CN207853356U - A kind of the wiring constructional device and its unmanned plane of unmanned plane - Google Patents

A kind of the wiring constructional device and its unmanned plane of unmanned plane Download PDF

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Publication number
CN207853356U
CN207853356U CN201720805587.2U CN201720805587U CN207853356U CN 207853356 U CN207853356 U CN 207853356U CN 201720805587 U CN201720805587 U CN 201720805587U CN 207853356 U CN207853356 U CN 207853356U
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China
Prior art keywords
wiring
support
wiring groove
cable
control device
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CN201720805587.2U
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Chinese (zh)
Inventor
钟志锋
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Guangzhou Tudao Information Technolony Co ltd
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Guangzhou Tudao Information Technolony Co ltd
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Priority to CN201720805587.2U priority Critical patent/CN207853356U/en
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Abstract

The utility model provides a kind of wiring structure, including control device, support device, motor, cable, wherein the support device is fixedly connected with control device 1, the support device further includes support portion, support ring, support column, supporting rod, and the support ring is connected on support portion;Described support column one end is fixed on support portion, and the other end is connected on the motor;Described supporting rod one end is connected on the motor, and the other end is connected in the support ring;The support column is equipped with support column wiring groove, and the support column wiring groove penetrates through entire supporting rod in the longitudinal direction, and wherein one section of the cable is arranged in the support column wiring groove;Cable (5) draws out of control device (1) and is connected to motor (3), or one end of cable is electrically connected by electric connector with the control device (1), and another section of cable is electrically connected with the motor (3).By the utility model, the heat-sinking capability of equipment is substantially increased.

