Photoelectric pod damping device
By combining a connecting plate, mounting plate, shock-absorbing ball, and connecting spring, the synchronous vibration problem of the optoelectronic pod in aircraft vibration is solved, achieving image stability and vibration reduction effect of the optoelectronic pod, reducing the risk of detachment, and extending the service life of the shock-absorbing ball.
Patent Information
- Application Number
- CN202423218827.8
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2024-12-25
- Publication Date
- 2025-11-04
- Estimated Expiration
- 2034-12-25
AI Technical Summary
The existing electro-optical pod racks lack vibration damping structures, causing the electro-optical pods to vibrate synchronously when the aircraft vibrates, affecting mission execution.
The system employs a combination structure of connecting plates, mounting plates, shock-absorbing balls, and connecting springs. The shock-absorbing balls connect the mounting ears to the mounting plates, and the system also incorporates a limit plate and padding design to reduce the impact of aircraft vibrations on the electro-optical pod.
It effectively reduces the impact of aircraft vibration on the optoelectronic pod, improves image stability, reduces the risk of shock-absorbing balls falling off, extends service life, and reduces maintenance frequency.
Smart Images

Figure CN223508486U_ABST
Abstract
Description
Technical Field
[0001] This utility model relates to the field of optoelectronic pod technology, and in particular to an optoelectronic pod vibration damping device. Background Technology
[0002] Aircraft equipped with electro-optical pods can perform a variety of missions, including reconnaissance, surveillance, search and rescue, identification, tracking, and navigation. Existing electro-optical pod mounting structures are primarily bolt-fixed, lacking vibration damping. During flight, aircraft vibrations can cause synchronized vibrations in the electro-optical pods, impacting mission performance. Utility Model Content
[0003] The purpose of this invention is to provide a vibration damping device for an optoelectronic pod, which reduces the impact of aircraft vibration on the optoelectronic pod and improves the image stability of the optoelectronic pod.
[0004] The objective of this utility model is achieved through the following technical solution:
[0005] A shock-absorbing device for an optoelectronic pod includes a connecting plate. The lower end of the connecting plate has a circular bracket adapted to the optoelectronic pod. The inner wall of the circular bracket has a mounting plate. The upper outer edge of the optoelectronic pod has multiple mounting ears. The mounting plate has through-holes adapted to the mounting ears. A mounting hole is provided on one side of the through-hole on the mounting plate. A shock-absorbing ball is provided between the mounting ears and the mounting hole. The lower end of the connecting plate has multiple connecting springs, and the lower ends of the multiple connecting springs have limiting plates adapted to the optoelectronic pod.
[0006] Furthermore, the lower end of the limiting plate is provided with a soft pad, and the soft pad has a gap with the upper end of the photoelectric pod.
[0007] Furthermore, both the connecting plate and the limiting plate have cable through holes at their centers, the soft pads include two, and the two soft pads are respectively disposed on both sides of the cable through hole, and the multiple connecting springs are evenly distributed on the outside of the cable through hole.
[0008] Furthermore, the sidewall of the circular bracket is symmetrically provided with multiple rectangular holes, and a lifting groove is formed between the two soft pads. The width of the rectangular holes is greater than the width of the lifting groove, and the radial direction of the lifting groove is consistent with the direction of the line connecting any two symmetrical rectangular holes.
[0009] Furthermore, the lower end face of the limiting plate is provided with lifting inclined surfaces at both ends of the lifting groove.
[0010] This utility model has the following advantages:
[0011] 1. The mounting ears and mounting plate are connected by multiple shock-absorbing balls, which can effectively reduce the impact of aircraft vibration on the electro-optical pod and improve the image stability of the electro-optical pod.
[0012] 2. The shock-absorbing balls are located above the mounting plate, which puts the shock-absorbing balls in a downward state, reducing the risk of falling off due to severe vibration and ensuring good stability.
[0013] 3. The shock-absorbing ball is placed inside the circular bracket, which protects the shock-absorbing ball, extends its service life, and reduces the frequency of maintenance and replacement. Attached Figure Description
[0014] Figure 1 This is a schematic diagram of the structure of this utility model.
[0015] Figure 2 This is a top view of the mounting plate structure.
[0016] Figure 3 This is a bottom view of the limiting plate.
