Unmanned aerial vehicle test tube transport case with damping function

Abstract

The utility model discloses an unmanned aerial vehicle test tube transportation box with a damping function, and belongs to the technical field of test tube transportation. The unmanned aerial vehicle test tube transport case with the damping function comprises a case body with a case cover; the fixing frame is detachably connected to the box body; the placing groove is formed in the fixing frame; the test tube is arranged in the placing groove; the gasket is connected in the placing groove; one end of the spring is fixedly connected to the inner bottom wall of the placing groove, and the other end of the spring is fixedly connected to the gasket; a limiting sleeve is fixedly connected in the placing groove, and the test tube is attached to the inner wall of the limiting sleeve; the test tubes are transported through the fixing frame in the device, a good fixing effect on the test tubes is achieved, vibration energy in the transportation process can be effectively absorbed through the gaskets and the springs arranged in the fixing frame, and then the transportation damping effect can be effectively achieved.

Description

TECHNICAL FIELD

[0001] The utility model relates to test tube transportation technical field especially, a kind of unmanned aerial vehicle test tube transport case with shock-absorbing function. BACKGROUND

[0002] With the progress of science and technology, unmanned aerial vehicle is increasingly widely used in medical treatment, transportation and other fields, especially in short-distance medical sample collection and other scenarios, unmanned aerial vehicle test tube transportation shows great potential. However, the existing unmanned aerial vehicle test tube transport case has deficiencies in shock-absorbing design. During flight, due to factors such as airflow fluctuation, take-off and landing vibration, test tubes are easily subjected to external impact, causing internal samples to be damaged or leaked, which seriously affects transportation safety and the accuracy of subsequent test results. Therefore, it is particularly important to develop an unmanned aerial vehicle test tube transport case with shock-absorbing function.

[0003] Most of the unmanned aerial vehicle test tube transport cases on the market currently use simple foam or sponge filling to achieve shock absorption, but this method is not effective in dealing with complex vibration environments, and the filling material is prone to aging and deformation after long-term use, which may cause the shock-absorbing performance to decrease. In addition, although some high-end transport cases use advanced shock-absorbing technology, the cost is high and it is difficult to popularize and apply. UTILITY MODEL CONTENT

[0004] The utility model aims at solving the problems raised in the above background art and proposes an unmanned aerial vehicle test tube transport case with shock-absorbing function.

[0005] To achieve the above-mentioned purpose, the utility model adopts the following technical solutions:

[0006] An unmanned aerial vehicle test tube transport case with shock-absorbing function comprises:

[0007] a box body with a box cover;

[0008] a fixing frame detachably connected to the box body;

[0009] a placing groove opened in the fixing frame;

[0010] a test tube installed in the placing groove;

[0011] a gasket connected in the placing groove;

[0012] the bottom of the test tube abuts against the gasket;

[0013] a spring fixedly connected at one end to the inner bottom wall of the placing groove and at the other end to the gasket.

[0014] Preferably, a limiting sleeve is fixedly connected in the placing groove, and the test tube abuts against the inner wall of the limiting sleeve.

[0015] Preferably, a limiting slot is formed on the box body, a limiting block is fixedly connected to the fixing frame, and the limiting block is matched with the limiting slot.

[0016] Further, a first magnet is fixedly connected to the fixing frame, a second magnet is fixedly connected to the bottom of the limiting slot, and the first magnet and the second magnet are attracted to each other.

[0017] Preferably, a connecting plate is fixedly connected to the sidewall of the box body, and a hanging rope is fixedly connected to the connecting plate.

[0018] Compared with the prior art, the unmanned aerial vehicle test tube transport box with the damping function has the following beneficial effects:

[0019] The parts not involved in the device are the same as or can be realized by the prior art, the fixing frame in the device is used for transporting test tubes, has a good fixing effect on the test tubes, and the gasket and the spring arranged in the fixing frame can effectively absorb the vibration energy in the transportation process, thereby effectively realizing the transportation damping effect. BRIEF DESCRIPTION OF DRAWINGS

[0020] Figure 1 A structure schematic view of the unmanned aerial vehicle test tube transport box with the damping function is provided.

[0021] Figure 2 A structure schematic view of the unmanned aerial vehicle test tube transport box with the damping function when the box cover is opened is provided.

[0022] Figure 3 A sectional view of the unmanned aerial vehicle test tube transport box with the damping function is provided.

[0023] Figure 4 A structure schematic view of the fixing frame in the unmanned aerial vehicle test tube transport box with the damping function is provided.

[0024] Figure 5 A sectional view of the fixing frame in the unmanned aerial vehicle test tube transport box with the damping function is provided.

[0025] In the drawing: 1, box body; 101, connecting plate; 1011, hanging rope; 102, limiting slot; 103, second magnet; 2, box cover; 3, fixing frame; 301, placing groove; 3011, limiting sleeve; 3012, spring; 302, gasket; 303, first magnet; 304, limiting block; 4, test tube. 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 part of the embodiments of the present application, rather than all the embodiments.

[0027] Embodiments

[0028] 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 part of the embodiments of the present application, rather than all the embodiments. Figures 1-5 A test tube transportation box with damping function for unmanned aerial vehicle, comprising:

[0029] The box body 1 is provided with a box cover 2.

[0030] The fixing frame 3 is detachably connected to the box body 1.

[0031] The placing groove 301 is arranged on the fixing frame 3.

[0032] The test tube 4 is installed in the placing groove 301.

