A real-time display device for low-altitude aircraft monitoring

Abstract

The utility model discloses a real-time display device for monitoring low-altitude aircraft, relates to the field of real-time monitoring display technology, and is characterized in that it comprises a portable case, the lower end of the portable case is equipped with a universal self-locking wheel group, the rear end of the portable case is fixedly connected with a push-pull rod, the upper end of the partition is fixedly equipped with a bidirectional motor, the two output ends of the bidirectional motor are fixedly connected with a bevel gear 1, the bevel gear 1 is meshed with a bevel gear 2, the bevel gear 2 is fixedly connected to the surface of a threaded rod, the upper end surface of the threaded rod is threadedly connected with a lifting plate, the middle part of the upper end of the lifting plate is provided with a display component, and the lower side of the partition is provided with a drone storage box, the device allows the user to easily drag the box, thereby facilitating carrying, and at the same time, when not in use, the portable case can protect the display component and the drone from collision, and at the same time, the spring damper further protects the drone by absorbing and dissipating impact energy.

Description

Technical Field

[0001] The utility model relates to the technical field of real-time monitoring and display, in particular to a real-time display device for monitoring low-altitude aircraft. Background Art

[0002] Low-altitude aircraft, also referred to as "drones", are unmanned aircraft that are controlled by radio remote control equipment and self-contained program control devices, or are fully or intermittently operated autonomously by onboard computers. With the development of society, most users often monitor drones through real-time display devices.

[0003] Currently, most real-time display devices are fixed integrated designs, which are inconvenient to carry when working outside, and drones are easily damaged by collisions when carried. Based on this, this solution provides a real-time display device for low-altitude aircraft monitoring to solve the above-mentioned problems. Utility Model Content

[0004] In order to solve the above technical problems, a real-time display device for low-altitude aircraft monitoring is provided. This technical solution solves the problems raised in the above background technology.

[0005] In order to achieve the above purpose, the technical solution adopted by the utility model is:

[0006] A real-time display device for monitoring low-altitude aircraft, characterized in that it comprises a portable box, a universal self-locking wheel set is installed at the lower end of the portable box, a push-pull rod is fixedly connected to the rear end of the portable box, a box cover is rotatably installed on the left and right sides of the upper end of the portable box, a partition is fixedly connected to the inner wall of the portable box, a bidirectional motor is fixedly installed on the upper end of the partition, two output ends of the bidirectional motor are fixedly connected to bevel gear 1, the upper end of bevel gear 1 is meshed with bevel gear 2, and bevel gear 2 is fixedly connected to the surface of a threaded rod, the left end of the threaded rod is installed inside a fixed frame, the outer end of the fixed frame is fixedly connected to the inner wall of the portable box, the upper end surface of the threaded rod is threadedly connected to a lifting plate, a display component is provided at the middle part of the upper end of the lifting plate, and a drone storage box is provided on the lower side of the partition.

[0007] Preferably, the left and right sides of the upper end of the lifting plate are fixedly connected to fixed plates, the upper end of the fixed plate is fixedly connected to a connecting rod, the upper end of the connecting rod is hinged to the driving block, the driving block is slidably installed inside the slide groove, and the slide groove is opened at the inner end of the box cover.

[0008] Preferably, a slide rail is fixedly connected to the lower side of the inner wall of the portable box, a slider is fixedly connected to the outer end of the drone storage box, and the other end of the slider is slidably connected to the slide rail.

[0009] Preferably, a placement plate is provided inside the drone storage box, and a plurality of groups of spring dampers are fixedly mounted on the lower end of the placement plate.

[0010] Preferably, a limit plate is fixedly connected to the inner wall of the fixed frame, and the limit plate is arranged on the upper side of the bidirectional motor.

[0011] Preferably, the display assembly includes a display screen and an operating table, the operating table is fixedly mounted on the upper end of the lifting plate, and the display screen is rotatably mounted on the rear end of the operating table.

[0012] Compared with the prior art, the utility model proposes a real-time display device for low-altitude aircraft monitoring, which has the following beneficial effects:

[0013] 1. The utility model is provided with a universal self-locking wheel set and a push-pull rod, allowing the user to easily drag the box. The push-pull rod provides a comfortable handle to facilitate the movement of the box. The universal wheel can rotate 360 ​​degrees freely, so that the box can easily change direction. At the same time, the self-locking function can ensure that the wheels do not slide when the box is docked, increasing the advantage of the box in position stability.

[0014] 2. In the utility model, the display assembly is installed on the lifting plate. When not in use, the display assembly is stored in the portable box, so as to protect the display assembly from external impact. When it is needed, the bevel gear 1 on both sides is driven by the bidirectional motor, and the transmission is transmitted through the bevel gear 2, thereby driving the threaded rod to rotate, and the rotation of the threaded rod drives the lifting plate to move. During the movement of the lifting plate, the connecting rod is driven to move together through the fixed plate, and the other end of the connecting rod is hinged to the driving block, so that the driving block slides inside the slide groove, and the box cover is lifted by the driving block, so that the box cover opens as the lifting plate rises and closes when it falls.

