CN216660362U - Airborne communication equipment shock attenuation frame - Google Patents
Airborne communication equipment shock attenuation frame Download PDFInfo
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- CN216660362U CN216660362U CN202122050140.8U CN202122050140U CN216660362U CN 216660362 U CN216660362 U CN 216660362U CN 202122050140 U CN202122050140 U CN 202122050140U CN 216660362 U CN216660362 U CN 216660362U
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Abstract
The utility model discloses a shock absorption rack for airborne communication equipment, and particularly relates to the technical field of communication equipment. According to the utility model, the damping box is arranged in the outer box body for fixing equipment, and the damping rod and the second spring are arranged in the longitudinal direction and the transverse direction of the damping box, so that the vibration in different directions in the flight process is relieved by the elasticity of the second spring, and the influence of the vibration on the damping box and the satellite communication equipment inside the damping box is relieved.
Description
Technical Field
The embodiment of the utility model relates to the technical field of communication equipment, in particular to a damping rack for airborne communication equipment.
Background
Satellite communication technology is a technical means for communication between two or more earth stations by using artificial earth satellites as relay stations to transmit radio waves, and is widely used in our lives, and nowadays, the development of the network era and the increasingly mature satellite communication technology are in an inseparable relationship, and the satellite communication technology can be used even on airplanes in ten thousand meters high altitude.
With the development of the airborne satellite communication technology, aviation passengers gradually get rid of the long and boring days in the flight process and isolated from the world, but the airplane can vibrate due to the influence of factors such as air flow and the like in the flight process, the airborne satellite communication equipment is influenced, the simple damping device can only relieve the vibration in a single direction, the vibration in different directions in the flight process cannot be effectively relieved, and the damping effect is poor.
SUMMERY OF THE UTILITY MODEL
Therefore, the embodiment of the utility model provides a damping rack for airborne communication equipment, wherein a damping box is arranged in an outer box body to fix the equipment, and a damping rod and a second spring are arranged in the longitudinal direction and the transverse direction of the damping box, so that the vibration in different directions in the flight process is relieved by the elasticity of the second spring, the influence of the vibration on the damping box and the satellite communication equipment inside the damping box is relieved, and the problem that the damping effect is poor because the damping device in the prior art can only relieve the vibration in a single direction is solved.
In order to achieve the above object, the embodiments of the present invention provide the following technical solutions: a shock absorption rack for airborne communication equipment comprises an outer box body, wherein a shock absorption mechanism is arranged inside the outer box body;
damper includes the surge tank, the surge tank is established at outer internal portion, surge tank both sides and top and bottom are all fixed and are equipped with the shock attenuation pole, the surge tank rear side is equipped with first spring, first spring one end and outer internal wall fixed connection of casing, the internal portion of outer container is equipped with the slide bar, slide bar outer end cover is equipped with a plurality of sliding seat, the outer end of sliding seat is all fixed and is equipped with the shock attenuation outer tube, the shock attenuation pole is established and is extended to the shock attenuation outer tube inside shock attenuation outer tube one side and one end, inside second spring and the second spring one end and the shock attenuation pole one end fixed connection of being equipped with of shock attenuation outer tube, the second spring other end and sliding seat outer end fixed connection.
Furthermore, the front ends of the outer box body and the shock absorption box are respectively provided with a box body door and a shock absorption box door, and the box body door and the shock absorption box door are respectively movably connected with the outer box body and the shock absorption box through hinges.
Furthermore, soundproof cotton is fixedly arranged on the inner wall of the outer box body and the inner side of the box body door.
Further, an electric push rod is arranged inside the shock absorption box, one end of the electric push rod is fixedly connected with the top end inside the shock absorption box, a pressing plate is fixedly arranged at the other end of the electric push rod, a first rubber pad is arranged at the bottom end of the pressing plate, a fixing seat is arranged at the bottom of the pressing plate, the fixing seat is fixedly arranged at the bottom end inside the shock absorption box, and a second rubber pad is arranged at the top end of the fixing seat.
Furthermore, a hanging buckle is fixedly arranged on the rear side of the damping box, a connecting ring is fixedly arranged at the other end of the first spring, and the first spring is connected with the damping box through the hanging buckle and the connecting ring.
Furthermore, a plurality of fixing columns are arranged at the outer ends of the sliding rods, and the fixing columns are fixedly connected with the outer box body.
