CN212909759U - Airborne solar blind ultraviolet imager - Google Patents
Airborne solar blind ultraviolet imager Download PDFInfo
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- CN212909759U CN212909759U CN202021470824.2U CN202021470824U CN212909759U CN 212909759 U CN212909759 U CN 212909759U CN 202021470824 U CN202021470824 U CN 202021470824U CN 212909759 U CN212909759 U CN 212909759U
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Abstract
The invention discloses an airborne solar blind ultraviolet imager.A telescopic rod is arranged on the lower surface of a mounting plate; the outer pipe of the telescopic lifting rod penetrates through the through hole of the balance rod and can extend downwards, and the inner rod of the telescopic lifting rod is rotatably connected to the fixing plate; the solar blind ultraviolet all-in-one machine is fixedly installed at the lower end of the fixing plate; the mounting plate is higher than the balance bar and is fixed at the lower end of the aircraft; the length of the balancing rod is larger than that of the mounting plate; a left sliding chute structure and a right sliding chute structure are arranged between the balancing rod and the fixed block; wherein the spout structure specifically is: a left sliding groove and a right sliding groove are arranged on the lower surface of the balance rod by taking the through hole passing through the telescopic rod as a symmetrical point, and a sliding block is arranged in each sliding groove to slide; the slide block is connected with one end of the diagonal rod and drives one end of the diagonal rod to slide in the chute; the other end of the diagonal rod is rotatably fixed on the upper surface of the fixed plate; the inclined rod adjusts an included angle between the inclined rod and the fixing plate through an inclined rod cylinder fixedly connected with the inclined rod. The invention has simple structure and easy control.
Description
Technical Field
The invention relates to the field of high-voltage power equipment detection, in particular to an airborne solar blind ultraviolet imager.
Background
With the continuous improvement of the transmission high voltage grade, the line patrol operation of the transmission line is more and more important for maintaining the safe, stable and efficient operation of the regional power grid, and is also the urgent priority of the operation of the power grid. The traditional manual line patrol method takes long time, has high labor cost and great difficulty, and is difficult to complete in some line areas and some patrol projects. The intelligent inspection by using the aerial vehicle can effectively improve the inspection efficiency of the power transmission line. The ultraviolet imaging is characterized by non-contact and remote imaging, is not interfered by an electric field, has the characteristics of intuition, accuracy, high sensitivity, rapidness, safety, wide application range and the like, and has become one of important means for monitoring the health state and diagnosing faults of the power equipment. The solar blind ultraviolet module is combined with the aircraft, so that corona detection of parts such as a lead, an insulating terminal and a hardware fitting can be realized, and related information is recorded, so that the inspection efficiency of the power transmission line is improved. The solar blind ultraviolet module generally divides ultraviolet visible light into a visible light channel and an ultraviolet light channel through a spectroscope, and can output ultraviolet and/or visible videos to the monitoring terminal through image acquisition and fusion equipment. In the in-service use process, make into the form of integrated machine with the solar blind ultraviolet module usually, hang in the lower extreme of aircraft during the use, the technical problem that exists is, when the messenger carries out picture collection, the adjustment to the viewing range of the scene collection lens of solar blind ultraviolet module is realized to the direction of the high flight of remote control messenger's flight usually, often appears adjusting excessive problem this moment, if the module is from taking lifting angle to adjust this moment, more be favorable to finely tuning the viewing range.
Disclosure of Invention
1. The technical problem to be solved is as follows:
aiming at the technical problem, the invention provides an airborne solar blind ultraviolet imager which is used for being suspended on the lower surface of an aircraft to collect visible and ultraviolet picture information and realizing the adjustment of the view finding range of a scene collecting lens of a solar blind ultraviolet module through a self-contained fine adjustment mechanism.