[0015] 3. The utility model is provided with a drone storage box, and a placement plate is provided inside the box for placing the drone, and the drone is fixed and restrained by a fixing mechanism. A plurality of groups of spring dampers are connected to the lower end of the placement plate. The drone storage box is used to protect the drone from external collisions, and the spring dampers effectively control and reduce the vibration and impact of the drone by absorbing and dissipating the impact energy, thereby effectively protecting the safety of the drone. BRIEF DESCRIPTION OF THE DRAWINGS

[0016] Figure 1 It is a schematic diagram of the overall structure of the utility model;

[0017] Figure 2 It is a cross-sectional view of the storage structure of the display component in the utility model;

[0018] Figure 3 This is a schematic diagram of the connection structure between the lifting plate and the box cover in the utility model;

[0019] Figure 4 This is a cross-sectional view of the internal structure of the drone storage box in the utility model.

[0020] The numbers in the figure are:

[0021] 1. Portable box; 101. Partition; 102. Slide rail; 2. Box cover; 201. Slide groove; 202. Drive block; 3. Bidirectional motor; 4. Bevel gear one; 5. Bevel gear two; 6. Fixed frame; 601. Limit plate; 7. Threaded rod; 8. Lifting plate; 801. Fixed plate; 802. Connecting rod; 9. Display assembly; 10. UAV storage box; 1001. Slider; 11. Placement plate; 12. Spring damper; 13. Push-pull rod; 14. Universal self-locking wheel set. DETAILED DESCRIPTION

[0022] The following description is used to disclose the present invention so that those skilled in the art can implement the present invention. The preferred embodiments described below are only examples, and those skilled in the art may think of other obvious variations.

[0023] Reference Figure 1-4As shown, a real-time display device for low-altitude aircraft monitoring is characterized in that it includes a portable box 1, a universal self-locking wheel set 14 is installed at the lower end of the portable box 1, and a push-pull rod 13 is fixedly connected to the rear end of the portable box 1, allowing the user to easily drag the box. The push-pull rod 13 provides a comfortable handle for convenient movement of the box. The universal wheels can rotate freely 360 degrees, so that the box can easily change direction. At the same time, the self-locking function can ensure that the wheels do not slide when the box is docked, which increases the advantage of the box in positional stability. The upper left and right sides of the upper end of the portable box 1 are rotatably installed with a box cover 2, the inner wall of the portable box 1 is fixedly connected to a partition 101, and the upper end of the partition 101 is fixedly installed with a bidirectional motor 3. The two output ends of the bidirectional motor 3 are fixedly connected to a bevel gear 1 4, and the upper end of the bevel gear 1 4 is meshed with a bevel gear 2 5. The bevel gear 2 5 is fixedly connected to the surface of the threaded rod 7, and the left end of the threaded rod 7 is fixedly installed on the fixed Inside the frame 6, the outer end of the fixed frame 6 is fixedly connected to the inner wall of the portable box 1, the upper end surface of the threaded rod 7 is threadedly connected with a lifting plate 8, and a display component 9 is arranged in the middle of the upper end of the lifting plate 8. The left and right sides of the upper end of the lifting plate 8 are fixedly connected with fixed plates 801, and the upper end of the fixed plate 801 is fixedly connected with a connecting rod 802, and the upper end of the connecting rod 802 is hinged to the driving block 202, and the driving block 202 is slidably installed inside the slide groove 201, and the slide groove 201 is opened at the inner end of the box cover 2. When not in use, the display assembly 9 is stored in the portable box 1, so as to protect the display assembly 9 from external impact. When it is needed, the bidirectional motor 3 drives the bevel gear 1 4 on both sides, and the bevel gear 2 5 is driven to drive the threaded rod 7 to rotate. The threaded rod 7 rotates and drives the lifting plate 8 to move. During the movement of the lifting plate 8, the connecting rod 802 is driven to move together through the fixed plate 801. The other end of the connecting rod 802 is hinged to the driving block 202, so that the driving block 202 slides inside the slide groove 201, and the box cover 2 is lifted by the driving block 202, so that the box cover 202 is opened when the lifting plate 8 rises and closed when it falls.

[0024] Specifically, in this embodiment, a slide rail 102 is fixedly connected to the lower side of the inner wall of the portable box 1 , a slider 1001 is fixedly connected to the outer end of the drone storage box 10 , and the other end of the slider 1001 is slidably connected to the slide rail 102 .

[0025] Specifically, in this embodiment, a placement plate 11 is provided inside the drone storage box 10, and a plurality of groups of spring dampers 12 are fixedly installed at the lower end of the placement plate 11. The placement plate 11 is used to place the drone, and the drone is fixedly restrained by a fixing mechanism (not shown in the figure). The lower end of the placement plate 11 is connected with a plurality of groups of spring dampers 12. The drone storage box 10 is used to protect the drone from external collisions, and the spring dampers 12 absorb and dissipate impact energy, effectively control and reduce the vibration and impact of the drone, and thus effectively protect the safety of the drone.

