CN213768966U - High-precision measuring equipment of satellite remote sensing image auxiliary power line determination system - Google Patents
High-precision measuring equipment of satellite remote sensing image auxiliary power line determination system Download PDFInfo
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- CN213768966U CN213768966U CN202022352098.0U CN202022352098U CN213768966U CN 213768966 U CN213768966 U CN 213768966U CN 202022352098 U CN202022352098 U CN 202022352098U CN 213768966 U CN213768966 U CN 213768966U
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- 238000005259 measurement Methods 0.000 claims description 6
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- 238000005516 engineering process Methods 0.000 abstract description 2
- 230000002146 bilateral effect Effects 0.000 abstract 1
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- 241000251468 Actinopterygii Species 0.000 description 3
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Abstract
The utility model relates to the field of electric power technology, and a satellite remote sensing image auxiliary electric power circuit surveys high accuracy measuring equipment of system surely is disclosed, including unmanned aerial vehicle, unmanned aerial vehicle includes the wing that organism and bilateral symmetry set up, the top of two wings all is provided with the paddle, the fixed lens of deciding of being equipped with in bottom of organism, the bottom both sides of organism are all fixed and are equipped with the clamp plate, logical groove has all been seted up to the bottom of two clamp plates, the cell wall contact who leads to the groove is connected with the depression bar, the bottom of two depression bars all passes logical groove and extends to the outside, and be provided with camera lens protection mechanism jointly, the top of two organisms is all fixed and is equipped with first U-shaped piece, first U-shaped piece rotates through first pivot and is connected with second U-shaped piece, the fixed arc that is equipped with in top of second U-shaped piece. The utility model discloses can prevent that unmanned aerial vehicle from producing the striking to power line and leading to the camera lens to damage to improve and decide the survey accuracy nature.
Description
Technical Field
The utility model relates to an electric power tech field especially relates to satellite remote sensing image auxiliary power line surveys high accuracy measurement device of system surely.
Background
Line is surveyed surely to be the important aspect of power line construction in railway electric power engineering, is the important link of guaranteeing later stage engineering quality, construction difficulty and construction progress, along with the progress of science and technology, begins to use satellite remote sensing image and unmanned aerial vehicle to take photo by plane to measure power line gradually.
When current use unmanned aerial vehicle take photo by plane and satellite remote sensing image is supplementary, unmanned aerial vehicle probably collides with the birds at the flight in-process, can lead to unmanned aerial vehicle bottom camera lens to receive the fish tail easily because the fall out of control and contact with trees branch and leaf etc. simultaneously to the accuracy nature of electric power line survey has been influenced.
SUMMERY OF THE UTILITY MODEL
The utility model aims at solving among the prior art power line survey and adopt unmanned aerial vehicle to decide time measuring, unmanned aerial vehicle can receive the collision striking with birds, contacts with trees branch and leaf when falling out of control simultaneously, leads to unmanned aerial vehicle's camera lens to receive the fish tail, influences the problem of surveying the accuracy surely, and the high accuracy measuring equipment who is used for satellite remote sensing image auxiliary power line survey system that proposes.
In order to achieve the above purpose, the utility model adopts the following technical scheme:
the high-precision measuring equipment of the satellite remote sensing image auxiliary power line determination system comprises an unmanned aerial vehicle, the unmanned aerial vehicle comprises a machine body and wings which are symmetrically arranged on two sides, blades are arranged above the two wings, the bottom of the machine body is fixedly provided with a fixed lens, the two sides of the bottom of the machine body are both fixedly provided with a pressing plate, the bottoms of the two pressing plates are both provided with a through groove, the groove walls of the through grooves are in contact connection with pressure levers, the bottoms of the two pressure levers penetrate through the through grooves and extend to the outside, and is provided with a lens protection mechanism together, the top parts of the two machine bodies are both fixedly provided with a first U-shaped block, the first U-shaped block is rotatably connected with a second U-shaped block through a first shaft pin, an arc-shaped plate is fixedly arranged at the top of the second U-shaped block, and a buffering protection mechanism is arranged between the other end of the arc-shaped plate and the top of the machine body.