2. The technical scheme is as follows:
an airborne solar blind ultraviolet imager comprises an installation plate and a solar blind ultraviolet all-in-one machine; the method is characterized in that: the lower surface of the mounting plate is provided with a telescopic rod; the outer pipe of the telescopic lifting rod penetrates through the through hole of the balance rod and can extend downwards, and the inner rod of the telescopic lifting rod is rotatably connected to the fixing plate; the solar blind ultraviolet all-in-one machine is fixedly installed at the lower end of the fixing plate; the mounting plate is higher than the balance bar and is fixed at the lower end of the aircraft; the length of the balance bar is larger than that of the mounting plate; a left sliding groove structure and a right sliding groove structure are arranged between the balancing rod and the fixed block; wherein the spout structure specifically is: a left sliding groove and a right sliding groove are arranged on the lower surface of the balance rod by taking the through hole passing through the telescopic rod as a symmetrical point, and a sliding block is arranged in each sliding groove to slide; the slide block is connected with one end of the diagonal rod and drives one end of the diagonal rod to slide in the chute; the other end of the diagonal rod is rotatably fixed on the upper surface of the fixed plate; the inclined rod adjusts an included angle between the inclined rod and the fixing plate through an inclined rod cylinder fixedly connected with the inclined rod.
Further, the mounting plate comprises a tubular fixing sleeve and a base plate; the base plate is fixed on the lower surface of the aircraft; the fixed sleeve is fixedly sleeved on the surface of the upper end outer pipe of the telescopic rod; the fixed sleeve is arranged on the lower surface of the substrate through a spiral structure; the fixed sleeve is connected with the fixed sleeve motor to realize the rotation of the fixed sleeve in a spiral structure.
Furthermore, the solar blind ultraviolet all-in-one machine is of a box-type structure and comprises a protective shell, a lens, an optical path and an electric circuit; the protective casing is provided with an anti-vibration device.
Further, the device also comprises a control module; and the control module is connected with the telescopic rod driving circuit, the fixed sleeve motor driving circuit and the diagonal rod cylinder driving circuit.
3. Has the advantages that:
(1) the utility model discloses a flexible liter shrinkage pole can realize the fine setting of the upper and lower horizontal position of solar blind ultraviolet all-in-one from top to bottom.
(2) The utility model discloses a control two spout structures, through the contained angle between slide bar and the fixed plate about the control, realize the angle fine setting with horizontal plane contained angle of the ultraviolet all-in-one of solar blind.
(3) The utility model discloses a to the rotatory control of rising draw, realize the fine setting to the rotation angle of the blind ultraviolet all-in-one in day.
Drawings
Fig. 1 is a schematic structural view of the present invention;
fig. 2 is a structural diagram of the control system of the present invention.
Detailed Description
The present invention will be described in detail with reference to the accompanying drawings.
As shown in fig. 1 to 2, an airborne solar blind ultraviolet imager comprises an installation plate 1 and a solar blind ultraviolet all-in-one machine 2; the lower surface of the mounting plate is provided with a telescopic rod 3; the outer pipe of the telescopic rod penetrates through the through hole of the balance rod 8 and can extend downwards, and the inner rod of the telescopic rod is rotatably connected to the fixing plate 4; the solar blind ultraviolet all-in-one machine 2 is fixedly arranged at the lower end of the fixing plate; the mounting plate is higher than the balance bar and is fixed at the lower end of the aircraft; the length of the balance bar is larger than that of the mounting plate; a left sliding groove structure and a right sliding groove structure are arranged between the balancing rod and the fixed block; wherein the spout structure specifically is: a left sliding groove and a right sliding groove are arranged on the lower surface of the balance rod taking the through hole passing through the telescopic rod as a symmetrical point, and a sliding block 5 is arranged in each sliding groove in a sliding mode; the slide block is connected with one end of the diagonal rod 6 and drives one end of the diagonal rod to slide in the chute; the other end of the diagonal rod is rotatably fixed on the upper surface of the fixed plate; the inclined rod adjusts an included angle between the 7 and the fixing plate through an inclined rod cylinder fixedly connected with the inclined rod.
Further, the mounting plate comprises a tubular fixing sleeve 9 and a base plate; the base plate is fixed on the lower surface of the aircraft; the fixed sleeve is fixedly sleeved on the surface of the upper end outer pipe of the telescopic rod; the fixed sleeve is arranged on the lower surface of the substrate through a spiral structure; the fixed sleeve is connected with the fixed sleeve motor to realize the rotation of the fixed sleeve in a spiral structure.
