Terrain scanner

Abstract

The utility model relates to the technical field of scanners, and discloses a terrain scanner, comprising an aircraft, the bottom of which is provided with a mounting rack, and the interior of which is provided with a storage battery; the scanner is mounted in the mounting frame; a protection assembly is arranged in the aircraft; before the aircraft needs to land, a driving mechanism only needs to be started to drive a moving plate to move downwards, so that a limiting sliding block is driven to retract into the moving plate, limiting on a connecting plate is relieved, the connecting plate can be pushed downwards under the action of a spring outside a second guide rod, and then two protection plates are driven to slide out downwards; the protection plate slides to the position below the scanner, when the aircraft lands, landing can be buffered through contact between the protection plate and the ground, damage to the aircraft is reduced, meanwhile, when the aircraft flies normally, the protection plate is stored in the aircraft, the view of the scanner is not shielded, and the practicability of the device is enhanced.

Description

TECHNICAL FIELD

[0001] The utility model relates to scanner technical field, concretely is a topographic scanner. BACKGROUND

[0002] When studying the geological characteristics of the ore deposit, it is necessary to measure the topography and geomorphology from each ore-drawing platform to the three-option crushing station and from each slag-drawing platform to each dumping site, establish a three-dimensional topographic map, and calculate the self-unloading truck haul distance. According to the road topography of the three-dimensional topographic map, the transportation route is optimized to improve the transportation efficiency and reduce the loss. At this time, a topographic scanner is needed to take pictures of the topography and geomorphology in order to establish a three-dimensional map to visually display the topography.

[0003] The existing aerial scanner generally adds a fixed frame under the unmanned aerial vehicle, installs a monitoring camera under the unmanned aerial vehicle, and releases the unmanned aerial vehicle through the landing gear when taking off. However, during the scanning process of the unmanned aerial vehicle and the recovery operation process, it is difficult to control the unmanned aerial vehicle to land at a slow speed and in a horizontal attitude due to the operation of the technical personnel. Under the inertial action of the unmanned aerial vehicle, the bottom monitoring camera is easily damaged. In related technologies, a protective device is installed on the outside of the monitoring assembly. When the side or bottom is impacted, the detection assembly can be protected. When the bottom is impacted, the second protective plate is retracted to the inside of the first protective plate, and the monitoring assembly is retracted inwardly, which can play a protective role. However, since the monitoring assembly is installed at the bottom of the unmanned aerial vehicle, the protective plate surrounds the monitoring assembly, and the bottom of the protective plate needs to extend below the monitoring assembly to protect the monitoring assembly. Therefore, when the unmanned aerial vehicle is used for normal shooting, the field of view of the scanner is limited by the protective plate. When the camera needs to adjust the upward angle and shoot the front, it will be blocked by the protective plate, which affects the scanning work. SUMMARY

[0004] (I) Technical problem solved

[0005] In view of the deficiencies in the prior art, the utility model provides a topographic scanner, which has the advantages of protecting the scanner while the protective plate does not hinder the field of view of the scanner during normal flight of the aircraft, and solves the problem of the protective plate of the existing topographic scanner affecting the field of view of the scanner.

[0006] (II) Technical scheme

[0007] To achieve the above object, the utility model provides the following technical scheme: A topographic scanner, include: aircraft, its bottom is installed with mounting bracket, and the inside of aircraft is provided with battery; Scanner, install in the inside of mounting bracket; The inside of aircraft is provided with protection assembly; Protection assembly includes: drive mechanism, set up in the inside of aircraft; Moving plate, sliding connection is in the inside of aircraft, and moving plate is connected with drive mechanism; Limiting block, fixedly connected on the side surface of moving plate; Limiting mechanism, set up on the side surface of moving plate; Connecting plate, sliding connection is in the inside of aircraft, and connecting plate is in contact with limiting mechanism; No.

[0008] In some embodiments, the drive mechanism comprises: a micro motor fixedly connected to the inside of the aircraft, and the micro motor is electrically connected with the battery inside the aircraft; A threaded sleeve is fixedly connected to one end of the output end of the micro motor, and the threaded sleeve is rotatably connected to the inside of the aircraft; A threaded rod is threadedly connected to the inside of the threaded sleeve, and the bottom of the threaded rod is fixedly connected to the top of the moving plate.