Preferably, camera lens protection machanism includes the guard plate, the guard plate is located the below of surveying the camera lens surely, and the top with two the bottom fixed connection of depression bar, the spout has all been seted up to the cell wall both sides that lead to the groove, the top of depression bar is fixed and is equipped with the slider, the both ends and two of slider the cell wall contact of spout is connected, the fixed first spring that is equipped with between the top of slider and the internal surface top that leads to the groove.
Preferably, buffering protection mechanism includes the third U-shaped piece that two symmetries set up, two the third U-shaped piece respectively with the top of organism and the other end fixed connection of arc, two the third U-shaped piece all rotates through the second axis round pin to be connected with the fourth U-shaped piece, two the opposite side of fourth U-shaped piece all is fixed and is equipped with the connecting plate, two fixed second spring and the telescopic link of being equipped with between the connecting plate, the second spring cup joints with the telescopic link.
Preferably, two the top of arc all is fixed and is equipped with the riser, two through the elastic webbing fixed connection of two symmetry settings between the riser.
Preferably, both sides all are fixed and are equipped with the baffle around the top of guard plate, two the baffle is located the both sides of deciding the survey camera lens respectively.
Preferably, the protection plate and the baffle are made of transparent materials.
Compared with the prior art, the utility model provides a high accuracy measuring equipment for satellite remote sensing image auxiliary power line surveys system surely possesses following beneficial effect:
1. this high accuracy measuring equipment of satellite remote sensing image auxiliary power line survey system prevents that unmanned aerial vehicle from striking with outside article and receiving the damage at the flight in-process through first U-shaped piece, second U-shaped piece, arc and the buffering protection machanism that is equipped with.
2. This satellite remote sensing image auxiliary power line surveys high accuracy measuring equipment of system surely, through guard plate, baffle and the camera lens protection machanism that is equipped with, prevent that unmanned aerial vehicle from receiving the fish tail of trees branch and leaf at the flight in-process, improve the accuracy nature of survey camera lens surely to power line, through carrying out effectual protection to the camera lens.
The part that does not relate to in the device all is the same with prior art or can adopt prior art to realize, the utility model discloses simple structure can protect unmanned aerial vehicle's the outside and bottom camera lens, prevents that unmanned aerial vehicle from deciding the test to the power line and producing the striking with outside article and leading to the camera lens to damage to improve the accuracy nature of power line deciding the survey.
Drawings
Fig. 1 is a schematic structural diagram of a high-precision measurement device of a satellite remote sensing image auxiliary power line measurement system provided by the utility model;
FIG. 2 is a schematic top view of the structure of FIG. 1;
fig. 3 is an enlarged view of a portion a of fig. 1.
In the figure: the device comprises a machine body 1, wings 2, blades 3, a fixed measuring lens 4, a pressing plate 5, a pressing rod 6, a first U-shaped block 7, a second U-shaped block 8, an arc-shaped plate 9, a protection plate 10, a sliding block 11, a first spring 12, a third U-shaped block 13, a fourth U-shaped block 14, a connecting plate 15, a second spring 16, a telescopic rod 17, a vertical plate 18, an elastic belt 19 and a baffle 20.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments.
In the description of the present invention, it is to be understood that the terms "upper", "lower", "front", "rear", "left", "right", "top", "bottom", "inner", "outer", and the like indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings, and are only for convenience of description and simplicity of description, and do not indicate or imply that the device or element being referred to must have a particular orientation, be constructed and operated in a particular orientation, and therefore, should not be construed as limiting the present invention.
Referring to fig. 1-3, a high-precision measuring device of a satellite remote sensing image auxiliary power line gauging system comprises an unmanned aerial vehicle, the unmanned aerial vehicle comprises a machine body 1 and wings 2 symmetrically arranged on both sides, blades 3 are arranged above the two wings 2, a gauging lens 4 is fixedly arranged at the bottom of the machine body 1, the gauging lens 4 can accurately gauge a power line, pressing plates 5 are fixedly arranged on both sides of the bottom of the machine body 1, through grooves are formed at the bottoms of the two pressing plates 5, the groove walls of the through grooves are in contact connection with pressing rods 6, the bottoms of the two pressing rods 6 pass through the through grooves and extend to the outside, a lens protection mechanism is commonly arranged, a first U-shaped block 7 is fixedly arranged at the top of the two machine bodies 1, the first U-shaped block 7 is rotatably connected with a second U-shaped block 8 through a first shaft pin, an arc-shaped plate 9 is fixedly arranged at the top of the second U-shaped block 8, and the two arc-shaped plates 9 are arranged to wrap the machine body 1, prevent that unmanned aerial vehicle from receiving comparatively serious striking at the flight in-process, be provided with buffering protection machanism between the other end of two arcs 9 and the top of organism 1.
