CN112109893A - Unmanned aerial vehicle electric power inspection auxiliary device - Google Patents
Unmanned aerial vehicle electric power inspection auxiliary device Download PDFInfo
- Publication number
- CN112109893A CN112109893A CN202011118870.0A CN202011118870A CN112109893A CN 112109893 A CN112109893 A CN 112109893A CN 202011118870 A CN202011118870 A CN 202011118870A CN 112109893 A CN112109893 A CN 112109893A
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- Prior art keywords
- unmanned aerial
- aerial vehicle
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- vehicle body
- fixed
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- 238000007689 inspection Methods 0.000 title claims abstract description 25
- 238000001514 detection method Methods 0.000 claims abstract description 12
- 230000005540 biological transmission Effects 0.000 claims abstract description 4
- 230000001681 protective effect Effects 0.000 claims description 13
- 230000035939 shock Effects 0.000 claims description 9
- 238000010521 absorption reaction Methods 0.000 claims 3
- 238000009434 installation Methods 0.000 abstract description 4
- 238000010248 power generation Methods 0.000 description 4
- 230000008878 coupling Effects 0.000 description 3
- 238000010168 coupling process Methods 0.000 description 3
- 238000005859 coupling reaction Methods 0.000 description 3
- 238000013016 damping Methods 0.000 description 3
- 238000010586 diagram Methods 0.000 description 2
- 230000005611 electricity Effects 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
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Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/02—Aircraft not otherwise provided for characterised by special use
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface
- B64C25/58—Arrangements or adaptations of shock-absorbers or springs
- B64C25/62—Spring shock-absorbers; Springs
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D45/00—Aircraft indicators or protectors not otherwise provided for
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
- B64D47/08—Arrangements of cameras
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U30/00—Means for producing lift; Empennages; Arrangements thereof
- B64U30/20—Rotors; Rotor supports
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U50/00—Propulsion; Power supply
- B64U50/10—Propulsion
- B64U50/19—Propulsion using electrically powered motors
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2101/00—UAVs specially adapted for particular uses or applications
- B64U2101/30—UAVs specially adapted for particular uses or applications for imaging, photography or videography
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Remote Sensing (AREA)
- Electric Cable Installation (AREA)
Abstract
The invention discloses an unmanned aerial vehicle power inspection auxiliary device which comprises an unmanned aerial vehicle body, wherein a cantilever is installed on the side face of the unmanned aerial vehicle body, a first motor is installed at the bottom of the cantilever, an output shaft of the first motor penetrates out of the cantilever and is connected with a rotor wing, a supporting mechanism is installed at the bottom of the unmanned aerial vehicle body, an installation groove is formed in the unmanned aerial vehicle body, a second motor is fixed in the installation groove, a worm is installed on an output shaft of the second motor, a first rotating shaft is installed at the bottom of the unmanned aerial vehicle body, the first rotating shaft is inserted into the installation groove and connected with a worm wheel, the worm wheel is in meshing transmission with the worm, and a protection mechanism is fixed at the bottom of the. According to the unmanned aerial vehicle body landing protection mechanism, the landing stability of the unmanned aerial vehicle body is greatly improved by arranging the supporting mechanism, meanwhile, the camera in the detection mechanism can be effectively prevented from being polluted by the arranged protection mechanism, and the use convenience is improved.
Description
Technical Field
The invention relates to the technical field of unmanned aerial vehicles, in particular to an unmanned aerial vehicle power inspection auxiliary device.
Background
With the development of society, electricity has gradually become a main energy source for people's life, and wind power generation, thermal power generation, geothermal power generation, nuclear power generation and the like are all the needs for providing electricity to people's life and production.
Present electric power is patrolled and examined mostly and is gone on through unmanned aerial vehicle, but unmanned aerial vehicle's camera is patrolled and examined to present electric power is direct exposing outside mostly, lacks the protection machanism of supplementary use, and the camera is polluted very easily, uses to exist not enoughly, and we propose an unmanned aerial vehicle electric power and patrol and examine auxiliary device for this reason.