[0017] In the diagram, 1-connecting plate, 2-photoelectric pod, 3-circular bracket, 4-mounting plate, 5-mounting ear, 6-through notch, 7-mounting hole, 8-shock absorber ball, 9-connecting spring, 10-limiting plate, 11-soft pad, 12-cable hole, 13-rectangular hole, 14-lifting groove, 15-lifting ramp. Detailed Implementation
[0018] To make the objectives, technical solutions, and advantages of the embodiments of this utility model clearer, the technical solutions of the embodiments of this utility model will be clearly and completely described below with reference to the accompanying drawings. Obviously, the described embodiments are only some embodiments of this utility model, not all embodiments. The components of the embodiments of this utility model described and shown in the accompanying drawings can typically be arranged and designed in various different configurations.
[0019] Therefore, the following detailed description of the embodiments of the present invention provided in the accompanying drawings is not intended to limit the scope of the claimed invention, but merely to illustrate selected embodiments of the invention. All other embodiments obtained by those skilled in the art based on the embodiments of the present invention without inventive effort are within the scope of protection of the present invention.
[0020] It should be noted that, where there is no conflict, the embodiments and features in the embodiments of this utility model can be combined with each other.
[0021] It should be noted that similar labels and letters in the following figures indicate similar items. Therefore, once an item is defined in one figure, it does not need to be further defined and explained in subsequent figures.
[0022] In the description of this utility model, it should be noted that the terms "center," "upper," "lower," "left," "right," "vertical," "horizontal," "inner," and "outer," etc., indicate the orientation or positional relationship based on the orientation or positional relationship shown in the accompanying drawings, or the orientation or positional relationship commonly used when the product of this utility model is in use, or the orientation or positional relationship commonly understood by those skilled in the art. They are only used for the convenience of describing this utility model and simplifying the description, and do not indicate or imply that the device or element referred to must have a specific orientation, or be constructed and operated in a specific orientation. Therefore, they should not be construed as limitations on this utility model. In addition, the terms "first," "second," etc., are only used to distinguish descriptions and should not be construed as indicating or implying relative importance.
[0023] In the description of this utility model, it should also be noted that, unless otherwise explicitly specified and limited, the terms "set," "install," "connect," and "link" should be interpreted broadly. For example, they can refer to a fixed connection, a detachable connection, or an integral connection; they can refer to a mechanical connection or an electrical connection; they can refer to a direct connection or an indirect connection through an intermediate medium; and they can refer to the internal connection of two components. Those skilled in the art can understand the specific meaning of the above terms in this utility model based on the specific circumstances.
[0024] refer to Figure 1-3 As shown, one embodiment of this utility model is as follows:
[0025] A shock-absorbing device for a photoelectric pod includes a connecting plate 1. The lower end of the connecting plate 1 is provided with a circular bracket 3 adapted to a photoelectric pod 2. The inner wall of the circular bracket 3 is provided with a mounting plate 4. The upper outer edge of the photoelectric pod 2 is provided with multiple mounting ears 5. The mounting plate 4 is provided with a through-hole 6 adapted to the mounting ears 5. The mounting plate 4 is provided with a mounting hole 7 on one side of the through-hole 6. A shock-absorbing ball 8 is provided between the mounting ears 5 and the mounting hole 7. The lower end of the connecting plate 1 is provided with multiple connecting springs 9. The lower end of the multiple connecting springs 9 is provided with a limiting plate 10 adapted to the photoelectric pod 2.
[0026] Specifically, the connecting plate 1 can be fixed to the fuselage skin by rivets; the lower end of the limiting plate 10 is provided with a soft pad 11, and the soft pad 11 has a gap with the upper end of the photoelectric pod 2.
[0027] During installation, the upper end of the shock-absorbing ball 8 is pre-fitted into the mounting hole on the mounting ear 5. Then, the photoelectric pod 2 is operated so that the mounting ear 5 passes through the through-notch 6 and is positioned above the mounting plate 4. After rotation and adjustment, it is positioned above the mounting hole on the mounting plate 4. Then, the lower end of the shock-absorbing ball 8 is fitted into the mounting hole 7 on the mounting plate 4 to realize the installation of the photoelectric pod.