Lens protection mechanism includes guard plate 10, and guard plate 10 is located the below of surveying camera lens 4 surely, and the bottom fixed connection of top and two depression bars 6, and the spout has all been seted up to the cell wall both sides that lead to the groove, and the top of depression bar 6 is fixed and is equipped with slider 11, and the both ends of slider 11 are connected with the cell wall contact of two spouts, fixes being equipped with first spring 12 between the top of slider 11 and the internal surface top that leads to the groove, carries on spacingly through setting up slider 11 to the removal of depression bar 6.
Buffering protection machanism includes the third U-shaped piece 13 that two symmetries set up, two third U-shaped pieces 13 respectively with organism 1's top and the other end fixed connection of arc 9, two third U-shaped pieces 13 all rotate through the second axis round pin and are connected with fourth U-shaped piece 14, two fourth U-shaped piece 14's opposite side is all fixed and is equipped with connecting plate 15, fixed second spring 16 and the telescopic link 17 of being equipped with between two connecting plates 15, second spring 16 cup joints with telescopic link 17, through the relative rotation of first U-shaped piece 7 and second U-shaped piece 8 and third U-shaped piece 13 and fourth U-shaped piece 14, and cooperate the elasticity buffering of second spring 16, can carry out effectual buffering through the striking that the arc 9 received unmanned aerial vehicle.
The tops of the two arc-shaped plates 9 are fixedly provided with vertical plates 18, the two vertical plates 18 are fixedly connected through elastic belts 19 which are symmetrically arranged, and the buffer effect of the arc-shaped plates 9 on the impact can be improved by arranging the elastic belts 19.
Both sides are all fixed and are equipped with baffle 20 around the top of guard plate 10, and two baffle 20 are located the both sides of deciding to survey camera lens 4 respectively, and guard plate 10 and baffle 20 all adopt transparent material to make, can protect deciding to survey camera lens 4 through transparent material in, do not cause the influence to deciding to survey the measurement of camera lens.
In the utility model, in the flying process of the unmanned aerial vehicle, the electric power circuit is conveniently and accurately measured through the fixed measuring lens 4 arranged at the top of the machine body 1, meanwhile, the unmanned aerial vehicle is prevented from contacting with the branches and leaves of trees in the flying process through the arranged baffle plate 20, thereby ensuring that the fixed measuring lens 4 is not scratched, improving the accuracy of the fixed measuring lens 4 for the electric power circuit, simultaneously, the fixed measuring lens 4 is prevented from being directly damaged when the unmanned aerial vehicle is out of control and falls through the protection plate 10, the pressure bar 6 and the first spring 12, the fixed measuring lens 4 is protected, and also in the flying process of the unmanned aerial vehicle, through the arc plate 9 and the second spring 16 arranged at the top, when the unmanned aerial vehicle is impacted, through the relative rotation between the first U-shaped block 7 and the second U-shaped block 8 and between the third U-shaped block 13 and the fourth U-shaped block 14, and matching with the elastic buffering of the second spring 16, carry out effectual buffering with the striking that unmanned aerial vehicle received, prevent that unmanned aerial vehicle from receiving the striking to cause the damage to take place out of control to guarantee that the survey camera lens 4 does not receive the influence to the survey of power line.
The above, only be the concrete implementation of the preferred embodiment of the present invention, but the protection scope of the present invention is not limited thereto, and any person skilled in the art is in the technical scope of the present invention, according to the technical solution of the present invention and the utility model, the concept of which is equivalent to replace or change, should be covered within the protection scope of the present invention.