[0009] In some embodiments, the limiting mechanism comprises: a limiting slider slidingly connected to the inside of the moving plate; A side slider is fixedly connected to both sides of the limiting slider; A first guide rod is fixedly connected to the inside of the moving plate, the first guide rod is slidingly connected to the side slider, and the first guide rod is externally sleeved with a spring.

[0010] In some embodiments, one end of the limiting slider protrudes from the inside of the moving plate, the protruding portion is provided with an inclined surface, and one side of the connecting plate is provided with a groove with the same height as the protruding portion of the limiting slider.

[0011] In some embodiments, the limiting block, the limiting slider and the connecting plate are a group, the side surface of the moving plate is provided with two groups, and the two groups are symmetrically arranged.

[0012] In some embodiments, the number of protection plates is two, and the two protection plates are connected with the connecting plate through a mounting assembly; The mounting assembly comprises: a plug block fixedly connected to one end of the protection plate; A plug groove is formed in the inside of the other end of the protection plate; A mounting hole is formed in the top and bottom of the plug groove; A threaded hole is formed in the inside of the plug block.

[0013] In some embodiments, the diameter of the mounting hole is greater than the diameter of the threaded hole.

[0014] In some embodiments, the moving plate is located inside the aircraft and above the mounting rack, and the moving plate does not contact the mounting rack during movement.

[0015] (III) Beneficial Effects

[0016] Compared with the prior art, the terrain scanner has the following beneficial effects:

[0017] The utility model discloses a driving mechanism is started only, drive moving board moves down, will drive limit sliding block to withdraw to the inside of moving board to the limit of connecting plate is removed, and the connecting plate can be pushed down under the action of the spring outside no. BRIEF DESCRIPTION OF DRAWINGS

[0018] Figure 1 It is the structural schematic diagram of the utility model;

[0019] Figure 2 It is the structural schematic diagram of the utility model protection subassembly;

[0020] Figure 3 It is the structural schematic diagram of the utility model limit mechanism;

[0021] Figure 4 It is the structural schematic diagram of the utility model installation component.

[0022] In the drawing:

[0023] 11, aircraft; 12, mounting rack; 13, scanner;

[0024] 2, protection subassembly; 21, driving mechanism; 211, micro motor; 212, threaded sleeve; 213, threaded rod; 22, moving plate; 23, limit block; 24, limit mechanism; 241, limit sliding block; 242, side sliding block; 243, one guide rod; 25, connecting plate; 26, two guide rods; 27, protection plate;

[0025] 3, installation component; 31, plug block; 32, slot; 33, mounting hole; 34, threaded hole. DETAILED DESCRIPTION

[0026] With reference to the drawings of the embodiments of the present application, the technical solutions in the embodiments of the present application will be clearly and completely described. Obviously, the described embodiments are only a part of the embodiments of the present application, but not all the embodiments of the present application. Based on the embodiments of the present application, all the other embodiments obtained by a person of ordinary skill in the art without creative work under the premise that the embodiments of the present application fall within the protection scope of the present application.

[0027] It should be noted that all the directionality indications in the embodiments of the present application are only used to explain the relative position relationship, motion condition and the like between components in a certain posture, and if the certain posture changes, the directionality indications also change accordingly.

[0028] In the present application, unless otherwise explicitly specified and limited, the terms “connection”, “fixation” and the like should be understood in a broad sense, for example, “fixation” can be fixed connection, or detachable connection, or integral; can be mechanical connection, or electrical connection; can be direct connection, or indirect connection through an intermediate medium; can be internal connection of two elements or interaction relationship between two elements, unless otherwise explicitly limited. For a person of ordinary skill in the art, the specific meaning of the above terms in the present application can be understood according to the specific circumstances.

[0029] In addition, the description such as “first”, “second” and the like in the present application is only for the purpose of description, and cannot be understood as indicating or implying the relative importance of the indicated technical features or implicitly indicating the number of the indicated technical features. Therefore, the features limited by “first”, “second” can explicitly or implicitly include at least one of the features. In addition, the technical solutions of each embodiment can be combined with each other, but it must be based on that a person of ordinary skill in the art can realize that when the combination of technical solutions appears contradictory or unachievable, it should be considered that the combination of technical solutions does not exist, and is not within the protection scope of the present application.

[0030] In use, the operator installs the scanner on the aircraft, starts the aircraft near the mine, and photographs and surveys the geological conditions of the mine through the scanner.