Disclosure of Invention
The invention provides an unmanned aerial vehicle power inspection auxiliary device, which aims to solve the problems that in the prior art, a camera of an unmanned aerial vehicle for power inspection is mostly directly exposed outside, a protection mechanism for auxiliary use is lacked, and the camera is easily polluted.
In order to achieve the purpose, the invention adopts the following technical scheme:
the utility model provides an unmanned aerial vehicle electric power inspection auxiliary device, includes the unmanned aerial vehicle body, the side-mounting of unmanned aerial vehicle body has the cantilever, first motor is installed to the bottom of cantilever, the output shaft of first motor is worn out the cantilever and is connected with the rotor, supporting mechanism is installed to the bottom of unmanned aerial vehicle body, the mounting groove has been seted up to the inside of unmanned aerial vehicle body, the inside of mounting groove is fixed with the second motor, the worm is installed to the output shaft of second motor, first pivot is installed to the bottom of unmanned aerial vehicle body, first pivot inserts the inside of mounting groove and is connected with the worm wheel, worm wheel and worm meshing transmission, the bottom of first pivot is fixed with protection machanism, protection machanism's internally mounted has detection mechanism.
Preferably, the supporting mechanism includes the shock attenuation board, the both ends at shock attenuation board top all are fixed with the threaded rod, the sliding sleeve has cup jointed the fixed plate on the threaded rod, the threaded rod has lock nut through threaded connection, install the spring between fixed plate and the shock attenuation board, the top of fixed plate is fixed with the support column.
Preferably, the spring cup joints on the threaded rod, the support column is fixed with the bottom of unmanned aerial vehicle body.
Preferably, the output shaft of the second motor is connected with the worm through a coupler, and one end, far away from the second motor, of the worm is rotatably connected with the mounting groove.
Preferably, the protection mechanism includes the carousel fixed with first pivot, the both ends of carousel bottom all are fixed with the support, it is connected with the second pivot to rotate on the support, it is connected with first protection casing to rotate in the second pivot, be fixed with the second protection casing in the second pivot, the side-mounting of support has the third motor.
Preferably, first protection casing is fixed with the carousel, first protection casing and second protection casing sliding connection, the output shaft and the second pivot of third motor pass through the coupling joint.
Preferably, the detection mechanism comprises a mounting seat fixed in the protection mechanism, a fourth motor is installed on the side face of the mounting seat, an output shaft of the fourth motor is inserted into the mounting seat and connected with a mounting block, and a camera is installed at the bottom of the mounting block.
Preferably, the quantity of cantilever is a plurality of groups, a plurality of groups the cantilever is located the both sides of unmanned aerial vehicle body and is the symmetric distribution.
Compared with the prior art, the invention has the beneficial effects that:
1. when the unmanned aerial vehicle is used, the first motor is started, the output shaft of the first motor rotates to drive the rotor wing to rotate, the rotor wing rotates to provide flying and landing power for the unmanned aerial vehicle body, the whole device is downward when landing, the damping plate firstly contacts the ground, then the unmanned aerial vehicle body provides the supporting column to drive the fixing plate to be downward along the axial direction of the threaded rod and compress the spring, the spring deforms to generate elasticity, vibration of the unmanned aerial vehicle body is reduced when the unmanned aerial vehicle body is used, and the use stability is improved;
2. when the electric power inspection is carried out, the second motor, the third motor and the fourth motor are started, the output shaft of the third motor rotates to drive the second rotating shaft to rotate, the second rotating shaft drives the second protective cover to rotate, the second protective cover is completely accommodated in the first protective cover, the output shaft of the second motor rotates to drive the worm, the worm rotates with the worm gear to drive the first rotating shaft to rotate, the first rotating shaft drives the detection mechanism to rotate through the protection mechanism, the horizontal position of the camera is adjusted, the output shaft of the fourth motor rotates to drive the mounting block to rotate, the mounting block drives the vertical position of the camera, the flexibility of the electric power inspection is improved, the first protective cover and the second protective cover can effectively protect the detection mechanism when the electric power inspection is not carried out, the camera is effectively prevented from being polluted, and the electric power inspection device is very convenient to use.
