CN111439386B - Ultraviolet, visible light and infrared three-in-one unmanned aerial vehicle power inspection nacelle - Google Patents
Ultraviolet, visible light and infrared three-in-one unmanned aerial vehicle power inspection nacelle Download PDFInfo
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- CN111439386B CN111439386B CN202010305948.3A CN202010305948A CN111439386B CN 111439386 B CN111439386 B CN 111439386B CN 202010305948 A CN202010305948 A CN 202010305948A CN 111439386 B CN111439386 B CN 111439386B
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- China
- Prior art keywords
- nacelle
- glass cover
- electric telescopic
- aerial vehicle
- unmanned aerial
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- 238000007689 inspection Methods 0.000 title claims abstract description 23
- 239000011521 glass Substances 0.000 claims abstract description 48
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims description 48
- 238000003466 welding Methods 0.000 claims description 17
- 229910000831 Steel Inorganic materials 0.000 claims description 8
- 238000007789 sealing Methods 0.000 claims description 8
- 239000010959 steel Substances 0.000 claims description 8
- 238000002347 injection Methods 0.000 claims description 3
- 239000007924 injection Substances 0.000 claims description 3
- 238000000034 method Methods 0.000 abstract description 9
- 230000000694 effects Effects 0.000 abstract description 2
- 239000004576 sand Substances 0.000 abstract description 2
- 239000000428 dust Substances 0.000 description 3
- 238000004140 cleaning Methods 0.000 description 2
- 230000003749 cleanliness Effects 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 238000004804 winding Methods 0.000 description 2
- 230000004075 alteration Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 239000000243 solution Substances 0.000 description 1
- 239000007921 spray Substances 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
- 238000009736 wetting Methods 0.000 description 1
Classifications
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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
-
- 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
-
- 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
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Testing Resistance To Weather, Investigating Materials By Mechanical Methods (AREA)
- Wind Motors (AREA)
Abstract
The invention discloses an ultraviolet, visible light and infrared three-in-one unmanned aerial vehicle power inspection nacelle, which relates to the technical field of power inspection equipment and comprises a storage box, wherein an inner cavity is formed in the storage box, a nacelle body is connected in the inner cavity, the inner cavity is connected with the nacelle body through a rotating shaft, a first electric telescopic rod is connected to the top end of the nacelle body, a stop lever is welded in the storage box, and one side of the stop lever is connected with the nacelle body. According to the invention, the nacelle body is protected by adding the glass cover, so that the nacelle body is prevented from being scratched with branches or other things in the inspection process, the nacelle body cannot be normally used, the nacelle body is protected by the glass cover, meanwhile, the blown sand enters the nacelle body, and meanwhile, the glass cover is externally provided with the groove to move, so that the larger shaking of the glass cover in the moving process is avoided, and the observation effect on the nacelle body is avoided.
Description
Technical Field
The invention belongs to the technical field of power inspection equipment, and particularly relates to an ultraviolet, visible light and infrared three-in-one unmanned aerial vehicle power inspection nacelle.
Background
With the development of scientific technology and the progress of the era, the country builds a power grid vigorously to meet the electricity consumption of people, the power grid needs to be maintained in the daily use process, the power grid can be detected through the unmanned plane and other fixed wing aircraft hanging pods, and the power grid can be rapidly inspected, however, various inspection pods on the market still have various problems.
The single-light pod disclosed by the authority publication No. CN 207510731U can realize that the zoom visible light camera can be switched to any position through two steering engines, and a high-precision two-axis stable platform is adopted to effectively isolate the disturbance and vibration of the airplane; the built-in continuous zooming visible light camera has excellent image quality and detail capturing capability, but the problem that the existing inspection nacelle is hung at the bottom of an unmanned aerial vehicle is not solved, when the inspection is carried out, the nacelle is easy to scratch with branches, influences are caused on the nacelle, meanwhile, the nacelle is easy to be stained with dust on the surface of the nacelle when the nacelle encounters more dust in the use process, so that the nacelle is not clear in observation of a power grid, and meanwhile, when the landing position of the unmanned aerial vehicle is uneven, the nacelle is easy to be in direct contact with the ground, and damage is caused to the nacelle, so that the unmanned aerial vehicle electronic inspection nacelle with three functions of ultraviolet, visible light and infrared is provided.