Description

A kind of the wiring constructional device and its unmanned plane of unmanned plane
Technical field
The utility model is related to cable laying, more particularly to a kind of unmanned plane wiring structure.
Background technology
Currently, the wiring of unmanned plane in the prior art is typically that cable is laid in inside sealing structure, it is entire nobody The agent structure of machine be it is integrated, it is non-removable.As a result, for small-sized or miniature drone caused by such a structure For, the heat that cable generates will can not ignore, as a result, heat can not distribute caused by excessive heat, unmanned plane It can not flying for long time.However, if directly that cable is exposed outside, caused result will be that cable is easily damaged.
Invention content
The technical problem to be solved by the utility model is to provide a kind of unmanned plane wiring structures, to solve the prior art In unmanned plane wiring structure heat dissipation capacity it is big, the technical issues of cable can not be protected.
The utility model provides a kind of unmanned plane wiring structure, including control device, support device, motor, cable, In,
The support device is fixedly connected with control device 1, and the support device further includes support portion, support ring, support Column, supporting rod, the support ring are connected on support portion;Described support column one end is fixed on support portion, and the other end is connected to institute It states on motor;Described supporting rod one end is connected on the motor, and the other end is connected in the support ring;The support column is set There are support column wiring groove, the support column wiring groove to penetrate through entire supporting rod in the longitudinal direction, the cable is wherein One section is arranged in the support column wiring groove;
Cable draws out of control device and is connected to motor.
Preferably, the support portion is equipped with support portion wiring groove, and a part for the cable is arranged on the support In portion's wiring groove;The support portion wiring groove is connected to the support column wiring groove;The support portion wiring groove with The support column wiring groove is generally aligned in the same plane or is at least partially situated on same plane.
Preferably, the control device is equipped with control device wiring groove, and the part of the cable is arranged on described In control device wiring groove;The control device wiring groove is connected to the support portion wiring groove;The control device Wiring groove is respectively positioned on same plane with the support portion wiring groove, support column wiring groove or is at least partially situated at same In one plane.
Preferably, the support column wiring groove top is several prominent equipped with extending towards support column wiring inside grooves It rises, several protrusions are staggered prevents line in the both sides of the support column wiring groove to limit the position of the cable Cable is deviate from from the support column wiring groove.
Preferably, the support portion wiring groove top is several prominent equipped with extending towards support portion wiring inside grooves It rises, several protrusions are staggered prevents line in the both sides of the support portion wiring groove to limit the position of the cable Cable is deviate from from the support portion wiring groove.
Preferably, the control device wiring groove top is several equipped with extending towards control device wiring inside grooves Protrusion, several protrusions are staggered in the both sides of the control device wiring groove, to limit the position of the cable, prevent Only cable is deviate from from the control device wiring groove.
Preferably, the support device includes bindiny mechanism, and control device can by the bindiny mechanism and support device Dismantling connection.
Preferably, the motor is equipped with heat sink strip.
Preferably, the heat sink strip is evenly distributed on the outside of motor.
By the utility model, it is big effectively to solve unmanned plane wiring structure heat dissipation capacity in the prior art, Wu Fabao The technical issues of protecting cable substantially increases the heat-sinking capability of unmanned plane, extends cruise duration.
Description of the drawings
Fig. 1 is a stereogram of the utility model.
Fig. 2 is the partial enlarged view of the utility model.
Specific implementation mode
With reference to the attached drawing in the utility model embodiment, the technical scheme in the embodiment of the utility model is retouched It states, described embodiment is only a part of the embodiment of the utility model, instead of all the embodiments.Based on this practicality Embodiment in novel, art technology those of ordinary skill is in the every other implementation for not making the creative labor and obtaining Mode shall fall within the protection scope of the present invention.
The utility model provides a kind of unmanned plane wiring structure comprising control device 1, support device 2, motor 3, cable 4, wherein
The support device 2 is fixedly connected with control device 1, and the support device 2 further includes support portion 21, support ring 22, support column 23, supporting rod 24, the support ring 22 are connected on support portion 21;23 one end of the support column is fixed on support Portion 21, the other end are connected on the motor 3;24 one end of the supporting rod is connected on the motor 3, and the other end is connected to institute It states in support ring 22;The support column 23 is equipped with support column wiring groove 231, and the support column wiring groove 231 is in length side Entire supporting rod 24 is penetrated through upwards, and wherein one section of the cable 4 is arranged in the support column wiring groove 231;
Cable 5 draws out of control device 1 and is connected to motor 3.
Preferably, the support portion 21 is equipped with support portion wiring groove, and a part for the cable 4 is arranged on the branch In the wiring groove of support part;It is highly preferred that the support portion wiring groove is connected to the support column wiring groove 231;More preferably Ground, the support portion wiring groove are generally aligned in the same plane or are at least partially situated at together with the support column wiring groove 231 In one plane.
Preferably, the control device 1 be equipped with control device wiring groove (not shown), one of the cable 4 Divide and is arranged in the control device wiring groove;It is highly preferred that the control device wiring groove is applied with the support portion Line groove is connected to (not shown);It is highly preferred that the control device wiring groove and the support portion wiring groove, support Column wiring groove 231 is respectively positioned on same plane or is at least partially situated on same plane.
By the way that above groove to be disposed on the same plane, may be implemented (to be not easy to take off safely in guarantee cable 4 Go out, position is effectively limited) under the premise of so that the length smaller of required cable 4, to save material and reduce line The resistance of cable reduces fever.Meanwhile the support device 2 is made of the light material of fine heat radiation property.In order to preferably protect The safety of cable 4 and groove is set to lay cable, will make cable capped to a certain extent and cable is caused to radiate difficulty Increase, and by structure above, heat dissipation problem can be but well solved, whole technique effect is better balanced, is avoided It attends to one thing and lose sight of another.
Preferably, 231 top of the support column wiring groove, which is equipped with towards support column wiring groove 231, extends internally number A protrusion 232, several protrusions 232 are staggered in the both sides of the support column wiring groove 231, to limit the cable 4 position prevents cable 4 from deviating from from the support column wiring groove 231.By these protrusions, cable can be better protected from Deviate from from support column wiring groove, and protrusion is to be staggered that can so that cable is easier to be disposed in support column wiring recessed In slot.
Preferably, the support portion wiring groove top is several prominent equipped with extending towards support portion wiring inside grooves It rises, several protrusions, which are staggered, to be prevented in the both sides of the support portion wiring groove with limiting the position of the cable 4 Cable 4 is deviate from from the support portion wiring groove.
Preferably, the control device wiring groove top is several equipped with extending towards control device wiring inside grooves Protrusion, several protrusions are staggered in the both sides of the control device wiring groove, to limit the position of the cable 4, Prevent cable 4 from deviating from from the control device wiring groove.
Preferably, the support device 2 includes bindiny mechanism's (not shown), and control device 1 passes through the connection machine Structure is detachably connected with support device 2.
Preferably, the motor 3 is equipped with heat sink strip;Preferably, it is evenly distributed on the outside of motor.So structure It can not only significantly realize the heat dissipation of motor, and the structural stability of motor can be significantly increased, prevent motor quilt It breaks, is the technical solution killed two birds with one stone, be no in the prior art set-up mode.So, not only so that whole Body structure has good stability and reliability, protects cable well, and heat dissipation can be better achieved.Due to this Utility model is the wiring structure for unmanned plane, especially to small drone, for the unmanned plane of toy rank, and this practicality Novel technical solution can make unmanned plane lightweight well, while cable being protected not to be damaged, and can also be well Realize that the heat dissipation of unmanned plane, the especially heat dissipation to the great motor of calorific value make heat dissipation effect most while protecting motor Bigization.This is particularly important for unmanned plane, especially small drone, can preferably keep the stability of structure, Big energy is saved, and motor is prevented to be burned out because of overheat.
It should be noted that as unmanned plane, when needing to carry out flight, unmanned plane includes propeller.The utility model A kind of wiring construction of unmanned plane is provided, it is preferred that emphasis is wiring construction, therefore do not show spiral shell in the attached drawing in the utility model Paddle is revolved, presentation is state that unmanned plane does not install propeller.It should also be noted that, it is provided by the utility model it is a kind of nobody The wiring construction of machine only illustrates a wiring construction in the utility model attached drawing, shows only a motor, be not meant to Unmanned plane only have there are one motor or only there are one the utility model wiring construction.
Wherein, the cable 4 is can to transmit electric energy and/or the cable of various types of signal.