Furthermore, the solar blind ultraviolet all-in-one machine is of a box-type structure and comprises a protective shell, a lens, an optical path and an electric circuit; the protective casing is provided with an anti-vibration device.
Further, the device also comprises a control module; and the control module is connected with the telescopic rod driving circuit, the fixed sleeve motor driving circuit and the diagonal rod cylinder driving circuit.
The specific embodiment is as follows: as shown in fig. 2, when the airborne solar blind ultraviolet imager is used, the mounting plate is mounted on the surface of the connecting plate of the aircraft through screws; when the aircraft flies to the vicinity of high-voltage equipment of an electric power system, the telescopic rod descends to drive the solar blind ultraviolet all-in-one machine to descend, the telescopic rod rotates to drive the solar blind ultraviolet all-in-one machine to rotate, and the inclined rod cylinder ascends or descends to drive an included angle between an inclined rod and a fixed plate connected with the inclined rod cylinder to change until the scene collection of a lens of the solar blind ultraviolet all-in-one machine is finished. Among the above-mentioned control process, the host computer passes through wireless communication module and transmits to the control module of aircraft in actual operation, and it is right to realize the utility model discloses a fine setting of finding a view.
Although the present invention has been described with reference to the preferred embodiments, it should be understood that various changes and modifications can be made therein by those skilled in the art without departing from the spirit and scope of the invention as defined by the appended claims.
Claims (4)
1. An airborne solar blind ultraviolet imager comprises an installation plate and a solar blind ultraviolet all-in-one machine; the method is characterized in that: the lower surface of the mounting plate is provided with a telescopic rod; the outer pipe of the telescopic lifting rod penetrates through the through hole of the balance rod and can extend downwards, and the inner rod of the telescopic lifting rod is rotatably connected to the fixing plate; the solar blind ultraviolet all-in-one machine is fixedly installed at the lower end of the fixing plate; the mounting plate is higher than the balance bar and is fixed at the lower end of the aircraft; the length of the balance bar is larger than that of the mounting plate; a left sliding groove structure and a right sliding groove structure are arranged between the balancing rod and the fixed block; wherein the spout structure specifically is: a left sliding groove and a right sliding groove are arranged on the lower surface of the balance rod by taking the through hole passing through the telescopic rod as a symmetrical point, and a sliding block is arranged in each sliding groove to slide; the slide block is connected with one end of the diagonal rod and drives one end of the diagonal rod to slide in the chute; the other end of the diagonal rod is rotatably fixed on the upper surface of the fixed plate; the inclined rod adjusts an included angle between the inclined rod and the fixing plate through an inclined rod cylinder fixedly connected with the inclined rod.
2. The airborne blind-day ultraviolet imager of claim 1, characterized in that: the mounting plate comprises a tubular fixing sleeve and a base plate; the base plate is fixed on the lower surface of the aircraft; the fixed sleeve is fixedly sleeved on the surface of the upper end outer pipe of the telescopic rod; the fixed sleeve is arranged on the lower surface of the substrate through a spiral structure; the fixed sleeve is connected with the fixed sleeve motor to realize the rotation of the fixed sleeve in a spiral structure.
3. The airborne blind-day ultraviolet imager of claim 1, characterized in that: the solar blind ultraviolet all-in-one machine is of a box-type structure and comprises a protective shell, a lens, an optical path and an electrical circuit; the protective casing is provided with an anti-vibration device.
4. The airborne blind-day ultraviolet imager of claim 2, characterized in that: the device also comprises a control module; and the control module is connected with the telescopic rod driving circuit, the fixed sleeve motor driving circuit and the diagonal rod cylinder driving circuit.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202021470824.2U CN212909759U (en) | 2020-07-23 | 2020-07-23 | Airborne solar blind ultraviolet imager |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202021470824.2U CN212909759U (en) | 2020-07-23 | 2020-07-23 | Airborne solar blind ultraviolet imager |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN212909759U true CN212909759U (en) | 2021-04-06 |
Family
ID=75292144
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202021470824.2U Active CN212909759U (en) | 2020-07-23 | 2020-07-23 | Airborne solar blind ultraviolet imager |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN212909759U (en) |
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2020
- 2020-07-23 CN CN202021470824.2U patent/CN212909759U/en active Active
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