[0031] In the related art, the detection assembly can be protected when being impacted from the side or the bottom by installing a protective device outside the monitoring assembly, and when being impacted from the bottom, the second protective plate is retracted inside the first protective plate, and the monitoring assembly is retracted inwardly, thereby playing a protection role. However, since the monitoring assembly is installed at the bottom of the unmanned aerial vehicle, the protective plate surrounds the monitoring assembly, and the bottom of the protective plate needs to extend below the monitoring assembly to protect the monitoring assembly. Thus, when the unmanned aerial vehicle is used to normally shoot, the field of view of the scanner is limited by the protective plate, and when the camera needs to be adjusted upwardly to shoot the front, the protective plate is blocked, thereby affecting the scanning work.

[0032] In order to solve the problems in the related art to some extent, the embodiment of the present application provides a terrain scanner. Before the aircraft 11 needs to land, only the driving mechanism 21 needs to be started, the moving plate 22 is driven to move downwardly, the limiting sliding block 241 is retracted to the inside of the moving plate 22, thereby releasing the limiting of the connecting plate 25, the connecting plate 25 is pushed downwardly under the action of the spring outside the second guide rod 26, thereby driving the two protective plates 27 to slide out downwardly, the protective plates 27 slide to the below of the scanner 13, and when the aircraft 11 lands, the landing is buffered by the contact between the protective plates 27 and the ground, thereby reducing the damage to the aircraft 11. Meanwhile, when the aircraft 11 normally flies, the protective plates 27 are retracted to the inside of the aircraft 11, do not block the field of view of the scanner 13, and the practicability of the device is enhanced.

[0033] The present application will be described below in combination with the drawings and specific embodiments:

[0034] In combination with Figures 1-4 the embodiment of the present application provides a terrain scanner, which comprises an aircraft 11, a mounting frame 12 is installed at the bottom of the aircraft 11, and a storage battery is arranged in the inside of the aircraft 11; a scanner 13 is installed in the inside of the mounting frame 12; a protective assembly 2 is arranged in the inside of the aircraft 11; the protective assembly 2 comprises a driving mechanism 21 arranged in the inside of the aircraft 11; a moving plate 22 is slidingly connected to the inside of the aircraft 11, and the moving plate 22 is connected with the driving mechanism 21; a limiting block 23 is fixedly connected to the side surface of the moving plate 22; a limiting mechanism 24 is arranged at the side surface of the moving plate 22; a connecting plate 25 is slidingly connected to the inside of the aircraft 11, and the connecting plate 25 is in contact with the limiting mechanism 24; a second guide rod 26 is fixedly connected to the inside of the aircraft 11, the second guide rod 26 is slidingly connected to the two sides of the connecting plate 25, and a spring is arranged outside the second guide rod 26; and a protective plate 27 is fixedly installed at the bottom of the connecting plate 25.

[0035] In use, the aircraft 11 is started, so that the aircraft 11 is lifted, the mounting frame 12 is adjusted through the remote control device to change the orientation and angle of the scanner 13, the mine is scanned, before the aircraft 11 is landed, the micro motor 211 is started to drive the threaded sleeve 212 to rotate, because the limiting blocks 23 on the two sides of the moving plate 22 limit the rotation of the moving plate 22, so the threaded rod 213 slides downward together with the moving plate 22, which drives the limiting sliding block 241 to slide downward, the limiting sliding block 241 is pressed to contact the inside of the aircraft 11, so as to be retracted into the inside of the moving plate 22, thereby releasing the limiting of the connecting plate 25, the connecting plate 25 is pushed downward under the action of the spring outside the second guide rod 26, thereby driving the two protective plates 27 to slide out downward, the protective plates 27 slide to the lower side of the scanner 13, the damper is arranged outside the second guide rod 26, which can buffer the impact caused by the contact of the protective plates 27 with the ground, so that the landing can be buffered through the contact of the protective plates 27 with the ground when the aircraft 11 lands, thereby reducing the damage to the scanner 13, because the outside of the second guide rod 26 is a damping spring, when the protective plates 27 normally contact the ground and are impacted, the protective plates 27 will not be completely retracted into the inside of the aircraft 11 due to the impact, so that the probability of the scanner 13 contacting the ground in the vertical direction can be reduced, at the same time, when the aircraft 11 normally flies, the protective plates 27 are retracted into the inside of the aircraft 11, which does not block the field of view of the scanner 13, thereby enhancing the practicability of the device.

