CN104029817A - Unmanned aerial vehicle - Google Patents
Unmanned aerial vehicle Download PDFInfo
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- CN104029817A CN104029817A CN201410311090.6A CN201410311090A CN104029817A CN 104029817 A CN104029817 A CN 104029817A CN 201410311090 A CN201410311090 A CN 201410311090A CN 104029817 A CN104029817 A CN 104029817A
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- unmanned plane
- uav
- aerial vehicle
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- unmanned aerial
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- 238000009413 insulation Methods 0.000 claims abstract description 21
- 230000005611 electricity Effects 0.000 claims description 13
- 238000004891 communication Methods 0.000 claims description 7
- 239000011152 fibreglass Substances 0.000 claims description 5
- 239000013307 optical fiber Substances 0.000 claims description 5
- 239000011344 liquid material Substances 0.000 claims description 3
- 239000007921 spray Substances 0.000 claims description 2
- 238000000034 method Methods 0.000 abstract description 12
- 239000011810 insulating material Substances 0.000 abstract description 3
- 210000002304 esc Anatomy 0.000 abstract 1
- 238000007689 inspection Methods 0.000 abstract 1
- 238000005516 engineering process Methods 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- 238000005507 spraying Methods 0.000 description 2
- 239000011248 coating agent Substances 0.000 description 1
- 238000000576 coating method Methods 0.000 description 1
- 239000004020 conductor Substances 0.000 description 1
- 238000013461 design Methods 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 238000005538 encapsulation Methods 0.000 description 1
- 238000002347 injection Methods 0.000 description 1
- 239000007924 injection Substances 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
- 238000005259 measurement Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 239000003973 paint Substances 0.000 description 1
- 230000011664 signaling Effects 0.000 description 1
- 239000000243 solution Substances 0.000 description 1
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Abstract
本发明公开提供了一种无人机。该无人机包括：绝缘机架主体、绝缘支架。其中，绝缘支架上均设置有由电池、电调、电机和螺旋桨封装组成的动力部件。本发明的动力部件采用独立电池对电机供电，保证了供电的可靠性。同时，本发明所公开的无人机的动力部件的外壳、机架主体和支架均采用绝缘材料，增加了无人机整体的绝缘度，从而保证无人机在巡检过程中不会对带电设备的运行造成影响。
The disclosure of the present invention provides an unmanned aerial vehicle. The drone includes: an insulating frame main body and an insulating bracket. Among them, power components composed of batteries, ESCs, motors and propeller packages are arranged on the insulating brackets. The power part of the invention adopts an independent battery to supply power to the motor, which ensures the reliability of power supply. At the same time, the outer shell, frame body and support of the power components of the UAV disclosed in the present invention are all made of insulating materials, which increases the overall insulation of the UAV, thereby ensuring that the UAV will not damage the charged parts during the inspection process. affect the operation of the equipment.
Description
Technical field
The present invention relates to electric power overhaul field, relate in particular a kind of unmanned plane.
Background technology
Along with the development of China's science and technology building, unmanned plane is being widely used aspect the maintenance of transformer and circuit.Adopt unmanned plane to patrol and examine quick rapidly, work efficiency is high, the image data of quick obtaining transformer and circuit at short notice, thus facilitate the running condition of service personnel judgement transformer and circuit.
At present for the integral structure of the unmanned plane of patrolling and examining most of be conductor material, thereby in the process of patrolling and examining usually due to nearer apart from transformer, affect the normal operation of charging equipment.
Summary of the invention
In view of this, the present invention openly provides a kind of unmanned plane, to guarantee that unmanned plane can not impact the operation of transformer in the process of patrolling and examining.
For achieving the above object, the invention provides following technical scheme:
A unmanned plane, comprising:
Insulation frame main body;
Be arranged in the insulating support of the both sides of described insulation frame main body;
One end of described insulating support is connected with described insulation frame main body, and the other end is provided with power part;
Wherein, described power part comprises: battery, electric mechanical, electrical tune, screw propeller and insulated shell;
The input end that described electricity is adjusted is connected with described battery, and mouth is connected with described motor;
Described motor is connected with described screw propeller, for driving described screw propeller to rotate;
Described battery, described motor, described electricity are adjusted and are encapsulated in described insulated shell.
