Super-strength airborne service life prolonging mechanism

Abstract

The utility model relates to the airborne technical field, in particular to a super-strength airborne service life prolonging mechanism which comprises an airborne body, first spring shock absorbers are evenly arranged at the bottom of the airborne body, sliding seats are arranged at the bottoms of the first spring shock absorbers, and a base plate is arranged below the sliding seats. Sliding grooves are formed in the positions, corresponding to the sliding seats, of the top face of the base plate, second spring shock absorbers are arranged on the inner walls of the sliding grooves, side vertical plates are arranged on the top face of the base plate in a bilateral symmetry mode, buffering pads are arranged on the inner sides of the side vertical plates, and a cooling fan is installed at the top of the airborne body. A temperature sensor is mounted on the top of the airborne body and located on the right side of the cooling fan, mounting plates are arranged on the left side and the right side of the base plate, and through holes are formed in the top faces of the mounting plates in a front-and-back symmetry mode, so that through the design, airborne internal elements can be prevented from being damaged in a damping and cooling mode; and thus, the airborne service life can be prolonged.

Description

Technical Field

[0001] This utility model relates to the field of airborne technology, specifically to an ultra-strong airborne life extension mechanism. Background Technology

[0002] Airborne equipment refers to the instruments, meters, or devices on an aircraft that can provide various types of parameters; hence, it is called aviation airborne equipment. With the continuous improvement of modern aircraft performance and the development of various technologies, the functions of aviation airborne instruments and equipment have become increasingly complex and diverse, achieving system integration and synthesis. In particular, the rapid development of information technology, network technology, and computer technology has driven and promoted the development of aircraft airborne equipment technology, continuously improving the integration, intelligence, and networking capabilities of airborne equipment.

[0003] Currently, airborne equipment shakes during use due to the movement of the vehicle, which can damage internal components. Additionally, excessive internal temperatures can also cause component damage, thus affecting the overall lifespan of the airborne equipment.

[0004] Therefore, an ultra-strong airborne life extension mechanism is needed to improve the above problems. Utility Model Content

[0005] The purpose of this invention is to provide an ultra-strong airborne life extension mechanism to solve the problems mentioned in the background art.

[0006] To achieve the above objectives, this utility model provides the following technical solution:

[0007] An ultra-strong airborne life extension mechanism includes an airborne body. First spring shock absorbers are uniformly arranged at the bottom of the airborne body. A slide is provided at the bottom of the first spring shock absorber. A base plate is provided below the slide. A sliding groove is installed on the top surface of the base plate, corresponding to the slide. A second spring shock absorber is provided on the inner wall of the sliding groove. Side plates are symmetrically arranged on the top surface of the base plate. A buffer pad is provided on the inner side of the side plates. A cooling fan is installed on the top of the airborne body. A temperature sensor is installed on the top of the airborne body, to the right of the cooling fan. Mounting plates are provided on the left and right sides of the base plate. Through holes are symmetrically opened on the front and back of the top surface of the mounting plates.

[0008] As a preferred embodiment of this utility model, the area of ​​the slide groove is larger than the area of ​​the slide block, and the connection between the slide block and the slide groove is a sliding connection.

[0009] As a preferred embodiment of this utility model, a groove is provided at the middle of the four sides of the slide corresponding to the second spring shock absorber, and the second spring shock absorber is installed in the groove.

[0010] As a preferred embodiment of this utility model, four first spring shock absorbers are provided, and the first spring shock absorbers are installed at the top corner of the slide block.

[0011] As a preferred embodiment of this utility model, the side panels and buffer pads are both designed with an L-shaped joint.

[0012] As a preferred embodiment of this utility model, the buffer pad is made of rubber material, and the buffer pad is connected to the side plate by fixed bonding.

[0013] As a preferred embodiment of this utility model, the temperature sensor and the cooling fan are connected electrically.

