tower material provided by the utility model；
Fig. 2 is the unmanned transporter aileron configuration schematic diagram of tower material provided by the utility model；
Fig. 3 is the structural representation of the aileron folded piece of the unmanned transporter of tower material provided by the utility model.
Embodiment
In order that the purpose of this utility model, technical scheme and advantage are more clearly understood, with reference to embodiments, to this
Utility model is further elaborated.It should be appreciated that specific embodiment described herein is only explaining this practicality
It is new, it is not used to limit the utility model.
Embodiment 1,
With reference to figure 1, the present embodiment provides a kind of unmanned transporter of tower material, including：Casing 1, it is symmetricly set on casing 1
Six ailerons 2 and the undercarriage 3 for being arranged on the downside of casing 1, casing 1 include plate and lower panel, difference above enclosed construction
Left panel and right panel provided with gas port 11 and the front panel and rear board in three face bending structures, left panel and the right side
The top of plate is obliquely installed multiple rows of gas port 11 by line of symmetry of its vertical center line, often arranges the leading close to vertical center line of gas port 11
Porosity levels height highest, the gas port 11 on left panel are corresponded with the position of gas port 11 in right panel, flown
Cheng Zhong, the air-flow of side enters from the gas port of side, and is discharged from the gas port of opposite side, reduces air flow as far as possible and causes
Body vibration, meanwhile, the front panel of three face bending structures and tabular is for example streamlined below can also reduce sky as much as possible
Body is unstable caused by flow of air.
In order to which close to streamlined structure, as the improvement of technical scheme, three faces of front panel and rear board are curved
In folded structure, the angle between two adjacent surfaces is 110-130 °；Optimal is 120 °.
Embodiment 2,
With reference to figure 1, the present embodiment provides a kind of unmanned transporter of tower material, including：Casing 1, it is symmetricly set on casing 1
Six ailerons 2 and the undercarriage 3 for being arranged on the downside of casing 1, casing 1 include plate and lower panel, difference above enclosed construction
Left panel and right panel provided with gas port 11 and the front panel and rear board in three face bending structures, left panel and the right side
The top of plate is obliquely installed multiple rows of gas port 11 by line of symmetry of its vertical center line, often arranges the leading close to vertical center line of gas port 11
Porosity levels height highest, the gas port 11 on left panel are corresponded with the position of gas port 11 in right panel, flown
Cheng Zhong, the air-flow of side enters from the gas port of side, and is discharged from the gas port of opposite side, reduces air flow as far as possible and causes
Body vibration, meanwhile, the front panel of three face bending structures and tabular is for example streamlined below can also reduce sky as much as possible
Body is unstable caused by flow of air.
In order to which close to streamlined structure, as the improvement of technical scheme, three faces of front panel and rear board are curved
In folded structure, the angle between two adjacent surfaces is 110-130 °；Optimal is 120 °.
Because front panel and rear board are three face bending structures, in order to adapt to this structure, left panel and right panel
Top is obliquely installed two row's gas ports 11 by line of symmetry of its vertical center line.In the present embodiment, the number of gas port 11 is often arranged
For 5.
Embodiment 3,
With reference to figure 1 and Fig. 2 is combined, the present embodiment provides a kind of unmanned transporter of tower material, including：Casing 1, it is symmetricly set on
Six ailerons 2 on casing 1 and the undercarriage 3 for being arranged on the downside of casing 1, casing 1 include above enclosed construction plate and under
Panel, the left panel for being respectively equipped with gas port 11 and right panel and the front panel and rear board in three face bending structures, the left side
The top of plate and right panel is obliquely installed multiple rows of gas port 11 by line of symmetry of its vertical center line, often arranges gas port 11 close to vertical
The gas port level height highest of center line, the gas port 11 on left panel correspond with the position of gas port 11 in right panel,
In flight course, the air-flow of side enters from the gas port of side, and is discharged from the gas port of opposite side, reduces air as far as possible
The vibration of body caused by flowing, meanwhile, the front panel of three face bending structures and tabular is for example streamlined below also can be as far as possible
Body caused by ground reduces air flow is unstable.