Disclosure of Invention
The invention aims to provide an ultraviolet, visible light and infrared three-in-one unmanned aerial vehicle power inspection nacelle so as to solve the problems in the background technology.
In order to achieve the above purpose, the present invention provides the following technical solutions:
the utility model provides an ultraviolet, visible light, infrared trinity unmanned aerial vehicle power inspection nacelle, includes the containing box, the inner chamber has been seted up to the inside of containing box, and the internal connection of inner chamber has the nacelle body, the inner chamber is connected with the nacelle body through the pivot, and the top of nacelle body is connected with first electric telescopic handle, the inside welding of containing box has the pin, and one side of pin is connected with the nacelle body, the nacelle body is connected with first electric telescopic handle through the cylindric lock, and the one end of first electric telescopic handle is connected with the containing box, the top welding of containing box has the connecting plate, and the top welding of connecting plate has the bracing piece, opposite one side is connected with the wire wheel between the bracing piece, and the one end of wire wheel is connected with the motor, the bottom of motor is connected with the connecting plate, the outer wall winding of wire wheel has the steel cable, and the steel cable runs through the connecting plate through the through-hole, the one end of steel cable is connected with the glass cover, and the outer wall of glass cover has seted up the recess nacelle body and containing box constitution revolution mechanic, and the cross-sectional area of containing box is less than the glass cover.
Preferably, the first electric telescopic rod forms a movable structure with the nacelle body through a cylindrical pin, and the maximum rotation angle of the nacelle body is 90 degrees.
Preferably, the wire wheels are symmetrically distributed about the central line of the connecting plate, and the central axis of the wire wheels is mutually overlapped with the central axis of the motor.
Preferably, the depth of the inner cavity is greater than the maximum width of the pod body, and the shape of the inner cavity is consistent with the pod body.
Preferably, the bottom welding of connecting plate has the shell, and just the welding of relative one side between the shell has the card strip, the outer wall and the recess of card strip are connected, the outer wall welding of shell has the fixed block, and the bottom welding of fixed block has the second electric telescopic handle, the bottom threaded connection of second electric telescopic handle has the rubber slab, and one side of rubber slab is connected with the glass cover, the bottom welding of fixed block has the third electric telescopic handle, and the bottom threaded connection of third electric telescopic handle has the closing plate, be connected with the water storage tank around the closing plate, and the outer wall and the shell welding of water storage tank mutually, the water injection hole has been seted up to the outer wall of water storage tank.
Preferably, the glass cover and the clamping strips form a moving structure through the grooves, and the grooves are symmetrically distributed about the central line of the glass cover.
Preferably, the water storage tanks are symmetrically distributed about the central line of the shell, and the central line of the water storage tanks is vertically distributed.
Preferably, the central axis of the third electric telescopic rod, the central axis of the water storage tank and the central axis of the sealing plate are mutually overlapped, and a movable structure is arranged between the sealing plate and the water storage tank.
Compared with the prior art, the invention has the beneficial effects that:
(1) According to the invention, the nacelle body is protected by adding the glass cover, so that the nacelle body is prevented from being scratched with branches or other things in the inspection process, the nacelle body cannot be normally used, the nacelle body is protected by the glass cover, meanwhile, the blown sand enters the nacelle body, and meanwhile, the glass cover is externally provided with the groove to move, so that the larger shaking of the glass cover in the moving process is avoided, and the observation effect on the nacelle body is avoided.
(2) According to the invention, the wiping device is additionally arranged outside the glass cover to ensure that dirt on the surface of the glass cover does not influence the observation of the nacelle body, and the water storage tank is additionally arranged to store water, so that dry dirt or dust can be conveniently wetted, dirt is easily wiped from the glass cover, the surface of the glass cover is ensured to be clean and transparent, and a picture shot by the nacelle body is ensured to be clear and accurate.
(3) According to the invention, the nacelle body can be taken in the storage box, so that when the unmanned aerial vehicle falls on uneven ground, the nacelle body can be taken in the storage box and is not in direct contact with the ground, the nacelle body is prevented from being damaged, the subsequent use is influenced, meanwhile, the nacelle body is controlled through the first electric telescopic rod, the nacelle body can be quickly contracted and stretched out, and meanwhile, the nacelle body is prevented from being controlled through the baffle rod, and the nacelle body shakes after stretching out, so that the use is influenced.