Furthermore, the front and the back of the outer box body and the two sides of the outer box body are fixedly provided with mounting plates, and a plurality of fixing holes are formed in the mounting plates.
The embodiment of the utility model has the following advantages:
according to the utility model, the damping box is arranged in the outer box body to fix equipment, and the damping rod and the second spring are arranged in the longitudinal direction and the transverse direction of the damping box, so that the vibration in different directions in the flight process is relieved by the elasticity of the second spring, the influence of the vibration on the damping box and the satellite communication equipment inside the damping box is relieved, and compared with the prior art, the vibration in different directions can be relieved.
Drawings
In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings used in the description of the embodiments or the prior art will be briefly described below. It should be apparent that the drawings in the following description are merely exemplary, and that other embodiments can be derived from the drawings provided by those of ordinary skill in the art without inventive effort.
The structures, ratios, sizes, and the like shown in the present specification are only used for matching with the contents disclosed in the specification, so as to be understood and read by those skilled in the art, and are not used to limit the conditions that the present invention can be implemented, so that the present invention has no technical significance, and any structural modifications, changes in the ratio relationship, or adjustments of the sizes, without affecting the effects and the achievable by the present invention, should still fall within the range that the technical contents disclosed in the present invention can cover.
FIG. 1 is a schematic view of the overall structure provided by the present invention;
FIG. 2 is a right side cross-sectional view provided by the present invention;
FIG. 3 is a cross-sectional view of a shock absorbing outer tube provided by the present invention;
FIG. 4 is a perspective view of the fixing base and the second rubber pad provided by the present invention;
FIG. 5 is a perspective view of a mounting plate provided by the present invention;
in the figure: the damping device comprises an outer box body 1, a soundproof cotton 2, a sliding seat 3, a sliding rod 4, a damping box 5, a fixed column 6, a damping outer tube 7, an electric push rod 8, a pressing plate 9, a first rubber pad 10, a second rubber pad 11, a fixed seat 12, a mounting plate 13, a box body door 14, a damping box door 15, a hanging buckle 16, a connecting ring 17, a first spring 18, a damping rod 19 and a second spring 20.
Detailed Description
The present invention is described in terms of particular embodiments, other advantages and features of the utility model will become apparent to those skilled in the art from the following disclosure, and it is to be understood that the described embodiments are merely exemplary of the utility model and that it is not intended to limit the utility model to the particular embodiments disclosed. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.
Referring to the attached fig. 1-5 of the specification, the damping frame for the airborne communication equipment of the embodiment comprises an outer box 1, wherein a damping mechanism is arranged inside the outer box 1;
Damper includes damper 5, damper 5 is established inside outer box 1, damper 5 both sides and top and bottom are all fixed and are equipped with shock attenuation pole 19, damper 5 rear side is equipped with first spring 18, first spring 18 one end and 1 inner wall fixed connection of outer box, 1 inside slide bar 4 that is equipped with of outer box, 4 outer pot heads of slide bar are equipped with a plurality of sliding seat 3, 3 outer ends of sliding seat are all fixed and are equipped with shock attenuation outer tube 7, shock attenuation pole 19 is established and is extended to shock attenuation outer tube 7 inside 7 in 7 one side of shock attenuation outer tube and one end, 7 inside second spring 20 and the inside second spring 20 one end and the 19 one end fixed connection of shock attenuation pole that are equipped with of shock attenuation outer tube, the second spring 20 other end and 3 outer end fixed connection of sliding seat.
Furthermore, the front ends of the outer box body 1 and the damper box 5 are respectively provided with a box body door 14 and a damper box door 15, and the box body door 14 and the damper box door 15 are respectively movably connected with the outer box body 1 and the damper box 5 through hinges, so that the communication equipment can be conveniently installed.
Furthermore, soundproof cotton 2 is fixedly arranged on the inner wall of the outer box body 1 and the inner side of the box body door 14, so that the effect of isolating noise is achieved.
Furthermore, an electric push rod 8 is arranged inside the shock absorption box 5, one end of the electric push rod 8 is fixedly connected with the top end inside the shock absorption box 5, a pressing plate 9 is fixedly arranged at the other end of the electric push rod 8, a first rubber pad 10 is arranged at the bottom end of the pressing plate 9, a fixed seat 12 is arranged at the bottom of the pressing plate 9, the fixed seat 12 is fixedly arranged at the bottom end inside the shock absorption box 5, and a second rubber pad 11 is arranged at the top end of the fixed seat 12 and used for fixing satellite communication equipment.