In order to which close to streamlined structure, as the improvement of technical scheme, three faces of front panel and rear board are curved
In folded structure, the angle between two adjacent surfaces is 110-130 °；Optimal is 120 °.
Because front panel and rear board are three face bending structures, in order to adapt to this structure, left panel and right panel
Top is obliquely installed two row's gas ports 11 by line of symmetry of its vertical center line.In the present embodiment, the number of gas port 11 is often arranged
For 5.
There are two stage casings for being symmetricly set on the face bending structure of front panel three in aileron 2, there are four to be symmetricly set on
The middle part of the left panel and right panel.The symmetrical structure of formation can keep transporting the stabilization of article in aircraft flight
Property.
Embodiment 4,
With reference to figure 1 and Fig. 2, Fig. 3 are combined, the present embodiment provides a kind of unmanned transporter of tower material, including：Casing 1, symmetrically set
Put six on casing 1 ailerons 2 and be arranged on the undercarriage 3 of the downside of casing 1, casing 1 includes plate above enclosed construction
With lower panel, the left panel and right panel and the front panel and rear board in three face bending structures of gas port 11 are respectively equipped with,
The top of left panel and right panel is obliquely installed multiple rows of gas port 11 by line of symmetry of its vertical center line, and it is close often to arrange gas port 11
The gas port level height highest of vertical center line, gas port 11 on left panel and 11 position of gas port one a pair in right panel
Should, in flight course, the air-flow of side enters from the gas port of side, and is discharged from the gas port of opposite side, reduces as far as possible
The vibration of body caused by air flow, meanwhile, the front panel of three face bending structures and tabular is for example streamlined below can also use up
Body caused by possibly reducing air flow is unstable.
In order to which close to streamlined structure, as the improvement of technical scheme, three faces of front panel and rear board are curved
In folded structure, the angle between two adjacent surfaces is 110-130 °；Optimal is 120 °.
Because front panel and rear board are three face bending structures, in order to adapt to this structure, left panel and right panel
Top is obliquely installed two row's gas ports 11 by line of symmetry of its vertical center line.In the present embodiment, the number of gas port 11 is often arranged
For 5.
There are two stage casings for being symmetricly set on the face bending structure of front panel three in aileron 2, there are four to be symmetricly set on
The middle part of the left panel and right panel.The symmetrical structure of formation can keep transporting the stabilization of article in aircraft flight
Property.
Upper and lower two fixed plates 201 are fixedly installed on casing 1, are connected between two fixed plates 201 by aileron folded piece
Aileron horn 211 is connect, aileron folded piece includes two parallel fixed seats 202, and two fixations up and down are connected to by fixed seat 202
Between plate 201, parallel guide chute is set in two parallel fixed seats 202, sets bolt to slide in two guide chutes
Bar 203, two parallel fixed seats 202 guide chute rear side by a connecting rod 204 with holes by two fixed seats
202 are connected, position centered on the hole, the vertical connection jackscrew 205 of bolt sliding bar 203, and limit is inserted on the jackscrew 205
The hole of connecting rod 204 is passed through after the spring of position, sets aileron horn connecting seat 206 to be connected by rotating shaft with fixed seat 202, in connecting seat
206 both sides set semicircle limit fastener, and when aileron 2 deploys, bolt sliding bar 203 blocks buckle, and carries out spacing.