[0036] In some embodiments, the driving mechanism 21 comprises a micro motor 211 fixedly connected to the inside of the aircraft 11, and the micro motor 211 is electrically connected with the battery in the inside of the aircraft 11; a threaded sleeve 212 fixedly connected to the output end of the micro motor 211, and the threaded sleeve 212 is rotationally connected with the inside of the aircraft 11; and a threaded rod 213 threadedly connected to the inside of the threaded sleeve 212, and the bottom of the threaded rod 213 is fixedly connected with the top of the moving plate 22.

[0037] In use, because the limiting blocks 23 are fixedly arranged outside the moving plate 22, and the moving plate 22 and the limiting blocks 23 are both slidingly connected with the inside of the aircraft 11, the rotation of the micro motor 211 to drive the threaded sleeve 212 will not drive the threaded rod 213 to rotate, but will adjust the up-and-down movement of the threaded rod 213, thereby facilitating the retraction of the limiting sliding block 241 into the inside of the moving plate 22, and facilitating the operation.

[0038] In some embodiments, the limiting mechanism 24 comprises a limiting sliding block 241 slidingly connected to the inside of the moving plate 22; side sliding blocks 242 fixedly connected to the two sides of the limiting sliding block 241; and a first guide rod 243 fixedly connected to the inside of the moving plate 22, the first guide rod 243 is slidingly connected with the side sliding blocks 242, and the outside of the first guide rod 243 is sleeved with a spring.

[0039] In use, when the connecting plate 25 is positioned, the protective plate 27 and the connecting plate 25 are pushed upward, and in the process of upward movement of the connecting plate 25, the inclined surface at the bottom of the limiting slider 241 is pressed, so as to push the limiting slider 241 into the inside of the moving plate 22 and compress the spring outside the first guide rod 243. When the groove on one side of the connecting plate 25 reaches the position of the limiting slider 241, the limiting slider 241 is no longer pressed, and the limiting slider 241 is pushed out of the inside of the moving plate 22 under the action of the spring outside the first guide rod 243 and is inserted into the groove on one side of the connecting plate 25, so as to position the connecting plate 25 and facilitate installation.

[0040] In some embodiments, one end of the limiting slider 241 extends out of the inside of the moving plate 22, the extending part is provided with an inclined surface, and one side of the connecting plate 25 is provided with a groove with the same height as the extending part of the limiting slider 241, so that the connecting plate 25 is abutted by the top of the limiting slider 241, preventing the connecting plate 25 from sliding out of one side of the limiting slider 241 when the aircraft 11 normally flies, causing the protective plate 27 to slide out and affecting the field of view of the scanner 13.

[0041] In some embodiments, the limiting block 23, the limiting slider 241 and the connecting plate 25 form a group, and two groups are provided on the side surface of the moving plate 22 and are symmetrically arranged, so as to enhance the limiting effect.

[0042] In some embodiments, the number of protective plates 27 is two, and the two protective plates 27 are connected with the connecting plate 25 through the mounting assembly 3; the mounting assembly 3 comprises: an insertion block 31 fixedly connected to one end of the protective plate 27; an insertion slot 32 formed in the inside of the other end of the protective plate 27; a mounting hole 33 formed in the top and bottom of the insertion slot 32; and a threaded hole 34 provided in the inside of the insertion block 31.

[0043] In use, the insertion block 31 of one protective plate 27 is inserted into the insertion slot 32 on one side of the other protective plate 27, then the threaded hole 34 is aligned with the threaded hole at the bottom of the connecting plate 25, and a screw is screwed through the mounting hole 33 for fixation, which is convenient and fast.

[0044] In some embodiments, the diameter of the mounting hole 33 is greater than the diameter of the threaded hole 34, so as to facilitate hiding the head of the screw into the inside of the mounting hole 33.

[0045] In some embodiments, the moving plate 22 is located inside the aircraft 11 and above the mounting frame 12, and the moving plate 22 does not contact the mounting frame 12 during movement, so as to prevent the up-and-down movement of the moving plate 22 from interfering with the normal use of the mounting frame 12.