Claims (9)

1. a kind of wiring constructional device of unmanned plane comprising control device (1), support device (2), motor (3), cable, In,
The support device (2) is fixedly connected with control device (1), and the support device (2) further includes support portion (21), support Ring (22), support column (23), supporting rod (24), the support ring (22) are connected on support portion (21);The support column (23) One end is fixed on support portion (21), and the other end is connected on the motor (3);Described supporting rod (24) one end is connected to the electricity On machine (3), the other end is connected in the support ring (22);The support column (23) is equipped with support column wiring groove (231), institute It states support column wiring groove (231) and penetrates through entire supporting rod (24) in the longitudinal direction, wherein one section of the cable (4) is set It sets in the support column wiring groove (231);
Cable draws out of control device (1) and is connected to motor (3).
2. a kind of wiring constructional device of unmanned plane according to claim 1, which is characterized in that the support portion (21) sets There are support portion wiring groove, a part for the cable (4) to be arranged in the support portion wiring groove;The support portion applies Line groove is connected to the support column wiring groove (231);The support portion wiring groove and the support column wiring groove (231) it is generally aligned in the same plane or is at least partially situated on same plane.
3. a kind of wiring constructional device of unmanned plane according to claim 2, which is characterized in that the control device (1) Equipped with control device wiring groove, a part for the cable (4) is arranged in the control device wiring groove;The control Device wiring groove processed is connected to the support portion wiring groove;The control device wiring groove and the support portion wiring are recessed Slot, support column wiring groove (231) are respectively positioned on same plane or are at least partially situated on same plane.
4. a kind of wiring constructional device of unmanned plane according to claim 3, which is characterized in that the support column wiring is recessed It is equipped with towards support column wiring groove (231) at the top of slot (231) and extends internally several protrusions (232), several protrusions (232) be staggered prevents cable in the both sides of the support column wiring groove (231) to limit the position of the cable (4) (4) deviate from from the support column wiring groove (231).
5. a kind of wiring constructional device of unmanned plane according to claim 3, which is characterized in that the support portion wiring is recessed Groove top portion is equipped with the several protrusions extended towards support portion wiring inside grooves, and several protrusions are staggered in the support The both sides of portion's wiring groove prevent cable (4) from deviating from from the support portion wiring groove to limit the position of the cable (4).
6. a kind of wiring constructional device of unmanned plane according to claim 3, which is characterized in that the control device wiring Groove top is equipped with the several protrusions extended towards control device wiring inside grooves, and several protrusions are staggered described The both sides of control device wiring groove prevent cable (4) from the control device wiring to limit the position of the cable (4) Groove is deviate from.
7. a kind of wiring constructional device of unmanned plane according to claim 1, which is characterized in that the support device (2) Including bindiny mechanism, control device (1) is detachably connected by the bindiny mechanism and support device (2).
8. a kind of wiring constructional device of unmanned plane according to claim 1, which is characterized in that the motor (3) is equipped with Heat sink strip, the heat sink strip are evenly distributed on the outside of motor.
9. a kind of unmanned plane, which uses a kind of wiring knot of unmanned plane described in any one of claim 1-8 Structure device, the control device are unmanned aerial vehicle (UAV) control devices, and the motor is the motor for driving propeller rotational.
CN201720805587.2U 2017-07-03 2017-07-03 A kind of the wiring constructional device and its unmanned plane of unmanned plane Active CN207853356U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201720805587.2U CN207853356U (en) 2017-07-03 2017-07-03 A kind of the wiring constructional device and its unmanned plane of unmanned plane

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201720805587.2U CN207853356U (en) 2017-07-03 2017-07-03 A kind of the wiring constructional device and its unmanned plane of unmanned plane

Publications (1)

Publication Number Publication Date
CN207853356U true CN207853356U (en) 2018-09-11

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107425485A (en) * 2017-07-03 2017-12-01 广州途道信息科技有限公司 A kind of wiring structure

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107425485A (en) * 2017-07-03 2017-12-01 广州途道信息科技有限公司 A kind of wiring structure

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