Embodiment 5,
With reference to figure 1 and Fig. 2, Fig. 3 are combined, the present embodiment provides a kind of unmanned transporter of tower material, including：Casing 1, symmetrically set
Put six on casing 1 ailerons 2 and be arranged on the undercarriage 3 of the downside of casing 1, casing 1 includes plate above enclosed construction
With lower panel, the left panel and right panel and the front panel and rear board in three face bending structures of gas port 11 are respectively equipped with,
The top of left panel and right panel is obliquely installed multiple rows of gas port 11 by line of symmetry of its vertical center line, and it is close often to arrange gas port 11
The gas port level height highest of vertical center line, gas port 11 on left panel and 11 position of gas port one a pair in right panel
Should, in flight course, the air-flow of side enters from the gas port of side, and is discharged from the gas port of opposite side, reduces as far as possible
The vibration of body caused by air flow, meanwhile, the front panel of three face bending structures and tabular is for example streamlined below can also use up
Body caused by possibly reducing air flow is unstable.
In order to which close to streamlined structure, as the improvement of technical scheme, three faces of front panel and rear board are curved
In folded structure, the angle between two adjacent surfaces is 110-130 °；Optimal is 120 °.
Because front panel and rear board are three face bending structures, in order to adapt to this structure, left panel and right panel
Top is obliquely installed two row's gas ports 11 by line of symmetry of its vertical center line.In the present embodiment, the number of gas port 11 is often arranged
For 5.
There are two stage casings for being symmetricly set on the face bending structure of front panel three in aileron 2, there are four to be symmetricly set on
The middle part of the left panel and right panel.The symmetrical structure of formation can keep transporting the stabilization of article in aircraft flight
Property.
Upper and lower two fixed plates 201 are fixedly installed on casing 1, are connected between two fixed plates 201 by aileron folded piece
Aileron horn 211 is connect, aileron folded piece includes two parallel fixed seats 202, and two fixations up and down are connected to by fixed seat 202
Between plate 201, parallel guide chute is set in two parallel fixed seats 202, sets bolt to slide in two guide chutes
Bar 203, two parallel fixed seats 202 guide chute rear side by a connecting rod 204 with holes by two fixed seats
202 are connected, position centered on the hole, the vertical connection jackscrew 205 of bolt sliding bar 203, and limit is inserted on the jackscrew 205
The hole of connecting rod 204 is passed through after the spring of position, sets aileron horn connecting seat 206 to be connected by rotating shaft with fixed seat 202, in connecting seat
206 both sides set semicircle limit fastener, and when aileron 2 deploys, bolt sliding bar 203 blocks buckle, and carries out spacing.
As a preferred embodiment, the outer side-lower in two fixed seats 202 sets connection otic placode 207, it is described
Aileron horn connecting seat 206 is arranged to cylindrical structure, and the lower section both sides of cylinder have the connection otic placode 208 of triangle, triangle
After the connection otic placode 207 of connection otic placode 208 and fixed seat is by a spiral shell axis connection, forms connecting seat 206 and connect with the axle of fixed seat 202
Connect, the axis of connecting seat cylinder has the tilt angle of 3-5 degree with plane where central plate.
The downside of connection otic placode 208 of triangle sets spacing preiection 209, has on the inside of the connection otic placode of fixed seat 202
90 degree of groove 210, it is raised spacing in groove when connecting seat 206 folds when rotating.Spiral shell is set on the cylinder of connecting seat 206
Keyhole, it is connected by bolt with aileron connecting rod 211.
Embodiment 6,
With reference to figure 1 and Fig. 2, Fig. 3 are combined, the present embodiment provides a kind of unmanned transporter of tower material, including：Casing 1, symmetrically set
Put six on casing 1 ailerons 2 and be arranged on the undercarriage 3 of the downside of casing 1, casing 1 includes plate above enclosed construction
With lower panel, the left panel and right panel and the front panel and rear board in three face bending structures of gas port 11 are respectively equipped with,
The top of left panel and right panel is obliquely installed multiple rows of gas port 11 by line of symmetry of its vertical center line, and it is close often to arrange gas port 11
The gas port level height highest of vertical center line, gas port 11 on left panel and 11 position of gas port one a pair in right panel
Should, in flight course, the air-flow of side enters from the gas port of side, and is discharged from the gas port of opposite side, reduces as far as possible
The vibration of body caused by air flow, meanwhile, the front panel of three face bending structures and tabular is for example streamlined below can also use up
Body caused by possibly reducing air flow is unstable.
