CN218986955U

CN218986955U - Aviation camera triaxial stabilized platform capable of realizing multi-angle steering

Info

Publication number: CN218986955U
Application number: CN202320218902.7U
Authority: CN
Inventors: 马秋瀚
Original assignee: Changchun Changguang Ruishi Photoelectric Technology Co ltd
Current assignee: Changchun Changguang Ruishi Photoelectric Technology Co ltd
Priority date: 2023-02-15
Filing date: 2023-02-15
Publication date: 2023-05-09
Anticipated expiration: 2033-02-15

Abstract

The utility model discloses an aviation camera triaxial stabilized platform capable of realizing multi-angle steering, which relates to the technical field of triaxial stabilized platforms and comprises an aviation equipment body, wherein two groups of shock absorption seats are fixed at the bottom end of the aviation equipment body, a sliding seat is arranged between the two groups of shock absorption seats in a sliding manner, a second electric telescopic rod is arranged on the inner wall of an adjusting seat fixed at the bottom end of the sliding seat, and a guide rail seat sliding on the inner wall of the adjusting seat is fixed at one end of the second electric telescopic rod. According to the utility model, the first electric telescopic rod and the second electric telescopic rod are started, so that the ball head can rotate in the sliding table under the mutual coordination of the sliding table, the guide rail seat and the adjusting seat, the telescopic rod can be pushed and stretched, the aerial camera body fixed at the bottom end of the fixed head can be rotated, the rotating angle of the aerial camera body can be increased, the problem that the rotating angle of the traditional triaxial stabilized platform is smaller is solved, the use limitation of the aerial camera is reduced, and the effect of multi-angle adjustment rotation is realized.

Description

Aviation camera triaxial stabilized platform capable of realizing multi-angle steering

Technical Field

The utility model relates to the technical field of triaxial stabilized platforms, in particular to an aviation camera triaxial stabilized platform capable of realizing multi-angle steering.

Background

The triaxial stabilized platform, which is sometimes also called a triaxial structure or a triaxial screw, is a key device for automatically tracking and positioning a target, and has high flexibility and stability in operation, so that the triaxial stabilized platform has high-level application in the aspects of aerospace, military and the like.

In the field of aviation photography, an aviation camera needs to be installed at the end part of a triaxial stabilized platform, and when an angle of the existing triaxial stabilized platform is adjusted, the existing triaxial stabilized platform can be adjusted by one hundred eighty degrees, the adjusting angle of the existing triaxial stabilized platform is smaller, certain limitations exist, and when the existing aviation camera is used, because aviation equipment is repeatedly stopped for many times, gaps are formed between the aviation equipment and the aviation camera in a fixed mode usually, and the problem that the damping effect is poor exists easily.

Disclosure of Invention

Based on the above, the present utility model aims to provide an aerial camera triaxial stabilized platform capable of realizing multi-angle steering, so as to solve the technical problems set forth in the above background.

In order to achieve the above purpose, the present utility model provides the following technical solutions: the utility model provides an aviation camera triaxial stabilized platform that can realize multi-angle and turn to, includes the aviation equipment body, aviation equipment body bottom mounting has two sets of shock attenuation seats, two sets of it has the slide to slide between the shock attenuation seat, slide bottom mounting has and adjusts the seat inner wall and install No. two electric telescopic handle, no. two electric telescopic handle one end is fixed with and slides in the guide rail seat of adjusting the seat inner wall, guide rail seat internally mounted has an electric telescopic handle, an electric telescopic handle one end is fixed with and slides in the slip table of guide rail seat inner wall, the slip table bottom rotates there is the bulb, bulb bottom mounting has the telescopic handle, the telescopic handle other end is fixed with the fixed head, fixed head bottom mounting has the aviation camera body of being connected with adjusting the seat bottom rotation.

Preferably, the first guide slot matched with the guide rail seat is formed in the inner wall of the adjusting seat, and the second guide slot matched with the sliding table is formed in the inner wall of the aerial camera body.

Preferably, the ball groove matched with the ball head is formed in the bottom end of the sliding table, two groups of pushing rods are arranged at the two ends of the telescopic rod in a sliding mode, a limiting spring is fixed between the two groups of pushing rods and the inner wall of the telescopic rod, and a movable groove matched with the aerial camera body is formed in the bottom end of the adjusting seat.

Preferably, the end part of the sliding seat rotates to form two groups of damping rotating rods, and the other end of each damping rotating rod rotates to form a sleeve seat.

Preferably, the inner wall of the shock absorption seat is fixed with two pairs of side seats, an inner sleeve rod is fixed between the two pairs of side seats, the sleeve seat is sleeved on the outer wall of the inner sleeve rod, and an inner shock absorption spring sleeved on the outer wall of the inner sleeve rod is fixed between the sleeve seat and the side seats.