Drawings
FIG. 1 is a schematic view of a front cross-sectional structure of the present invention;
FIG. 2 is a schematic side view of the present invention;
FIG. 3 is an enlarged schematic view of the structure of the present invention at A;
FIG. 4 is an enlarged schematic view of the structure of the present invention at B;
fig. 5 is an enlarged schematic view of the structure at C in the present invention.
In the figure: 1. a storage box; 2. an inner cavity; 3. a connecting plate; 4. a rotating shaft; 5. a cylindrical pin; 6. a first electric telescopic rod; 7. a fixed block; 8. a second electric telescopic rod; 9. a water storage tank; 10. a rubber plate; 11. A stop lever; 12. a nacelle body; 13. a glass cover; 14. a groove; 15. a through hole; 16. a water injection hole; 17. Clamping strips; 18. a housing; 19. a wire rope; 20. a third electric telescopic rod; 21. a wire wheel; 22. a support rod; 23. a motor; 24. and (5) sealing the plate.
Detailed Description
The following description of the embodiments of the present invention will be made clearly and completely with reference to the accompanying drawings, in which it is apparent that the embodiments described are only some embodiments of the present invention, but not all embodiments. All other embodiments, which can be made by those skilled in the art based on the embodiments of the invention without making any inventive effort, are intended to be within the scope of the invention.
Referring to fig. 1-5, the invention provides an ultraviolet, visible light and infrared three-in-one unmanned aerial vehicle power inspection nacelle technical scheme:
the unmanned aerial vehicle electric inspection nacelle of ultraviolet, visible light, infrared trinity, including containing box 1, inner chamber 2 has been seted up to the inside of containing box 1, and the internal connection of inner chamber 2 has nacelle body 12, inner chamber 2 is connected with nacelle body 12 through pivot 4, and the top of nacelle body 12 is connected with first electric telescopic handle 6, the inside welding of containing box 1 has pin 11, and one side of pin 11 is connected with nacelle body 12, nacelle body 12 is connected with first electric telescopic handle 6 through cylindric lock 5, and one end of first electric telescopic handle 6 is connected with containing box 1, the top welding of containing box 1 has connecting plate 3, and the top welding of connecting plate 3 has bracing piece 22, be connected with wire wheel 21 on the opposite side between the bracing piece 22, and the one end of wire wheel 21 is connected with motor 23, the bottom and the connecting plate 3 of motor 23 are connected, the outer wall winding of wire wheel 21 has steel cable 19, and steel cable 19 runs through connecting plate 3 through the through hole 15, the one end of wire cable 19 is connected with glass cover 13, and the outer wall of glass cover 13 has set up recess 14 body 12 through pivot 4 and containing box 1, and the cross-sectional area structure that is less than glass cover 13 of containing box 1.
The first electric telescopic rod 6 is connected with the nacelle body 12 through the cylindrical pin 5, so that the first electric telescopic rod 6 can conveniently control the nacelle body 12, the nacelle body 12 can be quickly retracted into the storage box 1 for protection, in this embodiment, preferably, the first electric telescopic rod 6 forms a movable structure between the cylindrical pin 5 and the nacelle body 12, and the maximum rotation angle of the nacelle body 12 is 90 °.
The wire wheel 21 is mainly added to control and roll the steel cable 19, so that the glass cover 13 can be better controlled, the glass cover can be quickly lifted, meanwhile, the wire wheel 21 is symmetrically distributed about the central line of the connecting plate 3, the glass cover 13 can be enabled to run more stably, the clamping stagnation phenomenon can not occur, in the embodiment, the wire wheel 21 is preferably symmetrically distributed about the central line of the connecting plate 3, and the central axis of the wire wheel 21 and the central axis of the motor 23 are mutually overlapped.
The depth of the inner cavity 2 is larger than the maximum width of the pod body 12, so that the pod body 12 can be fully received in the inner cavity 2, the pod body 12 can be protected, the pod body 12 is prevented from being damaged due to external pressure, and the later use is affected.
The cleaning of the surface of the glass cover 13 is carried out through adding devices such as the rubber plate 10, thereby ensuring the cleanliness of the surface of the glass cover 13, the nacelle body 12 is not influenced by the observation of the nacelle body 12 through the glass cover 13, ensuring the accuracy of the picture observed by the nacelle body 12, and reliable information.