Preferably, described insulation frame main body comprises:
Upper strata insulcrete, lower floor's insulcrete and be positioned at the insulation alighting gear of described lower floor insulcrete below;
Wherein, between described upper strata insulcrete and described lower floor insulcrete, be provided with unmanned aerial vehicle (UAV) control parts.
Preferably, described unmanned aerial vehicle (UAV) control parts are adjusted and are connected by optical fiber with described electricity.
Preferably, described unmanned aerial vehicle (UAV) control parts and described electricity are adjusted and are provided with infrared communication module.
Preferably, described unmanned aerial vehicle (UAV) control parts and described electricity are adjusted and are provided with radio communication module.
Preferably, described insulating support adopts fiberglass insulating tube;
It is inner that described optical fiber is positioned at described fiberglass insulating tube.
Preferably, described unmanned plane also comprises: the airborne equipment being connected with described unmanned aerial vehicle (UAV) control parts;
Described airborne equipment comprises: noctovisor, gas sensor and liquid material spray equipment.
Through as shown from the above technical solution, compared with prior art, the present invention openly provides a kind of unmanned plane.This unmanned plane comprises: insulation frame main body, insulating support.Wherein, on insulating support, be provided with the power part being formed by battery, electric tune, motor and screw propeller encapsulation.Power part of the present invention adopts independent battery to power to motor, has guaranteed the reliability of power supply.Meanwhile, the shell of the power part of unmanned plane disclosed in this invention, frame main body and support all adopt insulating material, have increased the insulativity of unmanned plane integral body, thereby guarantee that unmanned plane can not impact the operation of charging equipment in the process of patrolling and examining.
Accompanying drawing explanation
In order to be illustrated more clearly in the embodiment of the present invention or technical scheme of the prior art, to the accompanying drawing of required use in embodiment or description of the Prior Art be briefly described below, apparently, accompanying drawing in the following describes is only embodiments of the invention, for those of ordinary skills, do not paying under the prerequisite of creative work, other accompanying drawing can also be provided according to the accompanying drawing providing.
Fig. 1 shows the structural representation of a kind of unmanned plane of the present invention;
Fig. 2 shows the structural representation of the power part of a kind of unmanned plane of the present invention;
Fig. 3 shows the structural representation of the frame main body of a kind of unmanned plane of the present invention.
The specific embodiment
Below in conjunction with the accompanying drawing in the embodiment of the present invention, the technical scheme in the embodiment of the present invention is clearly and completely described, obviously, described embodiment is only the present invention's part embodiment, rather than whole embodiment.Embodiment based in the present invention, those of ordinary skills, not making the every other embodiment obtaining under creative work prerequisite, belong to the scope of protection of the invention.
Referring to Fig. 1, show the structural representation of a kind of unmanned plane of the present invention.As shown in Figure 1, unmanned plane disclosed in this invention comprises: insulation frame main body 1, be arranged in the insulating support 2 of both sides of insulation frame main body 1, and wherein, one end of insulating support 2 is connected with insulation frame main body 1, and the other end is provided with power part 3.It should be noted that, when actual design unmanned plane, steady in order to guarantee unmanned plane during flying, insulating support 2 adopts symmetrical structure conventionally.
In the present invention, the power part of disclosed unmanned plane adopts power supply independently motor to be powered.Referring to Fig. 2, show the structural representation of the power part of a kind of unmanned plane of the present invention.
Known as shown in Figure 2, the power part of unmanned plane mainly comprises: battery 4, motor 5, electricity are adjusted 6 screw propeller 7 and insulated shells.Wherein, battery 4, motor 5 and electricity are adjusted and are all encapsulated in insulated shell, reach the object with external environment insulation.
The input end of electricity tune 6 is connected with battery 4, and mouth is connected with motor 5, for control the rotative speed of motor according to the control command of the function unit output of unmanned plane, to drive screw propeller 7 to rotate.In power part, be provided with independently power supply motor is powered, thereby drive screw propeller to rotate, without externally fed.When outside is during because of unforeseen circumstances power-off, can not affect the rotation of screw propeller, guaranteed the power supply of screw propeller.
As can be seen here, the unmanned plane of impact for fear of to(for) transformer, the shell of the power part of unmanned plane disclosed in this invention, frame main body and support all adopt insulating material, increase the insulativity of unmanned plane integral body, thereby guarantee that unmanned plane can not impact the operation of charging equipment in the process of patrolling and examining.Such as, can adopt fiberglass insulating tube as the making material of support.
