CN206336422U - Vertical fin duct steering driving mechanism under power-line patrolling unmanned airship - Google Patents
Vertical fin duct steering driving mechanism under power-line patrolling unmanned airship Download PDFInfo
- Publication number
- CN206336422U CN206336422U CN201621321918.7U CN201621321918U CN206336422U CN 206336422 U CN206336422 U CN 206336422U CN 201621321918 U CN201621321918 U CN 201621321918U CN 206336422 U CN206336422 U CN 206336422U
- Authority
- CN
- China
- Prior art keywords
- vertical fin
- duct
- electric machine
- driving mechanism
- steering driving
- 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.)
- Active
Links
- 230000005611 electricity Effects 0.000 claims description 4
- 238000004891 communication Methods 0.000 claims description 3
- 230000009286 beneficial effect Effects 0.000 abstract description 2
- 230000002457 bidirectional effect Effects 0.000 description 5
- 230000005540 biological transmission Effects 0.000 description 3
- 238000000034 method Methods 0.000 description 2
- 238000006424 Flood reaction Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
- 230000007257 malfunction Effects 0.000 description 1
Landscapes
- Radio Relay Systems (AREA)
Abstract
Vertical fin duct steering driving mechanism under power-line patrolling unmanned airship, including lower vertical fin duct and duct motor control module, described lower vertical fin duct is arranged in fixed aerofoil, and described duct motor control module is connected by power control line with the brushless electric machine in lower vertical fin duct.The beneficial effects of the utility model are：When unmanned airship hovers in the air, lower vertical fin duct steering driving mechanism can realize that 360 degree of dirigible is flexibly turned to, and effectively raise the low-speed handing and turn performance of dirigible.
Description
Technical field
The utility model is related to vertical fin duct steering driving mechanism under power-line patrolling unmanned airship, belongs to power-line patrolling neck
Domain.
Background technology
With the continuous expansion of power network scale, the walking operation of transmission line of electricity to the safe and stable operation of power network increasingly
It is important.Transmission line of electricity in face of becoming increasingly complex crosses over region, and patrolling in hazard weathers such as ice damage, floods earthquake and landslides
Ray examination, traditional artificial patrolling method takes time long, human cost height, difficulty greatly, it is difficult to meet power network development
Need.Unmanned vehicle line walking can be saved effectively the time, it is ensured that the person and equipment safety, with vast potential for future development.
Unmanned airship is a kind of steerable aircraft for being lighter than air, the buoyancy produced by the gas closed in air bag
Float in the air, the pulling force produced by engine flies in the air.Other unmanned vehicles are compared to, unmanned airship has
High flight safety, good safety guarantee is provided by dirigible itself and carrying task device；Low latitude, low-speed performance
It is good, there is preferable structural maintenance and good flight controllability, non-aviation professional user ground service is ensured, fly the bands such as implementation
Great convenience is carried out.Therefore, using carrying platform of the unmanned airship as transmission line of electricity flight equipment, there is larger reality
With advantage and application prospect.
When unmanned airship is applied to power-line patrolling, it is desirable to which dirigible has good low latitude, low-speed performance.Traditional nobody flies
Ship realizes by the deflection of empennage and turns to, radius of turn is big, u-turn is difficult, hovering when can not 360 degree of fixed point rotaries, it is unfavorable
Work is looked into emphasis sight to hidden danger point or suspected malfunctions point in power-line patrolling, and these are the power-line patrolling popularizations of restriction unmanned airship
The principal element of application.
Utility model content
The purpose of this utility model is exactly in order to solve the above-mentioned technical problem to contain there is provided vertical fin under power-line patrolling unmanned airship
Road steering driving mechanism.
The utility model is achieved through the following technical solutions：
Vertical fin duct steering driving mechanism under power-line patrolling unmanned airship, including lower vertical fin duct and duct motor control mould
Block, described lower vertical fin duct is arranged in fixed aerofoil, and described duct motor control module is by power control line with
Brushless electric machine connection in vertical fin duct.
Wherein, brushless electric machine, propeller and electric machine support are provided with described lower vertical fin duct, brushless electric machine passes through motor
Support is fixed in fixed aerofoil, and one end of brushless electric machine is provided with propeller, and propeller is made up of two helicoid blades, spiral
The positive and negative rotation of oar provides the thrust of both direction.
Wherein, described duct motor control module includes radio receiving unit and wireless energy control units, wireless receiving list
Member is used to receive the operational order data from dirigible remote control, and radio receiving unit is wireless communication data terminal, nothing
Line traffic control unit has bidirectional electronic speed-regulating function, for controlling the positive and negative rotation of vertical fin shrouded propeller and rotation speed under dirigible
Degree.