Claims (6)
1. The high-precision measuring equipment of the satellite remote sensing image auxiliary power line fixed measuring system comprises an unmanned aerial vehicle and is characterized in that the unmanned aerial vehicle comprises a machine body (1) and wings (2) which are symmetrically arranged on two sides, paddles (3) are arranged above the two wings (2), a fixed measuring lens (4) is fixedly arranged at the bottom of the machine body (1), pressing plates (5) are fixedly arranged on two sides of the bottom of the machine body (1), through grooves are formed in the bottoms of the two pressing plates (5), the groove walls of the through grooves are in contact connection with pressing rods (6), the bottoms of the two pressing rods (6) penetrate through the through grooves and extend to the outside, a lens protection mechanism is jointly arranged, first U-shaped blocks (7) are fixedly arranged at the tops of the two machine bodies (1), and the first U-shaped blocks (7) are rotatably connected with second U-shaped blocks (8) through first shaft pins, arc plates (9) are fixedly arranged at the tops of the second U-shaped blocks (8), and a buffer protection mechanism is arranged between the other ends of the two arc plates (9) and the top of the machine body (1).
2. The high-precision measuring device of the satellite remote sensing image auxiliary power line surveying system according to claim 1, wherein the lens protection mechanism comprises a protection plate (10), the protection plate (10) is located below the surveying lens (4), the top of the protection plate is fixedly connected with the bottoms of the two pressing rods (6), sliding grooves are formed in both sides of the groove wall of the through groove, a sliding block (11) is fixedly arranged at the top of the pressing rod (6), the two ends of the sliding block (11) are in contact connection with the groove walls of the two sliding grooves, and a first spring (12) is fixedly arranged between the top of the sliding block (11) and the top of the inner surface of the through groove.
3. The high-precision measuring device of the satellite remote sensing image auxiliary power line surveying system according to claim 1, wherein the buffering protection mechanism comprises two third U-shaped blocks (13) which are symmetrically arranged, the two third U-shaped blocks (13) are respectively fixedly connected with the top of the machine body (1) and the other end of the arc-shaped plate (9), the two third U-shaped blocks (13) are respectively and rotatably connected with a fourth U-shaped block (14) through a second shaft pin, the other side of each fourth U-shaped block (14) is respectively and fixedly provided with a connecting plate (15), a second spring (16) and a telescopic rod (17) are fixedly arranged between the two connecting plates (15), and the second spring (16) is sleeved with the telescopic rod (17).
4. The high-precision measuring device of the satellite remote sensing image auxiliary power line surveying system according to claim 1, characterized in that a vertical plate (18) is fixedly arranged on the top of each of the two arc plates (9), and the two vertical plates (18) are fixedly connected through two symmetrically arranged elastic bands (19).
5. The high-precision measurement equipment of the satellite remote sensing image auxiliary power line survey system according to claim 2, characterized in that baffles (20) are fixedly arranged on the front side and the rear side of the top of the protection plate (10), and the two baffles (20) are respectively positioned on the two sides of the survey lens (4).
6. The high-precision measurement device of the satellite remote sensing image auxiliary power line survey system according to claim 2, characterized in that the protection plate (10) and the baffle (20) are made of transparent materials.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202022352098.0U CN213768966U (en) | 2020-10-22 | 2020-10-22 | High-precision measuring equipment of satellite remote sensing image auxiliary power line determination system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202022352098.0U CN213768966U (en) | 2020-10-22 | 2020-10-22 | High-precision measuring equipment of satellite remote sensing image auxiliary power line determination system |
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| Publication Number | Publication Date |
|---|---|
| CN213768966U true CN213768966U (en) | 2021-07-23 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202022352098.0U Expired - Fee Related CN213768966U (en) | 2020-10-22 | 2020-10-22 | High-precision measuring equipment of satellite remote sensing image auxiliary power line determination system |
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| CN (1) | CN213768966U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113608320A (en) * | 2021-10-08 | 2021-11-05 | 苏州思源科安信息技术有限公司 | Zoom lens device for face recognition |
-
2020
- 2020-10-22 CN CN202022352098.0U patent/CN213768966U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113608320A (en) * | 2021-10-08 | 2021-11-05 | 苏州思源科安信息技术有限公司 | Zoom lens device for face recognition |
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| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20210723 |