Referring to Fig. 3, show the structural representation of the insulation frame main body of a kind of unmanned plane of the present invention.Insulation frame main body comprises:
Upper strata insulcrete 31, lower floor's insulcrete 32 and be positioned at the insulation alighting gear 33 of lower floor's insulcrete 32 belows.
Wherein, the separate space between upper strata insulcrete 31He lower floor insulcrete 32 is provided with unmanned aerial vehicle (UAV) control parts 34.
The function unit 34 of this unmanned plane can communicate by any one signalling methods and the power part in optical-fibre communications, infrared communication or radio communication, thereby realizes the control to power part.
It should be noted that, because insulation unmanned plane body possesses enough insulating power, thereby cabinet size is not limited by insulation distance, load-carrying ability significantly promotes, can carry the airborne equipments such as noctovisor, gas sensor, liquid material injection device, realize the hot line work such as charged closely infrared measurement of temperature, charged lubricated, charged spraying RTV coating, charged spraying insulated paint.
Finally, also it should be noted that, in this article, relational terms such as the first and second grades is only used for an entity or operation to separate with another entity or operational zone, and not necessarily requires or imply and between these entities or operation, have the relation of any this reality or sequentially.And, term " comprises ", " comprising " or its any other variant are intended to contain comprising of nonexcludability, thereby the process, method, article or the equipment that make to comprise a series of key elements not only comprise those key elements, but also comprise other key elements of clearly not listing, or be also included as the intrinsic key element of this process, method, article or equipment.The in the situation that of more restrictions not, the key element being limited by statement " comprising ... ", and be not precluded within process, method, article or the equipment that comprises described key element and also have other identical element.
In this specification sheets, each embodiment adopts the mode of going forward one by one to describe, and each embodiment stresses is the difference with other embodiment, between each embodiment identical similar part mutually referring to.
Above-mentioned explanation to the disclosed embodiments, makes professional and technical personnel in the field can realize or use the application.To the multiple modification of these embodiment, will be apparent for those skilled in the art, General Principle as defined herein can be in the situation that do not depart from the application's spirit or scope, realization in other embodiments.Therefore, the application will can not be restricted to these embodiment shown in this article, but will meet the widest scope consistent with principle disclosed herein and features of novelty.
Claims (7)
1. a unmanned plane, is characterized in that, comprising:
Insulation frame main body;
Be arranged in the insulating support of the both sides of described insulation frame main body;
One end of described insulating support is connected with described insulation frame main body, and the other end is provided with power part;
Wherein, described power part comprises: battery, electric mechanical, electrical tune, screw propeller and insulated shell;
The input end that described electricity is adjusted is connected with described battery, and mouth is connected with described motor;
Described motor is connected with described screw propeller, for driving described screw propeller to rotate;
Described battery, described motor, described electricity are adjusted and are encapsulated in described insulated shell.
2. unmanned plane according to claim 1, is characterized in that, described insulation frame main body comprises:
Upper strata insulcrete, lower floor's insulcrete and be positioned at the insulation alighting gear of described lower floor insulcrete below;
Wherein, between described upper strata insulcrete and described lower floor insulcrete, be provided with unmanned aerial vehicle (UAV) control parts.
3. unmanned plane according to claim 2, is characterized in that, described unmanned aerial vehicle (UAV) control parts are adjusted and are connected by optical fiber with described electricity.
4. unmanned plane according to claim 2, is characterized in that, described unmanned aerial vehicle (UAV) control parts and described electricity are adjusted and be provided with infrared communication module.
5. unmanned plane according to claim 2, is characterized in that, described unmanned aerial vehicle (UAV) control parts and described electricity are adjusted and be provided with radio communication module.
6. unmanned plane according to claim 3, is characterized in that, described insulating support adopts fiberglass insulating tube;
It is inner that described optical fiber is positioned at described fiberglass insulating tube.