Wherein, described duct area accounts for the 40% of fixed aerofoil area.
Wherein, described electric machine support is that angle is 120 between hollow cylinder or prism structure, two electric machine supports
Degree.
Wherein, the quantity of described electric machine support is three.
Compared with prior art, the beneficial effects of the utility model are：When unmanned airship hovers in the air, lower vertical fin is contained
Road steering driving mechanism can realize that 360 degree of dirigible is flexibly turned to, and effectively raise the low-speed handing and turn performance of dirigible.
Brief description of the drawings
Fig. 1 is the side subdivision graph of vertical fin duct steering driving mechanism under the utility model power-line patrolling unmanned airship.
Fig. 2 is the rear subdivision graph of vertical fin duct steering driving mechanism under the utility model power-line patrolling unmanned airship.
Fig. 3 is the structured flowchart of vertical fin duct steering driving mechanism under the utility model power-line patrolling unmanned airship.
In figure：1st, brushless electric machine, 2, propeller, 3, lower vertical fin duct, 4, fixed aerofoil, 5, electric machine support, 6, power supply control
Line processed, 7, wireless energy control units, 8, radio receiving unit.
Embodiment
The utility model is described in further detail with specific embodiment below in conjunction with the accompanying drawings, and following examples are descriptive
, it is not limited, it is impossible to which protection domain of the present utility model is limited with this.
Embodiment 1
As depicted in figs. 1 and 2, vertical fin duct steering driving mechanism under power-line patrolling unmanned airship, including lower vertical fin duct 3
With duct motor control module, lower vertical fin duct 3 is arranged in fixed aerofoil 4, and the area of lower vertical fin duct 3 accounts for fixed aerofoil 4
The 40% of area, it is ensured that the intensity in lower vertical fin fixed-wing face 4, duct motor control module passes through power control line 6 and lower vertical fin
Brushless electric machine 1 in duct 3 is connected.
Wherein, lower vertical fin duct 3 includes brushless electric machine 1, propeller 2 and electric machine support 5, and brushless electric machine 1 passes through three skies
Electrocardio machine support 5 is fixed, and 5 angles of electric machine support are 120 degree, and lower vertical fin duct 3 is using being electric-only propulsion, and maximum can make dirigible
Propeller 2 in the u-turn of 360 degree of original place, lower vertical fin duct 3 is made up of two helicoid blades, and its positive and negative rotation can provide two
The thrust in direction.
Duct motor control module includes bidirectional electronic speed regulator, radio receiving unit 8 and wireless energy control units 7, wirelessly
Receiving unit 8 is as wireless communication data terminal, for receiving the operational order data from dirigible remote control；Wireless controlled
Unit 7 processed has bidirectional electronic speed-regulating function, for controlling the positive and negative rotation of the propeller 2 under dirigible in vertical fin duct 3 and turning
Dynamic speed.
As shown in figure 3, during work, by master manipulator（That is remote control）Control control circuit, passes through data radio station and transmitting
Antenna sends manipulation signal；By the reception antenna on dirigible（That is radio receiving unit 8）Remote control reception master manipulator is sent out
The manipulation signal control gone out；Also can be by self-driving programme-control（That is wireless energy control units 7）Controlled by bidirectional electronic speed regulator
Brushless electric machine, bidirectional electronic speed regulator is connected with power supply.
Working method principle：When unmanned airship hovers in the air, radio receiving unit 8 receives the deflection control of dirigible remote control
Signal processed, brushless electric machine 1 is controlled by wireless energy control units 7, lower vertical fin shrouded propeller 2 is provided pushing away for both direction
Power, the steering duct that also can be used alone in the case of without using rudder surface turns left or turned right.
Claims (6)
1. vertical fin duct steering driving mechanism under power-line patrolling unmanned airship, it is characterised in that including lower vertical fin duct and duct electricity
Machine control module, described lower vertical fin duct is arranged in fixed aerofoil, and described duct motor control module passes through power supply control
Line processed is connected with the brushless electric machine in lower vertical fin duct.
2. vertical fin duct steering driving mechanism under power-line patrolling unmanned airship according to claim 1, it is characterised in that institute
Brushless electric machine, propeller and electric machine support are provided with the lower vertical fin duct stated, brushless electric machine is fixed on fixation by electric machine support
In aerofoil, one end of brushless electric machine is provided with propeller, and propeller is made up of two helicoid blades, and the positive and negative rotation of propeller is carried
For the thrust of both direction.