The glass cover 13 forms a moving structure with the clamping strip 17 through the groove 14, which mainly prevents the glass cover 13 from being greatly affected by shaking in the process of moving up and down, and easily causes the glass cover 13 to be damaged, and meanwhile, the groove 14 and the clamping strip 17 ensure the glass cover 13 to run stably.
The addition of the water storage tank 9 is mainly convenient for wetting dirt which is easy to dry on the surface of the glass cover 13, the rubber plate 10 is convenient for cleaning the dirt which is easy to dry, and meanwhile, the water storage tanks 9 are symmetrically distributed to ensure that most of the area of the glass cover 13 can be sprayed with water, so that the surface cleanliness of the glass cover 13 is ensured.
The movable structure is formed between the sealing plate 24 and the water storage tank 9, and is mainly convenient for the sealing plate 24 to squeeze water in the water storage tank 9, so that water in the water storage tank 9 is conveniently sprayed on the surface of the glass cover 13, and meanwhile water is conveniently injected into the water storage tank 9.
The working principle and the using flow of the invention are as follows: when the ultraviolet, visible light and infrared three-in-one unmanned aerial vehicle power inspection nacelle is used, the running motor 23 (XD-25 GA 370) drives the wire wheel 21 between the supporting rods 22 to rotate and put down the steel cable 19 through the through hole 15 of the connecting plate 3, so that the glass cover 13 moves downwards, the groove 14 on the glass cover 13 and the clamping strip 17 inside the shell 18 move mutually in the downward moving process of the glass cover 13, the glass cover 13 is ensured not to shake violently in the moving process, the first electric telescopic rod 6 is operated, the nacelle body 12 (Pinling-Q10 TIR) is taken out from the inner cavity 2 of the storage box 1 through the rotating shaft 4, the rubber plate 10 is driven by the second electric telescopic rod 8 below the running fixed block 7 to clean the surface of the glass cover 13, the sealing plate 24 is driven to spray water in the water storage tank 9 through the running third electric telescopic rod 20 when the dirty on the surface of the glass cover 13 is dry, the dry dirty water is conveniently removed, all parts are reset to the water storage tank 9 to fill the water storage tank 16 at the high water storage tank 16, and the water storage tank is filled with water at the water storage tank 16 at the high water storage tank height after the water storage tank is filled with water storage tank 9, and the water storage tank is filled with water at the water storage tank is filled with water level and the water storage tank is filled with water.
Although embodiments of the present invention have been shown and described, it will be understood by those skilled in the art that various changes, modifications, substitutions and alterations can be made therein without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.
Claims (6)
1. The unmanned aerial vehicle power inspection pod comprises a storage box (1), and is characterized in that an inner cavity (2) is formed in the storage box (1), the inner cavity (2) is connected with a pod body (12), the inner cavity (2) is connected with the pod body (12) through a rotating shaft (4), the top end of the pod body (12) is connected with a first electric telescopic rod (6), a stop lever (11) is welded in the storage box (1), one side of the stop lever (11) is connected with the pod body (12), one end of the pod body (12) is connected with a first electric telescopic rod (6) through a cylindrical pin (5), one end of the first electric telescopic rod (6) is connected with the storage box (1), the top of the storage box (1) is welded with a connecting plate (3), the top of the connecting plate (3) is welded with a supporting rod (22), one opposite side of the supporting rod (22) is connected with a wire wheel (21), one end of the wire wheel (21) is connected with a motor (23), one end of the wire wheel (21) is connected with a wire rope (23), the bottom of the wire (3) is connected with the connecting plate (19) through a wire rope (19), one end of the steel cable (19) is connected with a glass cover (13), a groove (14) is formed in the outer wall of the glass cover (13), the nacelle body (12) and the storage box (1) form a rotating structure through a rotating shaft (4), and the cross section area of the storage box (1) is smaller than that of the glass cover (13);
the first electric telescopic rod (6) forms a movable structure between the cylindrical pin (5) and the nacelle body (12), and the maximum rotation angle of the nacelle body (12) is 90 degrees;
the bottom welding of connecting plate (3) has shell (18), and just the welding of relative one side between shell (18) has card strip (17), the outer wall of card strip (17) is connected with recess (14), the outer wall welding of shell (18) has fixed block (7), and the bottom welding of fixed block (7) has second electric telescopic handle (8), the bottom threaded connection of second electric telescopic handle (8) has rubber (10), and one side of rubber slab (10) is connected with glass cover (13), the bottom welding of fixed block (7) has third electric telescopic handle (20), and the bottom threaded connection of third electric telescopic handle (20) has closing plate (24), be connected with water storage tank (9) around closing plate (24), and the outer wall of water storage tank (9) welds with shell (18), water injection hole (16) have been seted up to the outer wall of water storage tank (9).