Preferably, an outer damping spring is fixed between the end part of the side seat and the sliding seat, and a damper is arranged between the sliding seat and the inner wall of the damping seat.

In summary, the utility model has the following advantages:

1. according to the utility model, the first electric telescopic rod and the second electric telescopic rod are started, so that the ball head can rotate in the sliding table under the mutual coordination of the sliding table, the guide rail seat and the adjusting seat, the telescopic rod can be pushed and stretched, the aerial camera body fixed at the bottom end of the fixed head can be rotated, the rotation angle of the aerial camera body can be increased, the problem that the rotation angle of the traditional triaxial stabilized platform is smaller is solved, the use limitation of the aerial camera is reduced, and the effect of multi-angle adjustment rotation is realized;

2. the sliding seat is extruded by the sliding seat, so that sleeve seats which are rotationally connected with the bottom ends of the two groups of damping rotating rods can be pushed to slide at the top ends of the inner sleeve rods, and the pressure generated by aviation equipment can be decomposed under the pressure decomposition action of the inner damping springs and the outer damping springs, and the damping action can be realized under the cooperation of the damper.

Drawings

FIG. 1 is a front view of an avionics body of the present utility model;

FIG. 2 is a top cross-sectional view of the adjustment seat of the present utility model;

FIG. 3 is a side cross-sectional view of the adjustment seat of the present utility model;

fig. 4 is a side cross-sectional view of the shock mount of the present utility model.

In the figure: 1. an avionics body; 2. a shock absorption seat; 3. a slide; 4. an adjusting seat; 5. an aerial camera body; 6. a guide rail seat; 7. a first electric telescopic rod; 8. a second electric telescopic rod; 9. a sliding table; 10. ball head; 11. a telescopic rod; 12. a fixed head; 13. a damping rotating rod; 14. a sleeve seat; 15. an inner loop bar; 16. a side seat; 17. an inner damping spring; 18. an outer damping spring; 19. a damper.

Detailed Description

The technical solutions in the embodiments of the present utility model will be clearly and completely described below with reference to the accompanying drawings in the embodiments of the present utility model. The embodiments described below by referring to the drawings are illustrative only and are not to be construed as limiting the utility model.

Hereinafter, an embodiment of the present utility model will be described in accordance with its entire structure.

1-4, can realize the triaxial stabilized platform of aero-camera that the multi-angle turns to, as shown in figure 1-4, including the aero-equipment body 1, the aero-equipment body 1 bottom is fixed with two sets of shock-absorbing seat 2, slide 3 has between two sets of shock-absorbing seat 2 to slide, slide 3 bottom end-fixed has adjusting seat 4 inner wall to install second electric telescopic handle 8, second electric telescopic handle 8 one end is fixed with the guide rail seat 6 that slides in adjusting seat 4 inner wall, guide rail seat 6 internally mounted has first electric telescopic handle 7, first electric telescopic handle 7 one end is fixed with the slip table 9 that slides in guide rail seat 6 inner wall, slip table 9 bottom rotates and has bulb 10, bulb 10 bottom end-fixed has telescopic handle 11, telescopic handle 11 other end is fixed with fixed head 12, fixed head 12 bottom end-fixed has the aero-camera body 5 that rotates with adjusting seat 4 bottom to be connected;

the guide way with guide rail seat 6 assorted is seted up to regulation seat 4 inner wall, aviation camera body 5 inner wall seted up with slip table 9 assorted No. two guide ways, slip table 9 bottom set up with bulb 10 assorted ball groove, telescopic link 11 both ends slip have two sets of push rods, and are fixed with spacing spring between two sets of push rods and the telescopic link 11 inner wall, regulation seat 4 bottom set up with aviation camera body 5 assorted movable groove.

When needs are adjusted aviation camera body 5 angle, the accessible starts electric telescopic handle 7, can promote slip table 9 and slide in guide rail seat 6 inside, starts No. two electric telescopic handle 8 then, can promote guide rail seat 6 and slide in adjusting seat 4 inside, adjusts slip table 9 bottom pivoted bulb 10 position, and the change of bulb 10 position this moment, stretchable and push telescopic handle 11 can drive telescopic handle 11 bottom fixed head 12 rotation, drives its bottom fixed aviation camera body 5 and rotates around adjusting seat 4 contact position department then, has reached angle regulation's effect.