[0033] The gasket 302 is connected in the placing groove 301.

[0034] The bottom of the test tube 4 abuts against the gasket 302.

[0035] The spring 3012 is fixedly connected to the inner bottom wall of the placing groove 301 at one end and fixedly connected to the gasket 302 at the other end.

[0036] During use, the test tube 4 is placed in the placing groove 301, and the bottom of the test tube 4 abuts against the gasket 302. After a plurality of test tubes 4 are placed in the fixing frame 3, the box cover 2 can be rotated by the worker, and the transportation of the box body 1 can be started after the box cover 2 is closed.

[0037] The test tube 4 is transported by the fixing frame 3 in the device, which has a good fixing effect on the test tube 4. The gasket 302 and the spring 3012 arranged in the fixing frame 3 can effectively absorb the vibration energy in the transportation process, thereby effectively realizing the transportation damping effect.

[0038] It should be noted that the gasket 302 is a rubber pad.

[0039] The limiting sleeve 3011 is fixedly connected in the placing groove 301, and the test tube 4 abuts against the inner wall of the limiting sleeve 3011.

[0040] 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 part of the embodiments of the present application, rather than all the embodiments. Figure 3 、 Figure 5 The test tube 4 is limited by the limiting sleeve 3011, thereby avoiding shaking of the test tube 4 during transportation, and thereby ensuring the stability of the test tube 4 during transportation.

[0041] A limiting groove 102 is provided on the housing 1, and a limiting block 304 is fixedly connected to the fixing frame 3. The limiting block 304 matches the limiting groove 102.

[0042] Reference Figure 2 , Figure 3 The limiting block 304 and the limiting groove 102 are used to lock the fixture, thereby ensuring the stability of the fixing frame 3 installed in the housing 1.

[0043] A first magnet 303 is fixedly connected to the fixed frame 3, and a second magnet 103 is fixedly connected to the bottom of the limiting groove 102. The first magnet 303 and the second magnet 103 attract each other.

[0044] Reference Figure 3 The stability of the mounting bracket 3 installed in the housing 1 can be further ensured by the attraction between the first magnet 303 and the second magnet 103.

[0045] A connecting plate 101 is fixedly connected to the side wall of the box 1, and a hanging rope 1011 is fixedly connected to the connecting plate 101.

[0046] Reference Figure 1 , Figure 2 By using the hanging rope 1011 set on the side wall of the container 1, the hanging rope 1011 can be hung on the drone during transportation, thereby avoiding the impact of drone vibration caused by rigid connection on the container 1, and further realizing the shock absorption of this transport container.

[0047] The above description is only a preferred embodiment of the present utility model, but the protection scope of the present utility model is not limited thereto. Any equivalent substitutions or changes made by those skilled in the art within the technical scope disclosed in the present utility model, based on the technical solution and inventive concept of the present utility model, should be included within the protection scope of the present utility model.

Claims

1. A unmanned aerial vehicle test tube transport case with shock absorption function, characterized in that, The utility model relates to a box body (1) with box cover (2), fixing frame (3) can be detachably connected on box body (1), placing groove (301) is set up on fixing frame (3), test tube (4) is installed in placing groove (301), gasket (302) is connected in placing groove (301), the bottom of test tube (4) is in contact with gasket (302), one end of spring (3012) is fixedly connected on the inner bottom wall of placing groove (301), and the other end is fixedly connected on gasket (302). The utility model discloses a box body (1) with box cover (2), fixing frame (3) can be detachably connected on box body (1), placing groove (301) is set up on fixing frame (3), test tube (4) is installed in placing groove (301), gasket (302) is connected in placing groove (301), the bottom of test tube (4) is in contact with gasket (302), one end of spring (3012) is fixedly connected on the inner bottom wall of placing groove (301), and the other end is fixedly connected on gasket (302). The utility model discloses a box body (1) with box cover (2), fixing frame (3) can be detachably connected on box body (1), placing groove (301) is set up on fixing frame (3), test tube (4) is installed in placing groove (301), gasket (302) is connected in placing groove (301), the bottom of test tube (4) is in contact with gasket (302), one end of spring (3012) is fixedly connected on the inner bottom wall of placing groove (301), and the other end is fixedly connected on gasket (302). The utility model discloses a box body (1) with box cover (2), fixing frame (3) can be detachably connected on box body (1), placing groove (301) is set up on fixing frame (3), test tube (4) is installed in placing groove (301), gasket (302) is connected in placing groove (301), the bottom of test tube (4) is in contact with gasket (302), one end of spring (3012) is fixedly connected on the inner bottom wall of placing groove (301), and the other end is fixedly connected on gasket (302). The utility model discloses a box body (1) with box cover (2), fixing frame (3) can be detachably connected on box body (1), placing groove (301) is set up on fixing frame (3), test tube (4) is installed in placing groove (301), gasket (302) is connected in placing groove (301), the bottom of test tube (4) is in contact with gasket (302), one end of spring (3012) is fixedly connected on the inner bottom wall of placing groove (301), and the other end is fixedly connected on gasket (302). ​ ​ ​ 2.The unmanned aerial vehicle test tube transport case with a shock absorption function of claim 1, wherein, ​ 3.The unmanned aerial vehicle test tube transport case with shock absorption function of claim 1, wherein, ​ 4. The unmanned aerial vehicle test tube transport box with shock absorption function according to claim 3, characterized in that, ​ 5. The unmanned aerial vehicle test tube transport box with shock absorption function according to claim 1, characterized in that, ​

Images