2. The ultraviolet, visible and infrared three-in-one unmanned aerial vehicle power inspection nacelle according to claim 1, wherein the wire wheels (21) are symmetrically distributed about the central line of the connecting plate (3), and the central axis of the wire wheels (21) and the central axis of the motor (23) are mutually coincident.
3. The ultraviolet, visible and infrared three-in-one unmanned aerial vehicle power inspection pod according to claim 1, wherein the depth of the inner cavity (2) is greater than the maximum width of the pod body (12), and the shape of the inner cavity (2) is consistent with the pod body (12).
4. The ultraviolet, visible and infrared three-in-one unmanned aerial vehicle power inspection nacelle according to claim 1, wherein the glass cover (13) and the clamping strips (17) form a moving structure through the grooves (14), and the grooves (14) are symmetrically distributed about the central line of the glass cover (13).
5. The ultraviolet, visible and infrared three-in-one unmanned aerial vehicle power inspection nacelle according to claim 1, wherein the water storage tanks (9) are symmetrically distributed about the central line of the shell (18), and the central lines of the water storage tanks (9) are vertically distributed.
6. The ultraviolet, visible and infrared three-in-one unmanned aerial vehicle power inspection nacelle according to claim 1, wherein the central axis of the third electric telescopic rod (20), the central axis of the water storage tank (9) and the central axis of the sealing plate (24) are mutually overlapped, and a movable structure is arranged between the sealing plate (24) and the water storage tank (9).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202010305948.3A CN111439386B (en) | 2020-04-17 | 2020-04-17 | Ultraviolet, visible light and infrared three-in-one unmanned aerial vehicle power inspection nacelle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202010305948.3A CN111439386B (en) | 2020-04-17 | 2020-04-17 | Ultraviolet, visible light and infrared three-in-one unmanned aerial vehicle power inspection nacelle |
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| Publication Number | Publication Date |
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| CN111439386A CN111439386A (en) | 2020-07-24 |
| CN111439386B true CN111439386B (en) | 2023-07-25 |
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| CN202010305948.3A Active CN111439386B (en) | 2020-04-17 | 2020-04-17 | Ultraviolet, visible light and infrared three-in-one unmanned aerial vehicle power inspection nacelle |
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| CN112896535B (en) * | 2021-03-09 | 2022-05-31 | 上海澄派信息科技有限公司 | Prevent that branch shelves unmanned aerial vehicle of saving oneself |
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| Publication number | Priority date | Publication date | Assignee | Title |
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| CN101811578B (en) * | 2010-04-23 | 2013-10-23 | 国家电网公司 | Special photoelectric nacelle of power patrol unmanned helicopter |
| CN102694351B (en) * | 2012-06-06 | 2015-05-13 | 长春理工大学 | High voltage overhead transmission line line-inspection unmanned aerial vehicle photoelectric detection device |
| JP6784434B2 (en) * | 2014-07-30 | 2020-11-11 | エスゼット ディージェイアイ テクノロジー カンパニー リミテッドＳｚ Ｄｊｉ Ｔｅｃｈｎｏｌｏｇｙ Ｃｏ．，Ｌｔｄ | Methods, UAV control programs, unmanned aerial vehicles, and control systems |
| CN106114814A (en) * | 2016-07-22 | 2016-11-16 | 四川克瑞斯航空科技有限公司 | A kind of many rotor wing unmanned aerial vehicles |
| CN207258000U (en) * | 2017-08-28 | 2018-04-20 | 国网甘肃省电力公司电力科学研究院 | A kind of inertial guidance data shares the multi-platform gondola of unmanned plane inspection |
| CN210041109U (en) * | 2019-04-25 | 2020-02-07 | 沈阳仕得蓝科技有限公司 | Transmission line inspection device |
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