Referring to fig. 1 and 4, two groups of shock absorbing rotating rods 13 are rotated at the end of the sliding seat 3, a sleeve seat 14 is rotated at the other end of the shock absorbing rotating rod 13, two pairs of side seats 16 are fixed on the inner wall of the shock absorbing seat 2, an inner sleeve rod 15 is fixed between the two groups of side seats 16, the sleeve seat 14 is sleeved on the outer wall of the inner sleeve rod 15, an inner shock absorbing spring 17 sleeved on the outer wall of the inner sleeve rod 15 is fixed between the sleeve seat 14 and the side seats 16, an outer shock absorbing spring 18 is fixed between the end of the side seat 16 and the sliding seat 3, and a damper 19 is installed between the sliding seat 3 and the inner wall of the shock absorbing seat 2.

When the aviation equipment body 1 stops, the sliding seat 3 can slide in the damping seat 2, the two groups of damping rotating rods 13 capable of pushing the end parts to rotate around the contact position with the damping seat 2 can push the two groups of sleeve seats 14 to slide on the outer wall of the inner sleeve rod 15, the two groups of inner damping springs 17 can be extruded, and meanwhile, the outer damping springs 18 between the side seats 16 and the sliding seat 3 can be extruded, and the damping effect is achieved under the cooperation of the damper 19.

When the angle of the aerial camera body 5 needs to be adjusted during use, the first electric telescopic rod 7 and the second electric telescopic rod 8 can be started to adjust the position of the ball head 10 rotating at the bottom end of the sliding table 9, and then the aerial camera body 5 fixed at the bottom end of the ball head is driven to rotate around the contact position with the adjusting seat 4, so that the effect of adjusting the angle is achieved.

Although embodiments of the utility model have been shown and described, the detailed description is to be construed as exemplary only and is not limiting of the utility model as the particular features, structures, materials, or characteristics may be combined in any suitable manner in any one or more embodiments or examples, and modifications, substitutions, variations, etc. may be made in the embodiments as desired by those skilled in the art without departing from the principles and spirit of the utility model, provided that such modifications are within the scope of the appended claims.

Claims

1. The utility model provides an aviation camera triaxial stabilized platform that can realize multi-angle and turn to, includes aviation equipment body (1), its characterized in that: the intelligent navigation device comprises an aviation device body (1), two groups of shock absorption bases (2) are fixed at the bottom end of the aviation device body, a sliding seat (3) is arranged between the two groups of shock absorption bases (2) in a sliding mode, a second electric telescopic rod (8) is arranged on the inner wall of an adjusting base (4) in a fixed mode, a guide rail base (6) sliding on the inner wall of the adjusting base (4) is fixed at one end of the second electric telescopic rod (8), an electric telescopic rod (7) is arranged in the guide rail base (6) in an internally mounted mode, a sliding table (9) sliding on the inner wall of the guide rail base (6) is fixed at one end of the first electric telescopic rod (7), a ball head (10) is arranged at the bottom end of the sliding table (9) in a rotating mode, a telescopic rod (11) is fixed at the bottom end of the ball head (10), a fixing head (12) is fixed at the other end of the telescopic rod (11), and a camera body (5) which is rotationally connected with the bottom end of the adjusting base (4).

2. The aerial camera triaxial stabilized platform capable of achieving multi-angle steering according to claim 1, characterized in that: the guide groove I matched with the guide rail seat (6) is formed in the inner wall of the adjusting seat (4), and the guide groove II matched with the sliding table (9) is formed in the inner wall of the aerial camera body (5).

3. The aerial camera triaxial stabilized platform capable of achieving multi-angle steering according to claim 1, characterized in that: the intelligent aviation camera is characterized in that a ball groove matched with the ball head (10) is formed in the bottom end of the sliding table (9), two groups of pushing rods are arranged at the two ends of the telescopic rod (11) in a sliding mode, limiting springs are fixed between the two groups of pushing rods and the inner wall of the telescopic rod (11), and a movable groove matched with the aviation camera body (5) is formed in the bottom end of the adjusting seat (4).

4. The aerial camera triaxial stabilized platform capable of achieving multi-angle steering according to claim 1, characterized in that: the end part of the sliding seat (3) rotates to form two groups of damping rotating rods (13), and the other end of each damping rotating rod (13) rotates to form a sleeve seat (14).

5. The triaxial stabilized platform for an aerial camera capable of realizing multi-angle steering according to claim 4, wherein: two pairs of side seats (16) are fixed on the inner wall of the shock absorption seat (2), an inner sleeve rod (15) is fixed between the two pairs of side seats (16), the sleeve seat (14) is sleeved on the outer wall of the inner sleeve rod (15), and an inner shock absorption spring (17) sleeved on the outer wall of the inner sleeve rod (15) is fixed between the sleeve seat (14) and the side seats (16).

6. The aerial camera triaxial stabilized platform capable of achieving multi-angle steering according to claim 5, characterized in that: an outer damping spring (18) is fixed between the end part of the side seat (16) and the sliding seat (3), and a damper (19) is arranged between the sliding seat (3) and the inner wall of the damping seat (2).