In order to which close to streamlined structure, as the improvement of technical scheme, three faces of front panel and rear board are curved
In folded structure, the angle between two adjacent surfaces is 110-130 °；Optimal is 120 °.
Because front panel and rear board are three face bending structures, in order to adapt to this structure, left panel and right panel
Top is obliquely installed two row's gas ports 11 by line of symmetry of its vertical center line.In the present embodiment, the number of gas port 11 is often arranged
For 5.
There are two stage casings for being symmetricly set on the face bending structure of front panel three in aileron 2, there are four to be symmetricly set on
The middle part of the left panel and right panel.The symmetrical structure of formation can keep transporting the stabilization of article in aircraft flight
Property.
Upper and lower two fixed plates 201 are fixedly installed on casing 1, are connected between two fixed plates 201 by aileron folded piece
Aileron horn 211 is connect, aileron folded piece includes two parallel fixed seats 202, and two fixations up and down are connected to by fixed seat 202
Between plate 201, parallel guide chute is set in two parallel fixed seats 202, sets bolt to slide in two guide chutes
Bar 203, two parallel fixed seats 202 guide chute rear side by a connecting rod 204 with holes by two fixed seats
202 are connected, position centered on the hole, the vertical connection jackscrew 205 of bolt sliding bar 203, and limit is inserted on the jackscrew 205
The hole of connecting rod 204 is passed through after the spring of position, sets aileron horn connecting seat 206 to be connected by rotating shaft with fixed seat 202, in connecting seat
206 both sides set semicircle limit fastener, and when aileron 2 deploys, bolt sliding bar 203 blocks buckle, and carries out spacing.
As a preferred embodiment, the outer side-lower in two fixed seats 202 sets connection otic placode 207, it is described
Aileron horn connecting seat 206 is arranged to cylindrical structure, and the lower section both sides of cylinder have the connection otic placode 208 of triangle, triangle
After the connection otic placode 207 of connection otic placode 208 and fixed seat is by a spiral shell axis connection, forms connecting seat 206 and connect with the axle of fixed seat 202
Connect, the axis of connecting seat cylinder has the tilt angle of 3-5 degree with plane where central plate.
The downside of connection otic placode 208 of triangle sets spacing preiection 209, has on the inside of the connection otic placode of fixed seat 202
90 degree of groove 210, it is raised spacing in groove when connecting seat 206 folds when rotating.Spiral shell is set on the cylinder of connecting seat 206
Keyhole, it is connected by bolt with aileron connecting rod 211.
The aileron 2 connects propeller 212 by aileron connecting rod 211, and connecting motor in the aileron connecting rod 211 connects
Female connector 213, motor connection set 213 are nested into the end of aileron connecting rod 211, and motor connection set 213 connects motor base 214,
Motor is arranged in motor base 214, and being nested into the sealing of motor base 214 by lid on motor 215 and motor lower cover 216 connects
Connect, propeller 212 is fixed on the outer rotor of motor by steady pin 217.
Claims (10)
- A kind of 1. unmanned transporter of tower material, it is characterised in that including：Casing, six ailerons being symmetricly set on casing and The undercarriage being arranged on the downside of casing；Wherein, casing include plate and lower panel above enclosed construction, the left panel for being respectively equipped with gas port and right panel and In the front panel and rear board of three face bending structures, the top of the left panel and right panel is inclined using its vertical center line as line of symmetry Multiple rows of gas port is tiltedly set, often arranges gas port level height highest of the gas port close to vertical center line, the gas port on left panel Corresponded with the air guide hole site in right panel.
- 2. the unmanned transporter of tower material as claimed in claim 1, it is characterised in that the three faces bending of the front panel and rear board In structure, the angle between two adjacent surfaces is 110-130 °.
- 3. the unmanned transporter of tower material as claimed in claim 1, it is characterised in that the top of the left panel and right panel is with it Vertical center line is that line of symmetry is obliquely installed two row's gas ports.
