Flight information monitoring equipment for unmanned aerial vehicle

Abstract

The utility model belongs to the technical field of information monitoring equipment, and discloses flight information monitoring equipment for an unmanned aerial vehicle, which comprises a box body, a box cover is mounted on the box body in a hinged manner, a lock catch is mounted between the box body and the box cover, the box body is provided with a placement groove and a power supply mounting groove, and the power supply mounting groove is provided with a power supply. A wire hole is formed between the power supply mounting groove and the placement groove, a power supply connecting wire plate is mounted at the bottom in the power supply mounting groove, a power supply is placed in the power supply mounting groove in a plug-in manner, a handle is mounted on the power supply, a baffle lock is mounted on the box body, a flight information monitor is placed in the placement groove, and a partition plate is placed in the placement groove. By the adoption of the structural design, the arrangement of the box body and the box cover and the handle installed in cooperation with the power source, the unmanned aerial vehicle and the flight information monitor can be packed together, taken out and moved, moving is convenient, and meanwhile the containing area is saved.

Description

Technical Field

[0001] This utility model belongs to the field of information monitoring equipment technology, specifically relating to a flight information monitoring device for unmanned aerial vehicles. Background Technology

[0002] Unmanned Aerial Vehicles (UAVs), also known as drones, are aircraft that do not require a pilot and are controlled by remote control or autonomous programs. The flight information monitor of an UAV serves as a terminal for feeding back visual information from the UAV.

[0003] Because it consists of two parts, two loading objects are needed to move them, which makes movement inconvenient. Utility Model Content

[0004] In view of the problems mentioned above in the background technology, the purpose of this utility model is to provide a flight information monitoring device for unmanned aerial vehicles.

[0005] To achieve the above-mentioned technical objectives, the technical solution adopted by this utility model is as follows:

[0006] A flight information monitoring device for an unmanned aerial vehicle (UAV) includes a housing with a hinged lid. A latch is installed between the housing and the lid. The housing has a placement slot and a power supply mounting slot. A wire hole is provided between the power supply mounting slot and the placement slot. A power connection board is installed at the bottom of the power supply mounting slot. A power supply is plugged into the power supply mounting slot. The power supply has a handle. The housing is equipped with a baffle lock, with the actuating end of the baffle lock located on the outer side of the power supply. A flight information monitor is placed in the placement slot. A partition is placed above the flight information monitor in the placement slot. A limiting slot is provided on the partition, and the UAV is placed in the limiting slot.

[0007] Furthermore, the casing has a charging port on the side, which allows the power supply to be used as a power bank, expanding its functionality.

[0008] Furthermore, the box lid is equipped with a document storage bag, which can be used as a place to store paper documents for data recording.

[0009] Furthermore, when the lid is fastened to the box body, the upper surface of the unmanned aerial vehicle (UAV) contacts the top inside the lid. This design allows the UAV to be confined during movement, preventing collisions.

[0010] Further defining the design, the baffle lock includes a straight plate rotatably mounted on the housing and a semi-circular groove on the surface of the housing. The straight plate has a spring groove, and a moving block is slidably mounted on the spring groove. A hemisphere with dimensions matching the semi-circular groove is integrally mounted on the moving block. A spring is installed between the moving block and the spring groove. A lever is integrally connected to the surface of the straight plate. With this design, moving the lever causes the end of the straight plate to move away from the power supply, allowing the power supply to be directly pulled out of the power supply mounting slot. Conversely, moving the lever causes the end of the straight plate to be outside the power supply, preventing the power supply from detaching from the power supply mounting slot. Moreover, the cooperation of the spring, hemisphere, and semi-circular groove also makes it difficult for the straight plate to move on its own.

[0011] The beneficial effects of using this utility model are as follows:

[0012] The structural design of this utility model, with its box body and lid, along with the handle for power supply installation, allows the unmanned aerial vehicle and flight information monitor to be packed together for easy transport while saving storage space.

[0013] The structural design and power supply configuration of this utility model ensure the usage time of the flight information monitor and also allow it to be used as a power bank, thus expanding its functionality.

[0014] With the structural design of this utility model, the flight information monitor located in the box can be shielded from light by the box cover during use, thereby preventing reflection problems. Attached Figure Description

[0015] This utility model can be further illustrated by the non-limiting embodiments given in the accompanying drawings;

[0016] Figure 1 This is a schematic diagram of the structure of an embodiment of the flight information monitoring device for unmanned aerial vehicles according to the present invention;

[0017] Figure 2 This is a schematic diagram of the structure of an embodiment of the flight information monitoring device for unmanned aerial vehicles when it is turned on;

[0018] Figure 3 This is a cross-sectional structural schematic diagram of an embodiment of a flight information monitoring device for unmanned aerial vehicles according to the present invention;

[0019] Figure 4 This is a schematic cross-sectional view of a baffle lock structure according to an embodiment of the flight information monitoring device for unmanned aerial vehicles of this utility model;

[0020] The symbols for the main components are explained below:

[0021] 1. Case body; 2. Case lid; 3. Lock; 4. Storage slot; 5. Power supply mounting slot; 6. Power connection strip; 7. Power supply; 8. Handle; 9. Baffle lock; 10. Flight information monitor; 11. Divider; 12. Limiting slot; 13. Unmanned aerial vehicle; 14. Charging interface; 15. Document storage bag;

[0022] Straight plate 91; semi-circular groove 92; spring groove 93; moving block 94; hemisphere 95; spring 96; dial 97. Detailed Implementation

[0023] To enable those skilled in the art to better understand this utility model, the technical solution of this utility model will be further described below in conjunction with the accompanying drawings and embodiments.