[0026] Specifically, in this embodiment, the inner wall of the fixed frame 6 is fixedly connected with a limit plate 601, and the limit plate 601 is arranged on the upper side of the bidirectional motor 3. The limit plate 601 is used to protect the motor.

[0027] Specifically, in this embodiment, the display assembly 9 includes a display screen and an operating table. The operating table is fixedly mounted on the upper end of the lifting plate 8, and the display screen is rotatably mounted on the rear end of the operating table.

[0028] The working principle of the utility model is as follows: the user moves the portable box 1 to a predetermined position through the push-pull rod 13 and the universal self-locking wheel set 14, and then the self-locking function can ensure that the wheels do not slide when the box is docked, thereby increasing the advantage of the box in position stability, and then the bidirectional motor 3 drives the bevel gear 1 4 on both sides, and the bevel gear 2 5 is driven to drive the threaded rod 7 to rotate, and the threaded rod 7 rotates to drive the lifting plate 8 to move. During the movement of the lifting plate 8, the connecting rod 802 is driven to move together through the fixed plate 801, and the other end of the connecting rod 802 is hinged to the driving block 202, so that the driving block 202 slides inside the slide groove 201, so that the box cover 2 is lifted up by the driving block 202, and the drone storage box 10 is pulled out, and the drone is started by controlling the operating table.

[0029] When not in use, the display assembly 9 is stored in the portable box 1, so as to protect the display assembly 9 from external impact. The drone is placed on the placement plate 11 and fixed and restrained by a fixing mechanism (not shown in the figure). The lower end of the placement plate 11 is connected to a plurality of groups of spring dampers 12. The drone storage box 10 is used to protect the drone from external collisions. The spring dampers 12 effectively control and reduce the vibration and impact of the drone by absorbing and dissipating the impact energy, thereby effectively protecting the safety of the drone.

[0030] The above shows and describes the basic principle, main features and advantages of the utility model. Those skilled in the art should understand that the utility model is not limited by the above embodiments. The above embodiments and the specification only describe the principles of the utility model. The utility model may be subject to various changes and improvements without departing from the spirit and scope of the utility model. These changes and improvements fall within the scope of the utility model to be protected. The scope of protection claimed by the utility model is defined by the attached claims and their equivalents.

Claims

1. A real-time display device for low-altitude aircraft monitoring, characterized in that: The portable box (1) comprises a universal self-locking wheel set (14) installed at the lower end of the portable box (1), a push-pull rod (13) fixedly connected to the rear end of the portable box (1), a box cover (2) rotatably installed on both the left and right sides of the upper end of the portable box (1), a partition (101) fixedly connected to the inner wall of the portable box (1), a bidirectional motor (3) fixedly installed on the upper end of the partition (101), and both output ends of the bidirectional motor (3) fixedly connected to a bevel gear 1 (4), and the bevel gear 1 The upper end of the bevel gear (4) is meshed with the bevel gear (5), the bevel gear (5) is fixedly connected to the surface of the threaded rod (7), the left end of the threaded rod (7) is installed inside the fixed frame (6), the outer end of the fixed frame (6) is fixedly connected to the inner wall of the portable box (1), the upper end surface of the threaded rod (7) is threadedly connected with a lifting plate (8), the middle part of the upper end of the lifting plate (8) is provided with a display assembly (9), and the lower side of the partition (101) is provided with a drone storage box (10).

2. A real-time display device for low-altitude aircraft monitoring according to claim 1, characterized in that: The upper end of the lifting plate (8) is fixedly connected to a fixed plate (801) on both left and right sides, the upper end of the fixed plate (801) is fixedly connected to a connecting rod (802), the upper end of the connecting rod (802) is hinged to the driving block (202), the driving block (202) is slidably installed inside the sliding groove (201), and the sliding groove (201) is opened at the inner side end of the box cover (2).

3. A real-time display device for low-altitude aircraft monitoring according to claim 1, characterized in that: A slide rail (102) is fixedly connected to the lower side of the inner wall of the portable box (1), a slider (1001) is fixedly connected to the outer end of the drone storage box (10), and the other end of the slider (1001) is slidably connected to the slide rail (102).

4. A real-time display device for low-altitude aircraft monitoring according to claim 1, characterized in that: A placement plate (11) is provided inside the drone storage box (10), and a plurality of groups of spring dampers (12) are fixedly mounted on the lower end of the placement plate (11).

5. A real-time display device for low-altitude aircraft monitoring according to claim 1, characterized in that: A limit plate (601) is fixedly connected to the inner wall of the fixed frame (6), and the limit plate (601) is arranged on the upper side of the bidirectional motor (3).

6. A real-time display device for low-altitude aircraft monitoring according to claim 1, characterized in that: The display assembly (9) comprises a display screen and an operating table, wherein the operating table is fixedly mounted on the upper end of the lifting plate (8), and the display screen is rotatably mounted on the rear end of the operating table.

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