- 4. the unmanned transporter of tower material as claimed in claim 3, it is characterised in that the number for often arranging gas port is 5.
- 5. the unmanned transporter of tower material as claimed in claim 1, it is characterised in that there are two to be symmetricly set on institute in the aileron The stage casing of the face bending structure of front panel three is stated, there are four middle parts for being symmetricly set on the left panel and right panel.
- 6. the unmanned transporter of tower material as claimed in claim 1, it is characterised in that upper and lower two are fixedly installed on the casing Individual fixed plate, connects aileron horn between two fixed plates by aileron folded piece, and aileron folded piece includes two parallel fixations Seat, it is connected to by fixed seat up and down between two fixed plates, parallel guide chute is set in two parallel fixed seats, two Bolt sliding bar is set in individual guide chute, passes through a connection with holes in the rear side of the guide chute of two parallel fixed seats Bar connects two fixed seats, position centered on the hole, the bolt sliding bar vertical connection jackscrew, is inserted on the jackscrew The hole of connecting rod is passed through after limit spring, sets aileron horn connecting seat to be connected by rotating shaft with fixed seat, is set in connecting seat both sides Semicircle limit fastener is put, when aileron deploys, bolt sliding bar blocks buckle, and carries out spacing.
- 7. the unmanned transporter of tower material as claimed in claim 6, it is characterised in that set and connect in the outer side-lower of two fixed seats Ear connecting plate, the aileron horn connecting seat are arranged to cylindrical structure, and the lower section both sides of cylinder have the connection otic placode of triangle, triangle After the connection otic placode of shape and the connection otic placode of fixed seat are by a spiral shell axis connection, connecting seat and fixed seat axis connection, connection are formed The axis of seat cylinder has the tilt angle of 3-5 degree with plane where central plate.
- 8. the unmanned transporter of tower material as claimed in claim 7, it is characterised in that set on the downside of the connection otic placode of the triangle Spacing preiection, there is 90 degree of groove on the inside of the connection otic placode of fixed seat, it is raised spacing when connecting seat folds when rotating In groove.
- 9. the unmanned transporter of tower material as claimed in claim 7, it is characterised in that bolt hole is set on the connecting seat cylinder, It is connected by bolt with aileron connecting rod.
- 10. the unmanned transporter of tower material as claimed in claim 6, it is characterised in that the aileron is connected by aileron connecting rod Propeller, motor connection set is connected in the aileron connecting rod, motor connection set is nested into the end of aileron connecting rod, and motor connects Female connector connects motor base, and motor is arranged in motor base, and it is close to be nested into motor base by lid and motor lower cover on motor Envelope connection, propeller are fixed on the outer rotor of motor by steady pin.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720673806.6U CN206813295U (en) | 2017-06-12 | 2017-06-12 | A kind of unmanned transporter of tower material |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720673806.6U CN206813295U (en) | 2017-06-12 | 2017-06-12 | A kind of unmanned transporter of tower material |
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| Publication Number | Publication Date |
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| CN206813295U true CN206813295U (en) | 2017-12-29 |
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| CN201720673806.6U Active CN206813295U (en) | 2017-06-12 | 2017-06-12 | A kind of unmanned transporter of tower material |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107097932A (en) * | 2017-06-12 | 2017-08-29 | 国网辽宁省电力有限公司辽阳供电公司 | A kind of unmanned transporter of tower material |
| CN108163182A (en) * | 2018-02-24 | 2018-06-15 | 高琴 | A kind of folding deinsectization unmanned plane |
-
2017
- 2017-06-12 CN CN201720673806.6U patent/CN206813295U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107097932A (en) * | 2017-06-12 | 2017-08-29 | 国网辽宁省电力有限公司辽阳供电公司 | A kind of unmanned transporter of tower material |
| CN108163182A (en) * | 2018-02-24 | 2018-06-15 | 高琴 | A kind of folding deinsectization unmanned plane |
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