[0046] In the description of the specification, the description of the terms "one embodiment", "some embodiments", "an example", "a specific example", or "some examples" and the like means that the specific features, structures, materials or characteristics described in connection with the embodiment or example are included in at least one embodiment or example of the present application. In the specification, the illustrative description of the above terms does not necessarily refer to the same embodiment or example. Moreover, the specific features, structures, materials or characteristics described can be combined in any appropriate manner in any one or more embodiments or examples. In addition, those skilled in the art can combine and integrate different embodiments or examples described in the specification.

[0047] In addition, the technical solutions among various embodiments can be combined with each other, but it must be based on the fact that a person skilled in the art can realize it, and when the combination of technical solutions appears contradictory or cannot be realized, it should be considered that the combination of technical solutions does not exist and is not within the protection scope required by the present application.

[0048] Although the embodiments of the present application have been shown and described, it can be understood by those skilled in the art that various changes, modifications, replacements and variations can be made to the embodiments without departing from the principles and spirits of the present application, and the scope of the present application is defined by the appended claims and their equivalents.

Claims

1. A terrain scanner characterized by, Include: The aircraft (11) is mounted with a mounting bracket (12) at the bottom, and the inside of the aircraft (11) is provided with a battery; a scanner (13) is installed inside the mounting bracket (12); the inside of the aircraft (11) is provided with a protection assembly (2); the protection assembly (2) comprises: A driving mechanism (21) is provided inside the aircraft (11); a moving plate (22) is slidably connected to the inside of the aircraft (11), and the moving plate (22) is connected with the driving mechanism (21); a limiting block (23) is fixedly connected to the side of the moving plate (22); a limiting mechanism (24) is provided on the side of the moving plate (22); a connecting plate (25) is slidably connected to the inside of the aircraft (11), and the connecting plate (25) is in contact with the limiting mechanism (24); a second guide rod (26) is fixedly connected to the inside of the aircraft (11), the second guide rod (26) is slidably connected to the two sides of the connecting plate (25), and the outside of the second guide rod (26) is sleeved with a spring; a protection plate (27) is fixedly installed at the bottom of the connecting plate (25).

2. A terrain scanner according to claim 1, wherein, The driving mechanism (21) comprises: A micro motor (211) is fixedly connected to the inside of the aircraft (11), and the micro motor (211) is electrically connected with the battery inside the aircraft (11); a threaded sleeve (212) is fixedly connected to one end of the output end of the micro motor (211), and the threaded sleeve (212) is rotatably connected with the inside of the aircraft (11); a threaded rod (213) is threadedly connected to the inside of the threaded sleeve (212), and the bottom of the threaded rod (213) is fixedly connected with the top of the moving plate (22).

3. A terrain scanner according to claim 1, wherein, The limiting mechanism (24) comprises: A limiting slide block (241) is slidably connected to the inside of the moving plate (22); a side slide block (242) is fixedly connected to the two sides of the limiting slide block (241); a first guide rod (243) is fixedly connected to the inside of the moving plate (22), the first guide rod (243) is slidably connected with the side slide block (242), and the outside of the first guide rod (243) is sleeved with a spring.

4. A terrain scanner according to claim 3, wherein: One end of the limiting slide block (241) protrudes from the inside of the moving plate (22), the protruding part is provided with an inclined surface, and one side of the connecting plate (25) is provided with a groove with the same height as the protruding part of the limiting slide block (241).

5. A terrain scanner according to claim 3, wherein: The limiting block (23), the limiting slide block (241) and the connecting plate (25) are a group, the side of the moving plate (22) is provided with two groups, and they are symmetrically arranged.

6. A terrain scanner according to claim 1, wherein, The number of protection plates (27) is two, and the two protection plates (27) are connected with the connecting plate (25) through a mounting assembly (3); the mounting assembly (3) comprises: A plug (31) is fixedly connected to one end of the protection plate (27), a slot (32) is formed in the interior of the other end of the protection plate (27), mounting holes (33) are formed in the top and bottom of the slot (32), and threaded holes (34) are formed in the interior of the plug (31).

7. A terrain scanner according to claim 6, characterised in that: The diameter of the mounting holes (33) is larger than that of the threaded holes (34).

8. A terrain scanner according to claim 1, wherein: The moving plate (22) is located in the interior of the aircraft (11) and above the mounting rack (12), and the moving plate (22) does not contact the mounting rack (12) during movement.

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