[0028] The mounting lug 5 and the mounting plate 4 are connected by multiple shock-absorbing balls 8, which can effectively reduce the impact of aircraft vibration on the electro-optical pod and improve the image stability of the electro-optical pod. Furthermore, the shock-absorbing balls 8 are placed inside the circular mounting bracket 3, which protects them. A through-hole 6 is provided to position the shock-absorbing balls 8 above the mounting plate 4, keeping them in a downward-pressed state, reducing the risk of them falling off due to severe vibration and ensuring good stability. Simultaneously, this embodiment also uses a connecting spring 9 and a limiting plate 10 to restrict the upward movement of the electro-optical pod 2, further improving stability.
[0029] Furthermore, both the connecting plate 1 and the limiting plate 10 are provided with cable through holes 12 at their centers. The soft pads 11 include two, and the two soft pads 11 are respectively disposed on both sides of the cable through holes 12. The multiple connecting springs 9 are evenly distributed on the outside of the cable through holes 12.
[0030] The circular bracket 3 has a plurality of rectangular holes 13 symmetrically arranged on its side wall. A lifting groove 14 is formed between the two soft pads 11. The width of the rectangular hole 13 is greater than the width of the lifting groove 14. The radial direction of the lifting groove 14 is consistent with the direction of the line connecting any two symmetrical rectangular holes 13.
[0031] The lower end face of the limiting plate 10 is provided with lifting inclined surfaces 15 at both ends of the lifting groove 14.
[0032] While ensuring sufficient space for the upward movement of the photoelectric pod 2, the limiting plate should also facilitate disassembly and assembly operations. Therefore, this application implements the installation of the limiting plate by setting a connecting spring 9. The rectangular hole 13 effectively reduces the weight of the equipment while also facilitating the lifting of the limiting plate 10. Specifically, in implementation, two wedge-shaped blocks can be inserted through the rectangular hole 13 to support the limiting plate 10 and lift it upward, thereby expanding the upward movement space of the photoelectric pod 2 and facilitating disassembly and assembly operations. Specifically, the lower end of the rectangular hole 13 can be slightly higher than the position of the limiting plate 10 in the natural extension and retraction state of the connecting spring 9, so as to achieve a larger movement space when the photoelectric pod 2 moves upward. Therefore, this embodiment provides a lifting ramp 15 on the lower end surface of the limiting plate 10 so that the wedge-shaped blocks can more easily enter the lifting groove 14. In specific operation, care should be taken to avoid damage to the cables by the wedge-shaped blocks, which can be protected by attaching a soft pad to the front end of the wedge-shaped blocks.
[0033] Although the present invention has been described in detail with reference to the foregoing embodiments, those skilled in the art can still modify the technical solutions described in the foregoing embodiments or make equivalent substitutions for some of the technical features. Any modifications, equivalent substitutions, improvements, etc., made within the spirit and principles of the present invention should be included within the protection scope of the present invention.
Claims
1. A photoelectric pod vibration damping device, characterized in that: The device includes a connecting plate, a circular bracket adapted to the photovoltaic pod at its lower end, a mounting plate on the inner wall of the circular bracket, multiple mounting ears on the upper outer edge of the photovoltaic pod, a through-hole adapted to the mounting ears on the mounting plate, a mounting hole on one side of the through-hole on the mounting plate, a shock-absorbing ball between the mounting ear and the mounting hole, and multiple connecting springs at the lower end of the connecting plate, with a limiting plate adapted to the photovoltaic pod at the lower end of the multiple connecting springs.
2. The photoelectric pod vibration damping device according to claim 1, characterized in that: The lower end of the limiting plate is provided with a soft pad, and the soft pad has a gap with the upper end of the photoelectric pod.
3. The photoelectric pod vibration damping device according to claim 2, characterized in that: Both the connecting plate and the limiting plate have cable through holes at their centers. The soft pads include two pads, which are respectively disposed on both sides of the cable through holes. The multiple connecting springs are evenly distributed on the outside of the cable through holes.
4. The photoelectric pod vibration damping device according to claim 3, characterized in that: The circular bracket has multiple rectangular holes symmetrically arranged on its side wall. A lifting groove is formed between two of the soft pads. The width of the rectangular hole is greater than the width of the lifting groove. The radial direction of the lifting groove is consistent with the direction of the line connecting any two symmetrical rectangular holes.
5. The photoelectric pod vibration damping device according to claim 4, characterized in that: The lower end face of the limiting plate is provided with lifting inclined surfaces at both ends of the lifting groove.