Furthermore, a hanging buckle 16 is fixedly arranged on the rear side of the damper box 5, a connecting ring 17 is fixedly arranged at the other end of the first spring 18, and the first spring 18 is connected with the damper box 5 through the hanging buckle 16 and the connecting ring 17, so that the damper box 5 is connected with the outer box body 1.
Furthermore, a plurality of fixing columns 6 are arranged at the outer ends of the sliding rods 4, the fixing columns 6 are fixedly connected with the outer box body 1, the sliding rods 4 are fixedly connected with the outer box body 1 through the fixing columns 6, and the sliding rods 4 are convenient to fix.
Further, the front and the back of the outer box body 1 and both sides of the outer box body are fixedly provided with mounting plates 13, and the mounting plates 13 are provided with a plurality of fixing holes for fixing the outer box body 1.
The implementation scenario is specifically as follows: the box body door 14 and the damper box door 15 are opened in sequence, airborne satellite communication equipment is placed on the surface of the second rubber pad 11 in the damper box 5, the electric push rod 8 is started, the electric push rod 8 drives the pressing plate 9 and the first rubber pad 10 to move downwards, the first rubber pad 10 is in contact with the top end of the communication equipment, the equipment is pressed and fixed through the downward force of the electric push rod 8, then the damper box door 15 and the box body door 14 are closed, in the flying process, when left transverse vibration is generated, the damper box 5 can move left and right, so that the transverse damper rods 19 move, one damper rod 19 compresses the second spring 20 connected with the damper rod 19, the damper rod 19 on the other side stretches the second spring 20 connected with the damper rod, the transversely generated vibration can be buffered through the elastic force of the second spring 20, so as to reduce the influence of the vibration on the damper box 5 and the internal communication equipment, and at the same time, in the case of transverse vibration, the longitudinal damping rod 19 does not work, but the longitudinal sliding seat 3 slightly slides on the surface of the sliding rod 4 along with the transverse movement, and does not affect the transverse damping, and similarly, in the case of longitudinal vibration, the longitudinal damping rod 19 and the second spring 20 work to achieve the purpose of damping, the transverse sliding seat 3 slides on the surface of the sliding rod 4, and does not affect the transverse damping, so as to achieve the aim of relieving the vibration from different directions in the flying process, the damping box 5 is arranged in the outer box body 1 for fixing equipment, meanwhile, the damping rods 19 and the second springs 20 are arranged in the longitudinal direction and the transverse direction of the damping box 5, the vibration in different directions in the flight process is relieved through the elasticity of the second springs 20, the influence of the vibration on the damping box 5 and the satellite communication equipment inside the damping box is relieved, this embodiment has specifically solved among the prior art damping device often can only alleviate the vibrations of single direction and make the not good problem of shock attenuation effect.
The working principle is as follows:
referring to the attached drawings 1-5 of the specification, a box body door 14 and a damper box door 15 are opened in sequence, airborne satellite communication equipment is placed on the surface of a second rubber pad 11 in the damper box 5, an electric push rod 8 is started, the electric push rod 8 drives a pressing plate 9 and the first rubber pad 10 to move downwards, the first rubber pad 10 is in contact with the top end of the communication equipment, the equipment is pressed and fixed through the downward force of the electric push rod 8, then the damper box door 15 and the box body door 14 are closed, in the flight process, when left transverse vibration is generated, the damper box 5 can move left and right, transverse damper rods 19 move, one damper rod 19 compresses a second spring 20 connected with the damper rod 19, the damper rod 19 on the other side stretches the second spring 20 connected with the damper box door, the transverse generated vibration is buffered through the elastic force of the second spring 20, so that the influence of the vibration on the damper box 5 and the communication equipment inside the damper box is reduced, meanwhile, during transverse vibration, the longitudinal damping rod 19 does not work, but the longitudinal sliding seat 3 slightly slides on the surface of the sliding rod 4 along with the transverse movement and does not influence the transverse damping, and similarly, during the longitudinal vibration, the longitudinal damping rod 19 and the second spring 20 work to achieve the purpose of damping, and the transverse sliding seat 3 slides on the surface of the sliding rod 4 and does not influence the transverse damping, so that the purpose of relieving the vibration from different directions in the flight process is achieved.
Although the utility model has been described in detail above with reference to a general description and specific examples, it will be apparent to one skilled in the art that modifications or improvements may be made thereto based on the utility model. Accordingly, such modifications and improvements are intended to be within the scope of the utility model as claimed.