Drawings
Fig. 1 is a schematic structural diagram of an auxiliary device for power inspection of an unmanned aerial vehicle according to the present invention;
fig. 2 is an installation schematic diagram of a protection mechanism of the power inspection auxiliary device of the unmanned aerial vehicle, which is provided by the invention;
fig. 3 is a bottom view of a protection mechanism of the power inspection auxiliary device of the unmanned aerial vehicle, which is provided by the invention;
fig. 4 is an overall view of a supporting mechanism of the power inspection auxiliary device for the unmanned aerial vehicle according to the present invention.
In the figure: the unmanned aerial vehicle comprises an unmanned aerial vehicle body 1, a cantilever 2, a first motor 3, a rotor 4, a supporting mechanism 5, a damping plate 51, a threaded rod 52, a fixing plate 53, a lock nut 54, a spring 55, a support column 56, a mounting groove 6, a second motor 7, a worm 8, a first rotating shaft 9, a worm wheel 10, a protection mechanism 11, a rotating disk 111, a bracket 112, a second rotating shaft 113, a first protection cover 114, a second protection cover 115, a third motor 116, a detection mechanism 12, a mounting seat 121, a fourth motor 122, a mounting block 123 and a camera 124.
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments.
Referring to fig. 1-4, an unmanned aerial vehicle electric power inspection auxiliary device, including unmanned aerial vehicle body 1, the side-mounting of unmanned aerial vehicle body 1 has cantilever 2, first motor 3 is installed to the bottom of cantilever 2, the output shaft of first motor 3 wears out cantilever 2 and is connected with rotor 4, supporting mechanism 5 is installed to the bottom of unmanned aerial vehicle body 1, mounting groove 6 has been seted up to the inside of unmanned aerial vehicle body 1, the inside of mounting groove 6 is fixed with second motor 7, worm 8 is installed to the output shaft of second motor 7, first pivot 9 is installed to the bottom of unmanned aerial vehicle body 1, first pivot 9 inserts the inside of mounting groove 6 and is connected with worm wheel 10, worm wheel 10 and the meshing transmission of worm 8, the bottom of first pivot 9 is fixed with protection machanism 11, protection machanism 11's internally mounted has detection mechanism.
Specifically, supporting mechanism 5 includes shock attenuation board 51, the both ends at shock attenuation board 51 top all are fixed with threaded rod 52, sliding sleeve has fixed plate 53 on threaded rod 52, threaded rod 52 has lock nut 54 through threaded connection, install spring 55 between fixed plate 53 and the shock attenuation board 51, the top of fixed plate 53 is fixed with support column 56, spring 55 cup joints on threaded rod 52, support column 56 is fixed with unmanned aerial vehicle body 1's bottom, the output shaft of second motor 7 passes through the shaft coupling and is connected with worm 8, the one end that second motor 7 was kept away from to worm 8 rotates with mounting groove 6 and is connected.
Specifically, the protection mechanism 11 includes a rotary table 111 fixed with the first rotary shaft 9, both ends of the bottom of the rotary table 111 are fixed with a support 112, the support 112 is connected with a second rotary shaft 113 in a rotating manner, the second rotary shaft 113 is connected with a first protection cover 114 in a rotating manner, the second rotary shaft 113 is fixed with a second protection cover 115, a third motor 116 is installed on the side surface of the support 112, the first protection cover 114 is fixed with the rotary table 111, the first protection cover 114 is connected with the second protection cover 115 in a sliding manner, and an output shaft of the third motor 116 is connected with the second rotary shaft 113 through a coupling.
Specifically, the detection mechanism 12 includes a mounting seat 121 fixed in the protection mechanism 11, a fourth motor 122 is installed on a side surface of the mounting seat 121, an output shaft of the fourth motor 122 is inserted into the mounting seat 121 and is connected to a mounting block 123, and a camera 124 is installed at the bottom of the mounting block 123.
Specifically, the quantity of cantilever 2 is a plurality of groups, and a plurality of groups cantilever 2 are located the both sides of unmanned aerial vehicle body 1 and are the symmetric distribution.
The working principle is as follows: during use, the first motor 3 is started, the output shaft of the first motor 3 rotates to drive the rotor 4 to rotate, the rotor 4 rotates to provide flying and landing power for the unmanned aerial vehicle body 1, the whole device is downward when landing, the damping plate 51 firstly contacts the ground, then the unmanned aerial vehicle body 1 provides the supporting column 56 to drive the fixing plate 53 to be downward along the axial direction of the threaded rod 52 and compress the spring 55, the spring 55 deforms to generate elastic force to reduce the vibration of the unmanned aerial vehicle body 1 during use, and the use stability is improved;
when the electric power inspection is carried out, the second motor 7, the third motor 116 and the fourth motor 122 are started, the output shaft of the third motor 116 rotates to drive the second rotating shaft 113 to rotate, the second rotating shaft 113 drives the second protective cover 115 to rotate, the second protective cover 115 is completely accommodated in the first protective cover 114, the output shaft of the second motor 7 rotates to drive the worm 8, the worm 8 rotates with the worm wheel 10 to drive the first rotating shaft 9 to rotate, the first rotating shaft 9 drives the detection mechanism 12 to rotate through the protection mechanism 11 to adjust the horizontal position of the camera 124, the output shaft of the fourth motor 122 rotates to drive the mounting block 123 to rotate, the mounting block 123 drives the vertical position of the camera 124, and the flexibility of the electric power inspection is improved, and when not working, the first protective cover 114 and the second protective cover 115 can effectively protect the detection mechanism 12, effectively avoid the camera 124 from being polluted, and are very convenient to use.
The above description is only for the preferred embodiment of the present invention, but the scope of the present invention is not limited thereto, and any person skilled in the art should be considered to be within the technical scope of the present invention, and the technical solutions and the inventive concepts thereof according to the present invention should be equivalent or changed within the scope of the present invention.
Claims (8)
1. The utility model provides an unmanned aerial vehicle electric power inspection auxiliary device, includes unmanned aerial vehicle body (1), its characterized in that, cantilever (2) are installed to the side of unmanned aerial vehicle body (1), first motor (3) are installed to the bottom of cantilever (2), the output shaft of first motor (3) wears out cantilever (2) and is connected with rotor (4), supporting mechanism (5) are installed to the bottom of unmanned aerial vehicle body (1), mounting groove (6) have been seted up to the inside of unmanned aerial vehicle body (1), the inside of mounting groove (6) is fixed with second motor (7), worm (8) are installed to the output shaft of second motor (7), first pivot (9) are installed to the bottom of unmanned aerial vehicle body (1), first pivot (9) insert the inside of mounting groove (6) and are connected with worm wheel (10), worm wheel (10) and worm (8) meshing transmission, the bottom of first pivot (9) is fixed with protection machanism (11), the internally mounted of protection machanism (11) has detection mechanism (12).
2. The unmanned aerial vehicle electric power inspection auxiliary device of claim 1, wherein the supporting mechanism (5) includes a shock absorption plate (51), threaded rods (52) are fixed at both ends of the top of the shock absorption plate (51), a fixing plate (53) is sleeved on the threaded rods (52) in a sliding manner, the threaded rods (52) are connected with lock nuts (54) through threads, springs (55) are installed between the fixing plate (53) and the shock absorption plate (51), and supporting columns (56) are fixed at the top of the fixing plate (53).
3. The unmanned aerial vehicle power inspection auxiliary device of claim 2, wherein the spring (55) is sleeved on the threaded rod (52), and the support column (56) is fixed with the bottom of the unmanned aerial vehicle body (1).
4. The unmanned aerial vehicle power inspection auxiliary device of claim 1, wherein an output shaft of the second motor (7) is connected with a worm (8) through a coupler, and one end of the worm (8) far away from the second motor (7) is rotatably connected with the mounting groove (6).
