Inertial measurement support

By designing an inertial measurement bracket and using the combined structure of the damping block and the refrigeration plate, the problem of inertial measurement units on the drone is solved due to insufficient vibration and thermal management, and the accuracy and service life are improved.

CN222202918UActive Publication Date: 2024-12-20WUHAN LIKOV TECH CO LTD
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Patent Information

Application Number
CN202420508596.5
Authority / Receiving Office
CN · China
Patent Type
Utility models(China)
Current Assignee / Owner
Filing Date
2024-03-15
Publication Date
2024-12-20
Estimated Expiration
2034-03-15

AI Technical Summary

Technical Problem

The inertial measurement unit on the drone is affected by motor vibration during flight, resulting in a decrease in accuracy and insufficient thermal management, which affects the service life.

Method used

An inertial measurement bracket is designed, adopting a combined structure of the first and second damping blocks, telescopic rods, third damping blocks and refrigeration plates, and wraps the inertial measuring device through a support, a mount and a top cover to provide shock absorption. and heat dissipation effect.

Benefits of technology

It effectively reduces vibration of the inertial measuring device, improves accuracy, and extends its service life through the refrigeration plate.

✦ Generated by Eureka AI based on patent content.

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Abstract

The utility model provides an inertia measurement bracket which comprises a support, a mounting seat is arranged on the support, a first damping block and a plurality of telescopic rods are arranged between the support and the mounting seat, a second damping block is arranged in the mounting seat, a placing groove is formed in the second damping block, an inertia measurer is arranged in the placing groove, a top cover is arranged on the upper side of the mounting seat, and a plurality of telescopic rods are arranged on the top cover. A third damping block is fixed on one side, close to the inertial measurer, of the top cover, and a refrigeration sheet is fixed in the top cover. According to the utility model, the first damping block and the telescopic rod are mounted between the support and the mounting seat, so that a certain damping and buffering effect can be achieved, the second damping block is arranged in the mounting seat, and the third damping block is mounted on the top cover, so that the inertial measurement device can be wrapped, and further damping is performed on the inertial measurement device; and the refrigeration sheet is mounted in the top cover, so that heat dissipation can be performed on the inertial measurement device, and the service life of the inertial measurement device is prolonged.
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Description

Technical Field

[0001] The utility model relates to the technical field of brackets, in particular to an inertial measurement bracket. Background Art

[0002] An inertial measurement unit is a component that measures the speed and acceleration of an object in three-dimensional space and calculates the object's motion posture. It is usually composed of multiple sensors such as velocity sensors, acceleration sensors, and gyroscopes. The inertial measurement unit on a drone can monitor the flight status of the drone in real time. Existing inertial measurement units are generally placed in a cavity on a drone, but since the motor of a drone will vibrate during flight, the inertial measurement unit inside the drone will vibrate, and the inertial measurement unit is very sensitive to vibration, which affects the accuracy of the inertial measurement unit.

[0003] To this end, the utility model provides an inertial measurement bracket. Utility Model Content

[0004] In view of the deficiencies in the prior art, the purpose of the present invention is to provide an inertial measurement bracket to solve the problems raised in the above-mentioned background technology. The present invention can reduce the vibration of the inertial measurement unit, thereby ensuring the accuracy of the inertial measurement unit; it can also dissipate the heat of the inertial measurement unit to extend the service life of the inertial measurement unit.

[0005] In order to achieve the above-mentioned purpose, the utility model is realized through the following technical scheme: an inertial measurement bracket, including a support, a mounting base is installed on the support, a first damping block and a plurality of telescopic rods are installed between the support and the mounting base, a second damping block is installed in the mounting base, a placement groove is opened in the second damping block, an inertial measurement device is installed in the placement groove, a top cover is installed on the upper side of the mounting base, a third damping block is fixed on the side of the top cover close to the inertial measurement device, and a cooling plate is fixed in the top cover.

[0006] Furthermore, the upper and lower sides of the first damping block are respectively fixedly connected to the support and the mounting seat, and the two ends of the telescopic rod are respectively fixedly connected to the support and the mounting seat.

[0007] Furthermore, the support is provided with a plurality of mounting holes, and fixing bolts are installed in the mounting holes.

[0008] Furthermore, a mounting groove is provided in the mounting seat, the second damping block is fixed in the mounting groove, and a plurality of grooves are provided on the peripheral side of the second damping block.

[0009] Furthermore, a card block is fixed on the lower side of the top cover, and a card slot is opened on the mounting seat, the card slot corresponds to the card block, and the card block is made of rubber material.

[0010] Furthermore, the cooling plate includes a cooling surface and a heat dissipation surface, the cooling surface is in contact with the third damping block, a plurality of through grooves are provided in the third damping block, and both the third damping block and the second damping block are in contact with the inertial measurement unit.

[0011] Beneficial effects of the utility model: The utility model provides an inertial measurement bracket, comprising a support, a mounting seat, a first damping block, a telescopic rod, a second damping block, a top cover, a third damping block, an inertial measurement device, and a cooling plate.

[0012] Installing a first damping block and a telescopic rod between the support and the mounting seat can play a certain shock-absorbing and buffering role. Arranging a second damping block in the mounting seat and installing a third damping block on the top cover can wrap the inertial measurement unit, thereby further reducing the shock of the inertial measurement unit, thereby ensuring the accuracy of the inertial measurement unit. Installing a cooling plate in the top cover can dissipate the heat of the inertial measurement unit and extend the service life of the inertial measurement unit. BRIEF DESCRIPTION OF THE DRAWINGS

[0013] Figure 1 This is a schematic diagram of the overall assembly structure of an inertial measurement bracket of the utility model;

[0014] Figure 2 This is a schematic diagram of the overall assembly cross-sectional structure of an inertial measurement bracket of the utility model;

[0015] Figure 3 This is an exploded view of an inertial measurement bracket of the utility model;

[0016] In the figure: 1, support; 2, telescopic rod; 3, first damping block; 4, second damping block; 5, third damping block; 6, mounting seat; 7, mounting groove; 8, top cover; 9, cooling plate; 10, through groove; 11, clamping block; 12, clamping groove; 13, placement groove; 14, inertial measurement unit; 15, mounting hole; 16, groove. DETAILED DESCRIPTION

[0017] In order to make the technical means, creative features, objectives and effects achieved by the present invention easy to understand, the present invention is further described below in conjunction with specific implementation methods.

[0018] See also Figures 1 to 3 The utility model provides a technical solution: an inertial measurement bracket, including a support 1, a mounting base 6 is installed on the support 1, a first damping block 3 and a plurality of telescopic rods 2 are installed between the support 1 and the mounting base 6, a second damping block 4 is installed in the mounting base 6, a placement groove 13 is opened in the second damping block 4, an inertial measurement device 14 is installed in the placement groove 13, a top cover 8 is installed on the upper side of the mounting base 6, a third damping block 5 is fixed on the side of the top cover 8 close to the inertial measurement device 14, and a cooling plate 9 is fixed in the top cover 8.

[0019] In this embodiment, the upper and lower sides of the first damping block 3 are fixedly connected to the support 1 and the mounting seat 6 respectively, and the two ends of the telescopic rod 2 are fixedly connected to the support 1 and the mounting seat 6 respectively. A plurality of mounting holes 15 are opened on the support 1, and fixing bolts are installed in the mounting holes 15.

[0020] Specifically, when the device needs to be installed, the support 1 is fixed in the cavity of the drone by fixing bolts, and the fixing bolts pass through the mounting holes 15 and are threadedly installed with the drone to fix the support 1. At this time, the first damping block 3 can play a certain shock-absorbing role.

[0021] A mounting groove 7 is provided in the mounting seat 6, and the second damping block 4 is fixed in the mounting groove 7. A plurality of grooves 16 are provided on the peripheral side of the second damping block 4. A clamping block 11 is fixed on the lower side of the top cover 8. A clamping groove 12 is provided on the mounting seat 6, and the clamping groove 12 corresponds to the clamping block 11. The clamping block 11 is made of rubber material.

[0022] Specifically, after the support 1 is installed, the second damping block 4 is placed in the installation groove 7, and then the inertial measurement unit 14 is placed in the placement groove 13, and the block 11 of the top cover 8 is inserted into the slot 12. At this time, the third damping block 5 squeezes the inertial measurement unit 14 from the upper side downward, and the third damping block 5 cooperates with the second damping block 4 to completely wrap the inertial measurement unit 14, thereby further reducing the shock of the inertial measurement unit 14 and ensuring the accuracy of the inertial measurement unit 14. At the same time, compared with directly fixing the inertial measurement unit 14 with bolts or damping glue, the clamping fixation facilitates the disassembly and installation of the inertial measurement unit 14.

[0023] The cooling plate 9 includes a cooling surface and a heat dissipation surface. The cooling surface contacts the third damping block 5 . A plurality of through slots 10 are provided in the third damping block 5 . Both the third damping block 5 and the second damping block 4 contact the inertial measurement device 14 .

[0024] Specifically, when the inertial measurement unit 14 is working, it will generate heat. The cooling plate 9 is powered on to cool the cooling plate 9. The cooling surface can cool the inertial measurement unit 14, thereby preventing the inertial measurement unit 14 from having its service life reduced due to excessive temperature.

[0025] In addition, it should be understood that although the present specification is described according to implementation modes, not every implementation mode contains only one independent technical solution. This description of the specification is only for the sake of clarity. Those skilled in the art should regard the specification as a whole. The technical solutions in each embodiment may also be appropriately combined to form other implementation modes that can be understood by those skilled in the art.

Claims

1. An inertial measurement bracket, comprising a bracket (1), characterized in that: The support (1) is provided with a mounting seat (6), a first damping block (3) and a plurality of telescopic rods (2) are provided between the support (1) and the mounting seat (6), a second damping block (4) is provided in the mounting seat (6), a placement groove (13) is provided in the second damping block (4), an inertia measuring device (14) is provided in the placement groove (13), a top cover (8) is provided on the upper side of the mounting seat (6), a third damping block (5) is fixed on a side of the top cover (8) close to the inertia measuring device (14), and a cooling plate (9) is fixed in the top cover (8).

2. An inertial measurement bracket according to claim 1, characterized in that: The upper and lower sides of the first damping block (3) are respectively fixedly connected to the support (1) and the mounting seat (6), and the two ends of the telescopic rod (2) are respectively fixedly connected to the support (1) and the mounting seat (6).

3. The inertial measurement bracket according to claim 1, characterized in that: The support (1) is provided with a plurality of mounting holes (15), and fixing bolts are installed in the mounting holes (15).

4. The inertial measurement bracket according to claim 1, characterized in that: A mounting groove (7) is provided in the mounting seat (6), the second damping block (4) is fixed in the mounting groove (7), and a plurality of grooves (16) are provided on the circumference of the second damping block (4).

5. The inertial measurement bracket according to claim 1, characterized in that: A clamping block (11) is fixed on the lower side of the top cover (8), a clamping slot (12) is provided on the mounting seat (6), the clamping slot (12) corresponds to the clamping block (11), and the clamping block (11) is made of rubber material.

6. The inertial measurement bracket according to claim 1, characterized in that: The cooling plate (9) comprises a cooling surface and a heat dissipation surface, the cooling surface is in contact with the third damping block (5), a plurality of through slots (10) are provided in the third damping block (5), and both the third damping block (5) and the second damping block (4) are in contact with the inertial measurement device (14).