Claims (7)
1. The utility model provides an airborne communication equipment shock attenuation frame, includes outer box (1), its characterized in that: a damping mechanism is arranged inside the outer box body (1);
the damping mechanism comprises a damping box (5), the damping box (5) is arranged in the outer box body (1), shock absorption rods (19) are fixedly arranged on the two sides, the top end and the bottom end of the shock absorption box (5), a first spring (18) is arranged at the rear side of the damping box (5), one end of the first spring (18) is fixedly connected with the inner wall of the outer box body (1), a slide bar (4) is arranged in the outer box body (1), a plurality of slide seats (3) are sleeved at the outer end of the slide bar (4), the outer ends of the sliding seats (3) are respectively fixedly provided with a damping outer tube (7), the damping rods (19) are arranged on one side of the damping outer tube (7) and one end of each damping rod extends into the damping outer tube (7), a second spring (20) is arranged in the damping outer tube (7), one end of the second spring (20) is fixedly connected with one end of a damping rod (19), the other end of the second spring (20) is fixedly connected with the outer end of the sliding seat (3).
2. The airborne communication equipment shock mount of claim 1, wherein: the shock absorption box is characterized in that the front ends of the outer box body (1) and the shock absorption box (5) are respectively provided with a box body door (14) and a shock absorption box door (15), and the box body door (14) and the shock absorption box door (15) are respectively movably connected with the outer box body (1) and the shock absorption box (5) through hinges.
3. The airborne communication equipment shock mount of claim 2, wherein: soundproof cotton (2) is fixedly arranged on the inner wall of the outer box body (1) and the inner side of the box body door (14).
4. The airborne communication equipment shock mount of claim 1, wherein: the damping box is characterized in that an electric push rod (8) is arranged inside the damping box (5), one end of the electric push rod (8) is fixedly connected with the top end inside the damping box (5), a pressing plate (9) is fixedly arranged at the other end of the electric push rod (8), a first rubber pad (10) is arranged at the bottom end of the pressing plate (9), a fixing seat (12) is arranged at the bottom of the pressing plate (9), the fixing seat (12) is fixedly arranged at the bottom end inside the damping box (5), and a second rubber pad (11) is arranged at the top end of the fixing seat (12).
5. The airborne communication equipment shock mount of claim 1, wherein: the shock absorption box is characterized in that a hanging buckle (16) is fixedly arranged on the rear side of the shock absorption box (5), a connecting ring (17) is fixedly arranged at the other end of the first spring (18), and the first spring (18) is connected with the shock absorption box (5) through the hanging buckle (16) and the connecting ring (17).
6. The airborne communication equipment shock mount of claim 1, wherein: the outer end of the sliding rod (4) is provided with a plurality of fixing columns (6), the fixing columns (6) are fixedly connected with the outer box body (1), and the sliding rod (4) is fixedly connected with the outer box body (1) through the fixing columns (6).
7. The airborne communication equipment shock mount of claim 1, wherein: the outer box body (1) is provided with mounting plates (13) at the front and the back and on the two sides, and the mounting plates (13) are provided with a plurality of fixing holes.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202122050140.8U CN216660362U (en) | 2021-08-29 | 2021-08-29 | Airborne communication equipment shock attenuation frame |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202122050140.8U CN216660362U (en) | 2021-08-29 | 2021-08-29 | Airborne communication equipment shock attenuation frame |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN216660362U true CN216660362U (en) | 2022-06-03 |
Family
ID=81758910
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202122050140.8U Active CN216660362U (en) | 2021-08-29 | 2021-08-29 | Airborne communication equipment shock attenuation frame |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN216660362U (en) |
-
2021
- 2021-08-29 CN CN202122050140.8U patent/CN216660362U/en active Active
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CB03 | Change of inventor or designer information |
Inventor after: Zhang Yusong Inventor after: Yang Jinhui Inventor after: Liu Yuanyuan Inventor after: Wu Qiaoling Inventor before: Wu Qiaoling |
|
| CB03 | Change of inventor or designer information | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20230820 Address after: 443000 No.1, Xiba Jianshe Road, Xiling District, Yichang City, Hubei Province Patentee after: Zhang Yusong Address before: 510000 Room 401, No. 13, Longdong Chuangyi street, Tianhe District, Guangzhou City, Guangdong Province Patentee before: Wu Qiaoling |
|
| TR01 | Transfer of patent right |