5. The auxiliary device is patrolled and examined to unmanned aerial vehicle electric power of claim 1, characterized in that, protection machanism (11) include carousel (111) fixed with first pivot (9), both ends of carousel (111) bottom all are fixed with support (112), it is connected with second pivot (113) to rotate on support (112), it is connected with first protection casing (114) to rotate on second pivot (113), be fixed with second protection casing (115) on second pivot (113), the side-mounting of support (112) has third motor (116).
6. The unmanned aerial vehicle power inspection auxiliary device of claim 5, wherein the first protective cover (114) is fixed with the turntable (111), the first protective cover (114) is slidably connected with the second protective cover (115), and an output shaft of the third motor (116) is connected with the second rotating shaft (113) through a coupler.
7. The unmanned aerial vehicle power inspection auxiliary device according to claim 1, wherein the detection mechanism (12) comprises a mounting seat (121) fixed in the protection mechanism (11), a fourth motor (122) is installed on a side surface of the mounting seat (121), an output shaft of the fourth motor (122) is inserted into the mounting seat (121) and is connected with a mounting block (123), and a camera (124) is installed at the bottom of the mounting block (123).
8. The unmanned aerial vehicle electric power inspection auxiliary device of claim 1, wherein the number of cantilevers (2) is a plurality of groups, and the cantilevers (2) of the plurality of groups are located on two sides of the unmanned aerial vehicle body (1) and are symmetrically distributed.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202011118870.0A CN112109893A (en) | 2020-10-19 | 2020-10-19 | Unmanned aerial vehicle electric power inspection auxiliary device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202011118870.0A CN112109893A (en) | 2020-10-19 | 2020-10-19 | Unmanned aerial vehicle electric power inspection auxiliary device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN112109893A true CN112109893A (en) | 2020-12-22 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202011118870.0A Pending CN112109893A (en) | 2020-10-19 | 2020-10-19 | Unmanned aerial vehicle electric power inspection auxiliary device |
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| CN (1) | CN112109893A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112591127A (en) * | 2021-01-27 | 2021-04-02 | 杭州优旗贸易有限公司 | Safety landing device for protecting camera during unmanned aerial vehicle fault |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| KR20010103221A (en) * | 2000-05-08 | 2001-11-23 | 사태형 | landing skid structure of wireless movie camera system |
| CN208393639U (en) * | 2018-03-12 | 2019-01-18 | 卡德克斯技术（深圳）有限公司 | A kind of camera has the unmanned plane of safeguard function |
| CN110294106A (en) * | 2019-07-10 | 2019-10-01 | 江西异能无人机科技有限公司 | A kind of lightweight low energy consumption unmanned plane |
| CN211336477U (en) * | 2019-11-21 | 2020-08-25 | 青岛九天国际飞行学院股份有限公司 | Panoramic high-simulation flight device |
| CN213800185U (en) * | 2020-10-19 | 2021-07-27 | 拓航科技有限公司 | Unmanned aerial vehicle electric power inspection auxiliary device |
-
2020
- 2020-10-19 CN CN202011118870.0A patent/CN112109893A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| KR20010103221A (en) * | 2000-05-08 | 2001-11-23 | 사태형 | landing skid structure of wireless movie camera system |
| CN208393639U (en) * | 2018-03-12 | 2019-01-18 | 卡德克斯技术（深圳）有限公司 | A kind of camera has the unmanned plane of safeguard function |
| CN110294106A (en) * | 2019-07-10 | 2019-10-01 | 江西异能无人机科技有限公司 | A kind of lightweight low energy consumption unmanned plane |
| CN211336477U (en) * | 2019-11-21 | 2020-08-25 | 青岛九天国际飞行学院股份有限公司 | Panoramic high-simulation flight device |
| CN213800185U (en) * | 2020-10-19 | 2021-07-27 | 拓航科技有限公司 | Unmanned aerial vehicle electric power inspection auxiliary device |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112591127A (en) * | 2021-01-27 | 2021-04-02 | 杭州优旗贸易有限公司 | Safety landing device for protecting camera during unmanned aerial vehicle fault |
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