CN218198826U - Unmanned aerial vehicle thermal imaging monitoring devices for photovoltaic power plant - Google Patents
Unmanned aerial vehicle thermal imaging monitoring devices for photovoltaic power plant Download PDFInfo
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- CN218198826U CN218198826U CN202222341443.XU CN202222341443U CN218198826U CN 218198826 U CN218198826 U CN 218198826U CN 202222341443 U CN202222341443 U CN 202222341443U CN 218198826 U CN218198826 U CN 218198826U
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Abstract
The utility model discloses an unmanned aerial vehicle thermal imaging monitoring devices for photovoltaic power plant, including shock attenuation protection mechanism, ejection mechanism, rotation motor and ejection motor, shock attenuation protection mechanism includes the unmanned aerial vehicle body, rotate motor fixed mounting in the bottom of unmanned aerial vehicle body, two output difference fixed mounting that rotate the motor have driving gear and protection casing dwang, one side meshing of driving gear is connected with driven gear, the dwang mount is installed to the middle part symmetry of protection casing dwang, the both ends fixed mounting of protection casing dwang has the unmanned aerial vehicle protection casing, the utility model discloses a set up shock attenuation protection mechanism and carry out the shock attenuation protection to unmanned aerial vehicle, rotate the unmanned aerial vehicle protection casing to the horizontal direction through rotating the motor when unmanned aerial vehicle takes off, wrap up whole unmanned aerial vehicle paddle, avoid taking place the collision at flight in-process paddle and building or birds and lead to unmanned aerial vehicle's damage.
Description
Technical Field
The utility model relates to an unmanned aerial vehicle thermal imaging technology field, concretely relates to unmanned aerial vehicle thermal imaging monitoring devices for photovoltaic power plant.
Background
The thermal imaging technology is that an infrared detector and an optical imaging objective lens are utilized to receive an infrared radiation energy distribution pattern of a detected target and reflect the infrared radiation energy distribution pattern on a photosensitive element of the infrared detector, so that an infrared thermal image is obtained, and the thermal image corresponds to a thermal distribution field on the surface of an object.
Will utilize thermal imaging monitoring devices to monitor the electricity generation system in photovoltaic power plant, through install thermal imaging monitoring devices on unmanned aerial vehicle with photovoltaic power plant in the infrared radiation energy distribution map of each electricity generation system reflect infrared detector's photosensitive element on, the staff just can discover easily through observing infrared thermal image which electricity generation system's work original paper is good, which original paper damages unable work, can in time change the original paper that damages, reduce the burden of artificial monitoring, but current unmanned aerial vehicle application still has very big problem in photovoltaic power plant:
when current unmanned aerial vehicle thermal imaging uses outdoors, because the power generation component that misoperation leads to among unmanned aerial vehicle and the photovoltaic power plant very easily collides, cause great damage to unmanned aerial vehicle's paddle, probably lead to the organism condition out of control or fall, simultaneously, take place the collision of organism and ground very easily when unmanned aerial vehicle takes off with descending, cause unmanned aerial vehicle's damage, and unmanned aerial vehicle's take off condition is harsher, just can't take off when facing strong wind and torrential rain weather, in case unmanned aerial vehicle meets strong wind or the phenomenon that the torrential rain will take place to fall at the in-process of flying, when unmanned aerial vehicle takes place the condition of falling, because the area of whole photovoltaic power plant is very big, the place that unmanned aerial vehicle falls is random, the work of searching unmanned aerial vehicle becomes very difficult, it is not practical very much.
SUMMERY OF THE UTILITY MODEL
In order to overcome the technical problem, the utility model aims to provide an unmanned aerial vehicle thermal imaging monitoring devices for photovoltaic power plant carries out the shock attenuation protection to unmanned aerial vehicle through setting up shock attenuation protection mechanism, avoids unmanned aerial vehicle to collide the damage that leads to unmanned aerial vehicle at flight in-process paddle and building or birds, protects unmanned aerial vehicle through setting up ejection mechanism, protects unmanned aerial vehicle through the internally mounted parachute at the ejection storehouse, avoids unmanned aerial vehicle to take place the crash phenomenon.
The purpose of the utility model can be realized by the following technical proposal:
the utility model provides a photovoltaic power plant is with unmanned aerial vehicle thermal imaging monitoring devices, includes shock attenuation protection machanism (1) includes unmanned aerial vehicle body (102), rotates motor (109) dress and is in the bottom of unmanned aerial vehicle body (102), rotates motor (109) both sides output and is equipped with driving gear (111) and protection casing dwang (106) respectively, driving gear (111) meshing driven gear (112), dwang mount (110) are equipped with in protection casing dwang (106), unmanned aerial vehicle protection casing (101) are equipped with in the bottom of unmanned aerial vehicle body (102), unmanned aerial vehicle body (102) are equipped with paddle support (107), paddle support (107) connection flabellum pivot (103), unmanned aerial vehicle paddle (104) are equipped with in flabellum pivot (103) detector connecting axle (108) are installed to unmanned aerial vehicle body (102), thermal imaging detector (105) are equipped with in detector connecting axle (108).
Photovoltaic power plant uses unmanned aerial vehicle thermal imaging monitoring devices, unmanned aerial vehicle protection casing (101) are equipped with a set of damping sleeve (113), damping spring (115) are equipped with in damping sleeve (113), damping spring (115) are equipped with spring stopper (116), damping connecting rod (114) are equipped with in spring stopper (116), horizontal crashproof roof beam (117) are equipped with in damping connecting rod (114).
The utility model provides an unmanned aerial vehicle thermal imaging monitoring devices for photovoltaic power plant, shock attenuation connecting rod (114) and shock attenuation sleeve (113) sliding connection, unmanned aerial vehicle protection casing (101) are equipped with unmanned aerial vehicle base (118), unmanned aerial vehicle base (118) are through shock attenuation connecting rod (114) and shock attenuation sleeve (113) and unmanned aerial vehicle protection casing (101) fixed connection.
A photovoltaic power plant is with unmanned aerial vehicle thermal imaging monitoring devices, ejection mechanism (2) is including launching storehouse (201), it is equipped with sealed lid (202) to launch storehouse (201), it launches sleeve (208) to launch storehouse (201) and be equipped with, it launches spring (209) to launch sleeve (208) and be equipped with, it launches stopper (210) to launch being connected with of spring (209), it launches stopper (210) and is equipped with to launch pole (206), it is equipped with to launch pole (206) and launches fixed orifices (207), it launches platform (205) to launch pole (206) and be equipped with, it is equipped with parachute body (203) to launch platform (205), parachute body (203) and launch and have parachute rope (204) between the platform (205).
The utility model provides an unmanned aerial vehicle thermal imaging monitoring devices for photovoltaic power plant, it is equipped with motor support (211) to launch motor (212), motor support (211) dress is in launching storehouse (201), the output of launching motor (212) is equipped with launches carousel (213), it is equipped with carousel pivot (215) to launch carousel (213), carousel pivot (215) are connected with launches gag lever post (216), launch fixed sliding sleeve (214) is connected in gag lever post (216).
According to the thermal imaging monitoring device of the unmanned aerial vehicle for the photovoltaic power station, the fixed sliding sleeve (214) is arranged inside the ejection bin (201), and the ejection fixing hole (207) is connected with the ejection limiting rod (216) in a clamping manner; the ejection cabin (201) is arranged at the top of the unmanned aerial vehicle body (102).
Has the advantages that:
(1) The utility model discloses a set up shock attenuation protection mechanism and carry out the shock attenuation protection to unmanned aerial vehicle, it is rotatory to the horizontal direction with the unmanned aerial vehicle protection casing to rotate through rotating the motor when unmanned aerial vehicle takes off, wrap up whole unmanned aerial vehicle paddle, avoid colliding with building or birds in flight at in-process paddle and lead to unmanned aerial vehicle's damage, when unmanned aerial vehicle descends, through rotating unmanned aerial vehicle protection casing to horizontal direction, support unmanned aerial vehicle, avoid unmanned aerial vehicle to collide with ground when descending, lead to unmanned aerial vehicle to destroy.
(2) Protect unmanned aerial vehicle through setting up ejection mechanism, protect unmanned aerial vehicle through the internally mounted parachute at ejection storehouse, avoid unmanned aerial vehicle to take place the crash phenomenon, and be full of smog in ejection storehouse's inside, when starting ejection mechanism, the inside smog that has the colour of ejection storehouse can distribute out, when unmanned aerial vehicle takes place the crash, operating personnel discovers unmanned aerial vehicle's position very easily, avoids searching unmanned aerial vehicle.
Drawings
The present invention will be further described with reference to the accompanying drawings.
FIG. 1 is a schematic view of the overall structure of the present invention;
FIG. 2 is a schematic top view of the shock absorbing and protecting mechanism of the present invention;
FIG. 3 is a schematic view of the bottom structure of the middle shock absorbing protection mechanism of the present invention;
fig. 4 is a schematic structural view of the ejection mechanism in a contracted state;
fig. 5 is a schematic structural view of the ejection state of the ejection mechanism in the present invention;
fig. 6 is an enlarged schematic view of the area a in fig. 2 according to the present invention.
In the figure: 1. a shock absorption protection mechanism; 101. unmanned aerial vehicle protective cover; 102. an unmanned aerial vehicle body; 103. a fan blade rotating shaft; 104. unmanned aerial vehicle paddle; 105. a thermal imaging detector; 106. a protective cover rotating rod; 107. a blade support; 108. a detector connecting shaft; 109. rotating the motor; 110. rotating the rod fixing frame; 111. a driving gear; 112. a driven gear; 113. a shock-absorbing sleeve; 114. a shock-absorbing connecting rod; 115. a damping spring; 116. a spring retainer; 117. a transverse impact beam; 118. an unmanned aerial vehicle base; 2. an ejection mechanism; 201. ejecting a bin; 202. a sealing cover; 203. a parachute body; 204. parachute lines; 205. ejecting the platform; 206. a shooting rod; 207. ejecting the fixed hole; 208. ejecting the sleeve; 209. an ejection spring; 210. ejecting a stopper; 211. a motor bracket; 212. an ejection motor; 213. ejecting the turntable; 214. fixing the sliding sleeve; 215. a turntable spindle; 216. and ejecting the limiting rod.
Detailed Description
As shown in fig. 1-6, an unmanned aerial vehicle thermal imaging monitoring device for a photovoltaic power station comprises a shock absorption protection mechanism 1, an ejection mechanism 2, a rotating motor 109 and an ejection motor 212, wherein the shock absorption protection mechanism 1 comprises an unmanned aerial vehicle body 102, the rotating motor 109 is fixedly mounted at the bottom of the unmanned aerial vehicle body 102, two output ends of the rotating motor 109 are respectively fixedly mounted with a driving gear 111 and a shield rotating rod 106, one side of the driving gear 111 is engaged with a driven gear 112, rotating rod fixing frames 110 are symmetrically mounted at the middle part of the shield rotating rod 106, unmanned aerial vehicle shields 101 are fixedly mounted at two ends of the shield rotating rod 106, the unmanned aerial vehicle shields 101 are symmetrically arranged at the bottom of the unmanned aerial vehicle body 102, blade supports 107 are symmetrically mounted around the unmanned aerial vehicle body 102, a blade rotating shaft 103 is arranged at the end part of the blade supports 107, and unmanned aerial vehicle blades 104 are symmetrically mounted at the outer sides of the blade rotating shaft 103, a plurality of damping sleeves 113 are fixedly installed on one side of the unmanned aerial vehicle protective cover 101, a damping spring 115 is fixedly installed inside the damping sleeve 113, a spring stopper 116 is fixedly installed on one side of the damping spring 115, a damping connecting rod 114 is fixedly installed on one end, far away from the damping spring 115, of the spring stopper 116, a transverse anti-collision beam 117 is fixedly installed on one end, far away from the spring stopper 116, of the damping connecting rod 114, a detector connecting shaft 108 is fixedly installed on one side of the unmanned aerial vehicle body 102, a thermal imaging detector 105 is rotatably connected to one side of the detector connecting shaft 108, the damping connecting rod 114 penetrates through the inside of the damping sleeve 113 and is in sliding connection with the damping sleeve 113, unmanned aerial vehicle bases 118 are symmetrically arranged on the top and the bottom of the unmanned aerial vehicle protective cover 101, and the unmanned aerial vehicle bases 118 are fixedly connected with the unmanned aerial vehicle protective cover 101 through the damping connecting rod 114 and the damping sleeve 113, carry out the shock attenuation protection to unmanned aerial vehicle through setting up shock attenuation protection machanism 1, it is rotatory to the horizontal direction with unmanned aerial vehicle protection casing 101 through rotating motor 109 when unmanned aerial vehicle takes off, wrap up whole unmanned aerial vehicle paddle 104, avoid colliding with building or birds at flight in-process unmanned aerial vehicle paddle 104 and lead to unmanned aerial vehicle's damage, when unmanned aerial vehicle descends, through rotating unmanned aerial vehicle protection casing 101 to horizontal direction, support unmanned aerial vehicle, avoid unmanned aerial vehicle to collide with ground when descending, lead to unmanned aerial vehicle damage.
The ejection mechanism 2 comprises an ejection bin 201, a sealing cover 202 is fixedly installed at the top of the ejection bin 201, an ejection sleeve 208 is fixedly installed on the inner side of the bottom of the ejection bin 201, an ejection spring 209 is fixedly installed inside the ejection sleeve 208, an ejection stopper 210 is fixedly connected to the top of the ejection spring 209, an ejection rod 206 is fixedly installed at the top of the ejection stopper 210, an ejection fixing hole 207 is formed in the middle of the ejection rod 206, an ejection platform 205 is fixedly installed at the top of the ejection rod 206, a parachute body 203 is arranged at the top of the ejection platform 205, a parachute rope 204 is fixedly connected between the parachute body 203 and the ejection platform 205, a motor support 211 is fixedly installed at the bottom of the ejection motor 212, the motor support 211 is fixedly installed at one side inside the ejection bin 201, and an ejection turntable 213 is fixedly installed at the output end of the ejection motor 212, top one side fixed mounting who launches carousel 213 has carousel pivot 215, the outside of carousel pivot 215 is rotated and is connected with and launches gag lever post 216, the middle part sliding connection who launches gag lever post 216 has fixed sliding sleeve 214, fixed sliding sleeve 214 fixed mounting is in the inside of launching storehouse 201, it is connected with launching gag lever post 216 block to launch fixed orifices 207, launch storehouse 201 fixed mounting at the top of unmanned aerial vehicle body 102, protect unmanned aerial vehicle through setting up ejection mechanism 2, protect unmanned aerial vehicle through the internally mounted parachute body 203 at ejection storehouse 201, avoid unmanned aerial vehicle to take place the crash phenomenon, and be full of smog in the inside of launching storehouse 201, when starting ejection mechanism 2, it can distribute out to launch the inside pigmented smog of storehouse 201, when unmanned aerial vehicle takes place the aircraft, operating personnel discovers unmanned aerial vehicle's position very easily, avoid searching unmanned aerial vehicle.
The utility model discloses a theory of operation:
the utility model discloses when using, at first, when unmanned aerial vehicle takes off, rotate unmanned aerial vehicle protection casing 101 to the horizontal direction through rotating motor 109, utilize unmanned aerial vehicle protection casing 101 to protect unmanned aerial vehicle paddle 104, avoid unmanned aerial vehicle at the flight in-process because artificial misoperation, unmanned aerial vehicle paddle 104 collides with building or birds of flying lead to the damage of unmanned aerial vehicle, secondly, when unmanned aerial vehicle descends, rotate motor 109 and rotate unmanned aerial vehicle protection casing 101 to vertical direction, unmanned aerial vehicle base 118 carries out shock attenuation support to whole unmanned aerial vehicle, avoid unmanned aerial vehicle not steadily to descend when descending, lead to unmanned aerial vehicle to collide with ground and cause the damage of unmanned aerial vehicle, finally, under the condition that unmanned aerial vehicle takes place to crash, launch the inside parachute body 203 in storehouse 201 through ejection mechanism 2 and launch away, protect whole unmanned aerial vehicle, avoid unmanned aerial vehicle directly pounding to ground, cause the damage of unmanned aerial vehicle, and simultaneously, the smog that lockable storehouse 201 inside has the colour can give off in the air, operating personnel sees smog and regards to unmanned aerial vehicle's position, avoid the manual work to carry out unmanned aerial vehicle's search.
Claims (6)
1. The utility model provides a photovoltaic power plant is with unmanned aerial vehicle thermal imaging monitoring devices, includes shock attenuation protection machanism (1), ejection mechanism (2), its characterized in that, shock attenuation protection machanism (1) is including unmanned aerial vehicle body (102), rotates motor (109) dress the bottom of unmanned aerial vehicle body (102), rotates motor (109) both sides output and is equipped with driving gear (111) and protection casing dwang (106) respectively, driving gear (111) meshing driven gear (112), dwang mount (110) are equipped with in protection casing dwang (106), unmanned aerial vehicle protection casing (101) dress is in the bottom of unmanned aerial vehicle body (102), unmanned aerial vehicle body (102) is equipped with paddle support (107), fan blade pivot (103) is connected in paddle support (107), unmanned aerial vehicle paddle (104) are equipped with in fan blade pivot (103) detector (108) is installed in unmanned aerial vehicle body (102), thermal imaging detector connecting axle (105) are equipped with.
2. The thermal imaging monitoring device of unmanned aerial vehicle for photovoltaic power plant of claim 1, characterized in that, a set of shock attenuation sleeve (113) is equipped with to the unmanned aerial vehicle protection casing (101), damping spring (115) is equipped with in the shock attenuation sleeve (113), damping spring (115) is equipped with spring stopper (116), damping connecting rod (114) is equipped with to spring stopper (116), horizontal anticollision roof beam (117) is equipped with to damping connecting rod (114).
3. The thermal imaging monitoring device for the unmanned aerial vehicle for the photovoltaic power plant of claim 2, characterized in that, the shock absorption connecting rod (114) is connected with the shock absorption sleeve (113) in a sliding manner, the unmanned aerial vehicle protective cover (101) is provided with an unmanned aerial vehicle base (118), and the unmanned aerial vehicle base (118) is fixedly connected with the unmanned aerial vehicle protective cover (101) through the shock absorption connecting rod (114) and the shock absorption sleeve (113).
4. The unmanned aerial vehicle thermal imaging monitoring device for photovoltaic power plant of claim 3, characterized in that, the ejection mechanism (2) is including launching storehouse (201), it is equipped with sealed lid (202) to launch storehouse (201), launch storehouse (201) and be equipped with ejection sleeve (208), ejection spring (209) are equipped with to launch sleeve (208), the connection of launching spring (209) launches stopper (210), launch stopper (210) is equipped with ejection rod (206), ejection rod (206) are equipped with and launch fixed orifices (207), ejection rod (206) are equipped with and launch platform (205), what launch platform (205) is equipped with parachute body (203), there is parachute rope (204) between parachute body (203) and ejection platform (205).
5. The unmanned aerial vehicle thermal imaging monitoring device for the photovoltaic power plant of claim 4, characterized in that a motor bracket (211) is installed on an ejection motor (212), the motor bracket (211) is installed in the ejection bin (201), an ejection turntable (213) is installed at the output end of the ejection motor (212), a turntable rotating shaft (215) is installed on the ejection turntable (213), the ejection limiting rod (216) is connected to the turntable rotating shaft (215), and the ejection limiting rod (216) is connected to a fixed sliding sleeve (214).
6. The unmanned aerial vehicle thermal imaging monitoring device for the photovoltaic power station as claimed in claim 5, wherein the fixed sliding sleeve (214) is installed inside the ejection bin (201), and the ejection fixing hole (207) is connected with the ejection limiting rod (216) in a clamping manner; the ejection cabin (201) is arranged at the top of the unmanned aerial vehicle body (102).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202222341443.XU CN218198826U (en) | 2022-09-04 | 2022-09-04 | Unmanned aerial vehicle thermal imaging monitoring devices for photovoltaic power plant |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202222341443.XU CN218198826U (en) | 2022-09-04 | 2022-09-04 | Unmanned aerial vehicle thermal imaging monitoring devices for photovoltaic power plant |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN218198826U true CN218198826U (en) | 2023-01-03 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202222341443.XU Active CN218198826U (en) | 2022-09-04 | 2022-09-04 | Unmanned aerial vehicle thermal imaging monitoring devices for photovoltaic power plant |
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| Country | Link |
|---|---|
| CN (1) | CN218198826U (en) |
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2022
- 2022-09-04 CN CN202222341443.XU patent/CN218198826U/en active Active
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