3. vertical fin duct steering driving mechanism under power-line patrolling unmanned airship according to claim 1, it is characterised in that institute
The duct motor control module stated includes radio receiving unit and wireless energy control units, and radio receiving unit is used to receive from winged
The operational order data of ship remote control, radio receiving unit is wireless communication data terminal, and wireless energy control units have double
To electronic speed regulation function, positive and negative rotation and velocity of rotation for controlling vertical fin shrouded propeller under dirigible.
4. vertical fin duct steering driving mechanism under power-line patrolling unmanned airship according to claim 1 or 2, it is characterised in that
Described lower vertical fin duct area accounts for the 40% of fixed aerofoil area.
5. vertical fin duct steering driving mechanism under power-line patrolling unmanned airship according to claim 2, it is characterised in that institute
The electric machine support stated is that angle is 120 degree between hollow cylinder or prism structure, two electric machine supports.
6. vertical fin duct steering driving mechanism under power-line patrolling unmanned airship according to claim 5, it is characterised in that institute
The quantity for the electric machine support stated is three.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621321918.7U CN206336422U (en) | 2016-12-05 | 2016-12-05 | Vertical fin duct steering driving mechanism under power-line patrolling unmanned airship |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621321918.7U CN206336422U (en) | 2016-12-05 | 2016-12-05 | Vertical fin duct steering driving mechanism under power-line patrolling unmanned airship |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206336422U true CN206336422U (en) | 2017-07-18 |
Family
ID=59307425
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201621321918.7U Active CN206336422U (en) | 2016-12-05 | 2016-12-05 | Vertical fin duct steering driving mechanism under power-line patrolling unmanned airship |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206336422U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106628100A (en) * | 2016-12-05 | 2017-05-10 | 国网辽宁省电力有限公司丹东供电公司 | Lower vertical tail duct steering driving mechanism for power line inspection unmanned airship |
| CN108549396A (en) * | 2018-04-17 | 2018-09-18 | 福州大学 | A kind of Dual-motors Driving unmanned boat control system based on STM32F429 |
-
2016
- 2016-12-05 CN CN201621321918.7U patent/CN206336422U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106628100A (en) * | 2016-12-05 | 2017-05-10 | 国网辽宁省电力有限公司丹东供电公司 | Lower vertical tail duct steering driving mechanism for power line inspection unmanned airship |
| CN108549396A (en) * | 2018-04-17 | 2018-09-18 | 福州大学 | A kind of Dual-motors Driving unmanned boat control system based on STM32F429 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN206258735U (en) | The aerial demo system of multidimensional based on multiple no-manned plane | |
| CN204055195U (en) | A kind of six rotor diving aircraft | |
| CN104843181A (en) | Petrol-electric hybrid power fixed wing vertical take-off and landing unmanned plane system | |
| CN105109704A (en) | Mooring system based on multi-rotor flight platform | |
| CN201678037U (en) | Natural power levitation platform | |
| CN201494622U (en) | Wired electric flying and floating aircraft | |
| AU2019100363A4 (en) | Unmanned Aerial Vehicle And Its Program Control Device Unmanned Aerial Vehicle And Its Program Control Device | |
| CN106627010A (en) | Water-air amphibious unmanned aerial vehicle | |
| CN207157480U (en) | Unmanned investigation dirigible system and low latitude detecting system | |
| CN105966609B (en) | A kind of heavy autogyro hybrid power richochet system with variable-distance teetering rotor head | |
| CN204527630U (en) | A kind of oil electric mixed dynamic fixed-wing VUAV system | |
| CN102991663A (en) | System for mooring stratospheric telecommunication platform with rotor wing | |
| CN106184741A (en) | A kind of flying wing type ducted fan VUAV | |
| CN105346715A (en) | Vertical take-off and landing unmanned plane | |
| CN206336422U (en) | Vertical fin duct steering driving mechanism under power-line patrolling unmanned airship | |
| CN108638773A (en) | The wheeled land, water and air of a kind of three rotors three are dwelt robot | |
| CN107554783A (en) | A kind of amphibious unmanned plane of VTOL | |
| CN104015915A (en) | Unmanned gas saucer and manufacturing method thereof | |
| CN206434864U (en) | A kind of aircraft of VTOL | |
| CN208931640U (en) | It can be in the quadrotor drone of hydroplaning | |
| CN204078068U (en) | A kind of four-axle aircraft of overlength flying power | |
| CN202953165U (en) | Mooring rotor lift-off platform system | |
| CN104149565A (en) | Air and ground dual-purpose multifunctional trolley | |
| CN103523236A (en) | Unmanned aerial vehicle wind energy recycling device | |
| CN201354151Y (en) | Electric one-man aircraft |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant |