Radar multifunctional installation device for aerospace

Abstract

The invention discloses a radar multifunctional mounting device for aerospace. The radar multifunctional mounting device comprises a mounting box, an adjusting assembly and an angle control assembly. The angle control assembly is located on the rear side of the mounting plate, the angle control assembly comprises an electric sliding table assembly and a connecting rod structure, the connecting rod structure comprises two fixing blocks, the two fixing blocks are located on the upper side of the mounting plate and the other side of the connecting plate correspondingly, and a supporting column rod is rotationally connected between the two fixing blocks; the two supporting column rods are rotationally connected, the electric sliding table assembly is located on the connecting plate, and traction rods are connected between the electric sliding table assembly and the supporting column rods. An arc-shaped flow guide groove is formed in the portion, located between the two installation grooves, of the installation box, and a limiting column is connected to the connecting plate and connected with the arc-shaped flow guide groove in a sliding mode. Compared with the prior art, the mounting plate has the advantages that the mounting plate can be conveniently adjusted, the angle of the mounting plate can be conveniently adjusted, and the receiving angle of the mounting plate can be adjusted.

Description

Technical Field

[0001] The invention relates to the field of radar installation equipment, in particular to a radar multifunctional installation device used in aerospace. Background Art

[0002] Radar is the transliteration of the English word Radar, which is derived from the abbreviation of "radio detection and ranging", that is, using radio methods to detect targets and determine their spatial positions. Therefore, radar is also called "radio positioning". Radar is an electronic device that uses electromagnetic waves to detect targets. Radar emits electromagnetic waves to illuminate the target and receives its echo, thereby obtaining information such as the distance from the target to the electromagnetic wave emission point, the distance change rate, radial velocity, azimuth, altitude, etc. Radar is also used in the aerospace field, and radar needs to be fixed by an installation device during the installation process.

[0003] When the radar is installed on the mounting device, the angle of the radar is often adjusted to make the radar more stable. After the angle adjustment, the radar is supported and fixed by a motor, which has low stability and can easily cause the radar to deviate after being subjected to external forces, reducing the stability of the radar. Summary of the invention

[0004] The technical problem to be solved by the present invention is to overcome the above technical defects and provide a mounting device which can be easily adjusted, which can not only conveniently adjust the elevation angle of the mounting plate, but also adjust the angles of the left and right devices of the mounting plate.

[0005] In order to solve the above problems, the technical solution of the present invention is: a radar multifunctional installation device for aerospace, comprising an installation box, an adjustment component and an angle control component;

[0006] Two mounting grooves are arranged on the upper side of the mounting box, the two mounting grooves are distributed on both sides of the mounting box, a through hole is arranged between the two mounting grooves, the adjustment assembly is located between the two mounting grooves, the adjustment assembly includes two pillars, the two pillars are respectively located in the mounting grooves, and the two pillars are provided with transmission wheels, a transmission belt is connected between the transmission wheels, support columns are plugged on the two transmission wheels, a gear is arranged on the support column located at the rear side, a gear 2 is meshed on the gear, a support column 2 is arranged on the gear 2, and the support column 2 is plugged with the mounting groove;

[0007] A connecting plate is inserted on the other pillar, a supporting plate is provided on the front side of the connecting plate, and a mounting plate is rotatably connected on the supporting plate;

[0008] The angle control assembly is located at the rear side of the mounting plate, and the angle control assembly includes an electric slide assembly and a connecting rod structure, and the connecting rod structure includes two fixed blocks, and the two fixed blocks are respectively located on the upper side of the mounting plate and the other side of the connecting plate, and a support rod is rotatably connected between the two fixed blocks, and the two support rods are rotatably connected, and the electric slide assembly is located on the connecting plate and a traction rod is connected between the support rods;

[0009] An arc-shaped guide groove is arranged on the installation box between the two installation grooves, and a limit column is connected to the connection plate and is slidably connected to the arc-shaped guide groove.

[0010] Furthermore, the transmission belt passes through the through hole.

[0011] Furthermore, the gear 2 is connected with an adjustment hole, and the adjustment hole is a hexagonal structure.

[0012] Furthermore, the electric slide assembly includes a groove, in which a threaded rod driven by a motor is rotatably connected, and a moving block is provided on the threaded rod driven by the motor, and the moving block is rotatably connected to the traction rod.

[0013] The advantages of the present invention compared with the prior art are:

[0014] The present invention is provided with an installation box, and an adjustment component and an angle control component are provided on the installation box. The transmission of the transmission wheel in the adjustment component drives the transmission of the transmission belt, which can drive the adjustment of the left and right angles of the installation plate, thereby increasing the convenience of installing the radar receiving plate on the installation plate. In addition, the forward and backward movement of the electric slide can cooperate with the traction rod and the connecting rod structure, so that the elevation angle of the installation plate can be adjusted, thereby increasing practicality. BRIEF DESCRIPTION OF THE DRAWINGS

[0015] Figure 1 The present invention is a three-dimensional multifunctional installation device for radar used in aviation and aerospace Figure 1 .

[0016] Figure 2 The present invention is a three-dimensional multifunctional installation device for radar used in aviation and aerospace Figure 2 .

[0017] Figure 3 The present invention is a three-dimensional multifunctional installation device for radar used in aviation and aerospace Figure 3 .

[0018] As shown in the figure: 1. Installation box; 2. Through hole; 3. Drive wheel; 4. Drive belt; 5. Support column; 6. Gear; 7. Gear 2; 8. Support column 2; 9. Adjustment hole; 10. Connecting plate; 11. Support plate; 12. Installation plate; 13. Fixed block; 14. Support rod; 15. Traction rod; 16. Arc guide groove; 17. Limit column. DETAILED DESCRIPTION

[0019] The specific implementation of the present invention is further described below in conjunction with the accompanying drawings, wherein the same components are represented by the same reference numerals.

[0020] It should be noted that the words "front", "rear", "left", "right", "up" and "down" used in the following description refer to directions in the drawings, and the words "inside" and "outside" refer to directions toward or away from the geometric center of a specific component, respectively.

[0021] In order to make the contents of the present invention more clearly understood, the technical solutions in the embodiments of the present invention will be clearly and completely described below in conjunction with the accompanying drawings in the embodiments of the present invention.

[0022] like Figures 1 to 3 As shown, a radar multifunctional installation device for aerospace includes an installation box 1, an adjustment component and an angle control component; when in use, two installation slots are provided on the upper side of the installation box 1, and the two installation slots are distributed on both sides of the installation box 1, and a through hole 2 is provided between the two installation slots, and the adjustment component is located between the two installation slots, and the rotation of the transmission wheel 3 in the adjustment component drives the rotation of the pillar thereon, and the rotation of the connecting plate 10 on the pillar can realize the left and right movement of the installation plate 12, and the adjustment component includes two pillars, the two pillars are respectively located in the installation slots, and the two pillars are provided with transmission wheels 3, and a transmission belt 4 is connected between the transmission wheels 3, and the transmission belt 4 passes through the through hole 2, and the two transmission wheels 3 are both plugged with support columns 5, and the support columns 5 located at the rear side are provided with gears 6, and the gear 6 is meshed with a gear 2 7, and the gear 2 7 is provided with a support column 2 8, and the support column 2 8 is plugged with the installation slot;

[0023] The gear 2 7 is connected with an adjustment hole 9, and the adjustment hole 9 is a hexagonal structure. A connecting plate 10 is inserted on the other pillar, and a supporting plate 11 is provided on the front side of the connecting plate 10. A mounting plate 12 is rotatably connected to the supporting plate 11;

[0024] The angle control component is located on the rear side of the mounting plate 12, and the angle control component includes an electric slide assembly and a connecting rod structure. The connecting rod structure includes two fixed blocks 13, and the two fixed blocks 13 are respectively located on the upper side of the mounting plate 12 and the other side of the connecting plate 10. A support rod 14 is rotatably connected between the two fixed blocks 13, and the two support rods 14 are rotatably connected. The electric slide assembly is located on the connecting plate 10 and a traction rod 15 is connected between the support rods 14; when in use, the moving block on the electric slide is moved back and forth by rotating the screw driven by a motor in the electric slide. In this process, the traction rod 15 will move back and forth with the moving block, thereby pulling the support rod 14 on the lower side, and the rotational connection between the two support rods 14 is used to drag and adjust the inclination angle on the mounting plate 12, thereby achieving the angle adjustment of the mounting plate 12.

[0025] An arc-shaped guide groove 16 is provided on the installation box 1 between the two installation grooves, and a limiting column 17 is connected to the connection plate 10 and is slidably connected to the arc-shaped guide groove 16 .

[0026] The electric slide assembly includes a groove, in which a threaded rod driven by a motor is rotatably connected. A moving block is provided on the threaded rod driven by the motor, and the moving block is rotatably connected to the traction rod 15.

[0027] The present invention and its embodiments are described above, and such description is not restrictive. The drawings show only one embodiment of the present invention, and the actual structure is not limited thereto. In short, if ordinary technicians in the field are inspired by it, without departing from the purpose of the invention, they can design a structure and embodiment similar to the technical solution without creativity, which should belong to the protection scope of the present invention.

Claims

1. A multifunctional installation device for radar used in aerospace, characterized in that: It comprises a mounting box (1), an adjustment component and an angle control component; The upper side of the installation box (1) is provided with two installation slots, the two installation slots are distributed on both sides of the installation box (1), a through hole (2) is provided between the two installation slots, the adjustment component is located between the two installation slots, the adjustment component comprises two pillars, the two pillars are respectively located in the installation slots, and the two pillars are provided with transmission wheels (3), a transmission belt (4) is connected between the transmission wheels (3), and support columns (5) are inserted on the two transmission wheels (3), a gear (6) is provided on the support column (5) located at the rear side, a gear (7) is meshed with a second gear (7), a support column (8) is provided on the second gear (7), and the second support column (8) is inserted in the installation slot; A connecting plate (10) is inserted and connected to the other support column, a supporting plate (11) is provided on the front side of the connecting plate (10), and a mounting plate (12) is rotatably connected to the supporting plate (11); The angle control assembly is located at the rear side of the mounting plate (12), and the angle control assembly includes an electric slide assembly and a connecting rod structure, and the connecting rod structure includes two fixed blocks (13), and the two fixed blocks (13) are respectively located on the upper side of the mounting plate (12) and the other side of the connecting plate (10), and a support rod (14) is rotatably connected between the two fixed blocks (13), and the two support rods (14) are rotatably connected to each other, and the electric slide assembly is located on the connecting plate (10) and a traction rod (15) is connected between the support rod (14); An arc-shaped guide groove (16) is provided on the installation box (1) between the two installation grooves, and a limit column (17) is connected to the connection plate (10) and is slidably connected to the arc-shaped guide groove (16).

2. The radar multifunctional mounting device for aerospace according to claim 1, characterized in that: The transmission belt (4) passes through the through hole (2).

3. The radar multifunctional mounting device for aviation and aerospace according to claim 1, characterized in that: The gear 2 (7) is connected with an adjustment hole (9), and the adjustment hole (9) is a hexagonal structure.

4. The radar multifunctional mounting device for aviation and aerospace according to claim 1, characterized in that: The electric slide assembly comprises a groove, in which a threaded rod driven by a motor is rotatably connected, and a moving block is provided on the threaded rod driven by the motor, and the moving block is rotatably connected to a traction rod (15).

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