[0014] Compared with the prior art, the beneficial effects of this utility model are:

[0015] 1. In this utility model, the first spring shock absorber, slide block, base plate, slide groove, and second spring shock absorber dampen the airborne body from six directions (up, down, left, right, front, and back) when it shakes. This prevents damage to the internal components of the airborne body due to shaking. The cooling fan and temperature sensor dissipate the internal heat when it is too high, thus preventing damage to the internal components. In summary, the design prevents damage to the internal components of the airborne body through shock absorption and heat dissipation, thereby extending the service life of the airborne system. Attached Figure Description

[0016] Figure 1 This is a schematic diagram of the overall structure of this utility model;

[0017] Figure 2 This is a schematic diagram of part of the structure of this utility model;

[0018] Figure 3 This is a schematic diagram of the substrate structure of this utility model.

[0019] In the figure: 1. Airborne body; 2. First spring shock absorber; 3. Slide; 4. Base plate; 5. Slide groove; 6. Second spring shock absorber; 7. Side plate; 8. Buffer pad; 9. Cooling fan; 10. Temperature sensor; 11. Mounting plate; 12. Through hole. Detailed Implementation

[0020] The technical solutions of the present utility model will be clearly and completely described below with reference to the embodiments of the present utility model. Obviously, the described embodiments are only some embodiments of the present utility model, and not all embodiments. All other embodiments obtained by those skilled in the art based on the embodiments of the present utility model without creative effort are within the protection scope of the present utility model.

[0021] The technical solutions of the present utility model will be clearly and completely described below with reference to the embodiments of the present utility model. Obviously, the described embodiments are only some embodiments of the present utility model, and not all embodiments. All other embodiments obtained by those skilled in the art based on the embodiments of the present utility model without creative effort are within the protection scope of the present utility model.

[0022] To facilitate understanding of this utility model, a more comprehensive description of the utility model will be given below with reference to the accompanying drawings, and several embodiments of the utility model will be provided. However, the utility model can be implemented in many different forms and is not limited to the embodiments described herein. On the contrary, the purpose of providing these embodiments is to make the disclosure of the utility model more thorough and complete.

[0023] It should be noted that when an element is referred to as being "fixed to" another element, it can be directly on the other element or there may be an intervening element. When an element is referred to as being "connected to" another element, it can be directly connected to the other element or there may be an intervening element. The terms "vertical," "horizontal," "left," "right," and similar expressions used in this document are for illustrative purposes only.

[0024] Unless otherwise defined, all technical and scientific terms used herein have the same meaning as commonly understood by one of ordinary skill in the art to which this invention pertains. The terminology used herein is for the purpose of describing particular embodiments only and is not intended to limit the invention. The term "and / or" as used herein includes any and all combinations of one or more of the associated listed items.

[0025] For examples, please refer to Figure 1-3 This utility model provides a technical solution:

[0026] An ultra-strong airborne life extension mechanism includes an airborne body 1. First spring shock absorbers 2 are evenly arranged at the bottom of the airborne body 1. A slide block 3 is arranged at the bottom of the first spring shock absorber 2. A base plate 4 is arranged below the slide block 3. A slide groove 5 is installed on the top surface of the base plate 4 corresponding to the slide block 3. A second spring shock absorber 6 is arranged on the inner wall of the slide groove 5. Side plates 7 are symmetrically arranged on the top surface of the base plate 4. A buffer pad 8 is arranged on the inner side of the side plates 7. A cooling fan 9 is installed on the top of the airborne body 1. A temperature sensor 10 is installed on the top of the airborne body 1 and to the right of the cooling fan 9. Mounting plates 11 are arranged on the left and right sides of the base plate 4. Through holes 12 are symmetrically opened on the front and back of the top surface of the mounting plates 11.

[0027] In this embodiment, the area of ​​the slide groove 5 is larger than the area of ​​the slide block 3, and the slide block 3 and the slide groove 5 are connected by a sliding connection. Grooves are provided at the center of the four sides of the slide groove 5 corresponding to the second spring shock absorber 6, and the second spring shock absorber 6 is installed in the grooves. Four first spring shock absorbers 2 are provided, and the first spring shock absorbers 2 are installed at the top corner of the slide block 3. The side plate 7 and the buffer pad 8 both have an L-shaped design. The buffer pad 8 is made of rubber, and the connection between the buffer pad 8 and the side plate 7 is a fixed adhesive bonding. Temperature sensor 1... The connection between 0 and the cooling fan 9 is electrical. The first spring shock absorber 2, slide 3, base plate 4, slide groove 5 and the second spring shock absorber 6 dampen the airborne body 1 from six directions (up, down, left, right and front) when it shakes. This can prevent the internal components of the airborne body 1 from being damaged by shaking. The cooling fan 9 and temperature sensor 10 can expel the internal temperature of the airborne body 1 when the internal temperature is too high, thus preventing the internal components from being damaged by the excessive temperature.

[0028] The working process of this utility model is as follows: In use, the mounting plate 11 is first installed onto the carrier using bolts. When the airborne body 1 shakes, the first spring shock absorber 2 and the second spring shock absorber 6 will dampen the airborne body 1. When the internal temperature of the airborne body 1 is too high, the temperature sensor 10 will detect the high temperature information, and then the cooling fan 9 will start to dissipate the internal temperature of the airborne body 1. Through the first spring shock absorber 2, the slide 3, the base plate 4, the slide groove 5, and the second spring shock absorber 6, the airborne body 1 is damped from six directions (up, down, left, right, front, and back) when it shakes, thereby preventing damage to the internal components of the airborne body 1 due to shaking. The cooling fan 9 and the temperature sensor 10 can dissipate the internal temperature of the airborne body 1 when it is too high, thereby preventing damage to the internal components due to excessive temperature. In summary, the design can prevent damage to the internal components of the airborne body through shock absorption and heat dissipation, thereby extending the service life of the airborne body.

[0029] Although embodiments of the present invention have been shown and described, it will be understood by those skilled in the art that various changes, modifications, substitutions and alterations can be made to these embodiments without departing from the principles and spirit of the present invention, the scope of which is defined by the appended claims and their equivalents.

Claims

1. An ultra-strength airborne life extension mechanism comprising an airborne body (1) characterized by: The bottom of the airborne body (1) is uniformly provided with first spring shock absorbers (2), the bottom of the first spring shock absorbers (2) is provided with sliding seats (3), the lower portion of the sliding seats (3) is provided with base plates (4), the top surface of the base plates (4) and corresponding to the sliding seats (3) is installed with sliding grooves (5), the inner wall of the sliding grooves (5) is provided with second spring shock absorbers (6), the top surface of the base plates (4) is symmetrically provided with side vertical plates (7), the inner side of the side vertical plates (7) is provided with buffer pads (8), the top of the airborne body (1) is installed with heat dissipation fans (9), the top of the airborne body (1) and to the right of the heat dissipation fans (9) is installed with temperature sensors (10), the left and right sides of the base plates (4) are provided with mounting plates (11), the top surface of the mounting plates (11) is symmetrically provided with through holes (12).

2. A super strength on-board life extension mechanism according to claim 1, characterized in that: The area of the sliding groove (5) is greater than the area of the sliding seat (3), and the connection mode of the sliding seat (3) and the sliding groove (5) is sliding connection.

3. A super strength on-board life extension mechanism according to claim 1, wherein: The middle of the four edges of the sliding groove (5) is provided with a groove corresponding to the second spring shock absorber (6), and the second spring shock absorber (6) is installed in the groove.

4. The ultra-strength in-flight life extension mechanism of claim 1, wherein: The first spring shock absorber (2) is provided with four, and the first spring shock absorber (2) is installed at the top corner of the sliding seat (3).

5. A super strength on-board life extension mechanism according to claim 1, wherein: The shape structure of the side vertical plate (7) and the buffer pad (8) is L-shaped.

6. A super strength on-board life extension mechanism according to claim 1, wherein: The buffer pad (8) is made of rubber material, and the connection mode of the buffer pad (8) and the side vertical plate (7) is fixedly bonded.

7. A super strength on-board life extension mechanism according to claim 1, wherein: The connection mode of the temperature sensor (10) and the heat dissipation fan (9) is electrically connected.

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