7. unmanned plane according to claim 2, is characterized in that, described unmanned plane also comprises: the airborne equipment being connected with described unmanned aerial vehicle (UAV) control parts;
Described airborne equipment comprises: noctovisor, gas sensor and liquid material spray equipment.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410311090.6A CN104029817A (en) | 2014-07-01 | 2014-07-01 | Unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410311090.6A CN104029817A (en) | 2014-07-01 | 2014-07-01 | Unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN104029817A true CN104029817A (en) | 2014-09-10 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201410311090.6A Pending CN104029817A (en) | 2014-07-01 | 2014-07-01 | Unmanned aerial vehicle |
Country Status (1)
| Country | Link |
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| CN (1) | CN104029817A (en) |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105035338A (en) * | 2015-07-23 | 2015-11-11 | 国网辽宁省电力有限公司葫芦岛供电公司 | Device for detecting transmission line parts of unmanned aerial vehicle |
| CN105109684A (en) * | 2015-09-18 | 2015-12-02 | 施侃超 | Remote-control aircraft system with function of optical fiber communications, powered by external power source |
| CN105425810A (en) * | 2015-12-29 | 2016-03-23 | 国家电网公司 | Unmanned aerial vehicle for inspection |
| US11368002B2 (en) | 2016-11-22 | 2022-06-21 | Hydro-Quebec | Unmanned aerial vehicle for monitoring an electrical line |
| CN117013432A (en) * | 2023-09-28 | 2023-11-07 | 国网山西省电力公司太原供电公司 | Cable overhauling machine |
| US12097956B2 (en) | 2021-04-30 | 2024-09-24 | Hydro-Quebec | Drone with tool positioning system |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101381002A (en) * | 2008-10-24 | 2009-03-11 | 华北电力大学 | A flying robot for testing transmission line insulators |
| CN202042825U (en) * | 2011-03-09 | 2011-11-16 | 南京航空航天大学 | Transmission line inspection system based on multi-rotor unmanned aerial vehicle |
| CN202320781U (en) * | 2011-10-19 | 2012-07-11 | 华北电网有限公司大同超高压供电公司 | Mountain area transmission line patrol unmanned plane |
| CN202337361U (en) * | 2011-10-14 | 2012-07-18 | 广州虹天航空科技有限公司 | Three-shaft aircraft |
| CN102941920A (en) * | 2012-12-05 | 2013-02-27 | 南京理工大学 | High-tension transmission line inspection robot based on multi-rotor aircraft and method using robot |
| CN103144770A (en) * | 2013-03-19 | 2013-06-12 | 南京航空航天大学 | Full-automatic indoor environment control, obstacle avoidance and navigation type micro aerial vehicle |
-
2014
- 2014-07-01 CN CN201410311090.6A patent/CN104029817A/en active Pending
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101381002A (en) * | 2008-10-24 | 2009-03-11 | 华北电力大学 | A flying robot for testing transmission line insulators |
| CN202042825U (en) * | 2011-03-09 | 2011-11-16 | 南京航空航天大学 | Transmission line inspection system based on multi-rotor unmanned aerial vehicle |
| CN202337361U (en) * | 2011-10-14 | 2012-07-18 | 广州虹天航空科技有限公司 | Three-shaft aircraft |
| CN202320781U (en) * | 2011-10-19 | 2012-07-11 | 华北电网有限公司大同超高压供电公司 | Mountain area transmission line patrol unmanned plane |
| CN102941920A (en) * | 2012-12-05 | 2013-02-27 | 南京理工大学 | High-tension transmission line inspection robot based on multi-rotor aircraft and method using robot |
| CN103144770A (en) * | 2013-03-19 | 2013-06-12 | 南京航空航天大学 | Full-automatic indoor environment control, obstacle avoidance and navigation type micro aerial vehicle |
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105035338A (en) * | 2015-07-23 | 2015-11-11 | 国网辽宁省电力有限公司葫芦岛供电公司 | Device for detecting transmission line parts of unmanned aerial vehicle |
| CN105109684A (en) * | 2015-09-18 | 2015-12-02 | 施侃超 | Remote-control aircraft system with function of optical fiber communications, powered by external power source |
| CN105425810A (en) * | 2015-12-29 | 2016-03-23 | 国家电网公司 | Unmanned aerial vehicle for inspection |
| US11368002B2 (en) | 2016-11-22 | 2022-06-21 | Hydro-Quebec | Unmanned aerial vehicle for monitoring an electrical line |
| US12097956B2 (en) | 2021-04-30 | 2024-09-24 | Hydro-Quebec | Drone with tool positioning system |
| CN117013432A (en) * | 2023-09-28 | 2023-11-07 | 国网山西省电力公司太原供电公司 | Cable overhauling machine |
| CN117013432B (en) * | 2023-09-28 | 2023-12-12 | 国网山西省电力公司太原供电公司 | A cable inspection machine |
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Application publication date: 20140910 |
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