[0024] like Figures 1-4 As shown, this utility model discloses a flight information monitoring device for unmanned aerial vehicles (UAVs), comprising a housing 1, a cover 2 hinged to the housing 1, a latch 3 between the housing 1 and the cover 2, a placement slot 4 and a power supply mounting slot 5, a wire hole between the power supply mounting slot 5 and the placement slot 4, a power connection plate 6 installed at the bottom inside the power supply mounting slot 5, a power supply 7 plugged into the power supply mounting slot 5, a handle 8 installed on the power supply 7, a baffle lock 9 installed on the housing 1, the active end of the baffle lock 9 being located on the outer side of the power supply 7, a flight information monitor 10 placed in the placement slot 4, a partition 11 placed above the flight information monitor 10 in the placement slot 4, a limiting groove 12 provided on the partition 11, and an UAV 13 placed in the limiting groove 12.

[0025] In this implementation case, when using a flight information monitoring device for unmanned aerial vehicles, the handle 8 allows the housing 1 to be easily moved to the usage position. The handle 8 is located on the power supply 7, which also facilitates the removal of the power supply 7 from the power supply mounting slot 5. After moving the device to the usage position, the latch 3 is opened to open the housing 2, and then the unmanned aerial vehicle 13 inside can be taken out. The partition 11 is removed, and the device can be used in conjunction with the flight information monitor 10 to achieve the intended purpose.

[0026] During use, both the cover 2 and the partition 11 can be used as sunshade components. When the power supply 7 needs to be replaced, the baffle lock 9 can be removed to directly pull the power supply 7 out of the power supply mounting slot 5 for replacement.

[0027] In summary, it has a compact structure and is easy to use.

[0028] The preferred housing 1 has a charging port 14 on the side. This design allows the power supply 7 to be used as a power bank, expanding its functionality. In fact, the style of the charging port 14 can also be selected according to the specific situation.

[0029] The preferred lid 2 has a document storage bag 15 installed inside. This design can be used as a place to store paper documents for data recording. In fact, the number and size of the document storage bags 15 can also be considered according to specific circumstances.

[0030] When the lid 2 is fastened to the body 1, the upper surface of the unmanned aerial vehicle 13 contacts the top inside the lid 2. This design allows the unmanned aerial vehicle 13 to be limited during movement without collision. In fact, limiting and fixing measures for the unmanned aerial vehicle 13 can also be considered according to specific circumstances.

[0031] The preferred baffle lock 9 includes a straight plate 91 rotatably mounted on the housing 1 and a semi-circular groove 92 on the surface of the housing 1. The straight plate 91 is provided with a spring groove 93, and a moving block 94 is slidably mounted on the spring groove 93. A hemisphere 95 with the same size and specifications as the semi-circular groove 92 is integrally mounted on the moving block 94. A spring 96 is installed between the moving block 94 and the spring groove 93. A dial 97 is integrally connected to the surface of the straight plate 91. With this design, by moving the dial 97, the end of the straight plate 91 is moved away from the power supply 7, and the power supply 7 can be directly pulled out of the power supply mounting slot 5. Conversely, by moving the dial 97, the end of the straight plate 91 is located outside the power supply 7, which can prevent the power supply 7 from detaching from the power supply mounting slot 5. Moreover, with the cooperation of the spring 96, the hemisphere 95 and the semi-circular groove 92, the straight plate 91 is not easy to move on its own. In fact, the choice of baffle lock 9 can also be considered according to specific circumstances.

[0032] The above embodiments are merely illustrative of the principles and effects of this utility model and are not intended to limit the scope of this utility model. Any person skilled in the art can modify or alter the above embodiments without departing from the spirit and scope of this utility model. Therefore, all equivalent modifications or alterations made by those skilled in the art without departing from the spirit and technical concept disclosed in this utility model should still be covered by the claims of this utility model.

Claims

1. A flight information monitoring device for an unmanned aerial vehicle, comprising a housing (1), wherein a housing (1) is hingedly fitted with a housing cover (2), characterized in that: A latch (3) is installed between the housing (1) and the cover (2). The housing (1) is provided with a placement slot (4) and a power installation slot (5). A wire hole is provided between the power installation slot (5) and the placement slot (4). A power connection board (6) is installed at the bottom of the power installation slot (5). A power supply (7) is plugged into the power installation slot (5). A handle (8) is installed on the power supply (7). A baffle lock (9) is installed on the housing (1). The working end of the baffle lock (9) is placed on the outer side of the power supply (7). A flight information monitor (10) is placed in the placement slot (4). A partition (11) is placed on the upper side of the flight information monitor (10) in the placement slot (4). A limiting slot (12) is provided on the partition (11). An unmanned aerial vehicle (13) is placed in the limiting slot (12).

2. The flight information monitoring device for unmanned aerial vehicles according to claim 1, characterized in that: The housing (1) has a charging port (14) on the side.

3. The flight information monitoring device for unmanned aerial vehicles according to claim 2, characterized in that: The box lid (2) has a document storage bag (15) installed inside.

4. The flight information monitoring device for unmanned aerial vehicles according to claim 3, characterized in that: When the lid (2) is fastened to the box body (1), the upper surface of the unmanned aerial vehicle (13) contacts the top inside the lid (2).

5. The flight information monitoring device for unmanned aerial vehicles according to claim 4, characterized in that: The baffle lock (9) includes a straight plate (91) rotatably mounted on the housing (1) and a semi-circular groove (92) provided on the surface of the housing (1). The straight plate (91) is provided with a spring groove (93). A moving block (94) is slidably mounted on the spring groove (93). A hemisphere (95) with a specification and size matching the semi-circular groove (92) is integrally mounted on the moving block (94). A spring (96) is installed between the moving block (94) and the spring groove (93). A dial (97) is integrally connected to the surface of the straight plate (91).

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