Airplane buckle with waterproof function
By designing the umbrella-like structure of plug-ins and foam components in the aircraft buckle, the problem of lack of waterproofing function and connection stability in the prior art is solved, and the firm connection between the aircraft buckle and sheet metal parts is achieved and the efficient waterproofing performance of the aircraft buckle and the sheet metal parts is achieved. , meets the IPX6 waterproof standard and provides vibration buffering effect.
Patent Information
- Application Number
- CN202420868212.0
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2024-04-25
- Publication Date
- 2024-12-10
- Estimated Expiration
- 2034-04-25
AI Technical Summary
The existing aircraft buckle lacks waterproof function, and lacks connection firmness and vibration cushioning performance, making it difficult to effectively close sheet metal holes and slow down fatigue during vibration.
An aircraft buckle is designed including a plug and a connector. The plug is composed of a plug connector, an elastic baffle and a foam assembly. The plug connector is fixedly connected to the foam assembly. The foam assembly includes an EPDM foam layer and a back The adhesive layer, through the avoidance hole and plug joint set, forms an umbrella-like structure to achieve a firm connection and waterproof effect.
It realizes the firm connection between the aircraft buckle and sheet metal parts and efficient waterproof performance, meets the IPX6 waterproof standard, and reduces the fatigue caused by vibration through the vibration buffering function of the foam assembly.
Smart Images

Figure CN222146695U_ABST
Abstract
Description
Technical Field
[0001] The utility model relates to the technical field of connector connection, in particular to an aircraft buckle with waterproof function. Background Art
[0002] Connectors, also known as connectors, plugs and sockets, generally refer to electrical connectors. That is, devices that connect two active devices to transmit current or signals. They are widely used in military systems such as aviation, aerospace, and national defense.
[0003] The JST connector is a common electronic connector used to connect electronic devices and circuit boards. It has the characteristics of miniaturization, high reliability, and easy operation. The JST connector is widely used in computers, consumer electronics, automobiles, industrial equipment and other fields. It can be used to connect various devices such as LCD screens, batteries, cameras, sensors, etc. The JST connector is generally composed of a plastic shell and a connecting piece. When connected, it is directly plugged in. The connection structure is not stable enough and is easy to fall off or have poor contact. At present, most JST connectors are connected and fixed to sheet metal parts by cable ties. The connector is tied and fixed to the sheet metal part, but the cable tie fixing method makes it difficult to accurately locate the connector installation position, and the connector installation firmness is poor.
[0004] The Chinese utility model patent with the patent number of 202021977657.0 discloses an aircraft buckle for fixing the JAE connector, including an elastic plug, a baffle and a connector. The elastic plug is a plug rod with the bottom end connected to the middle of the V-shaped plug buckle. The cavity between the inner wall of the plug buckle and the plug rod constitutes an extrusion deformation cavity. The top of the plug rod is connected to the baffle. The connector is located on the other side of the baffle. The connector is provided with a slot for connecting with the JAE connector. It is only necessary to open a round hole on the fixed plate, and the elastic plug connector is pressed into it, and the JAE connector is connected to the connector. In assembling lithium-ion batteries, it is only necessary to open a round hole on the fixed plate. The operation is convenient and quick, and the JAE connector can also be disassembled. However, the aircraft buckle of the above structure cannot achieve effective closure of the sheet metal hole, does not have a waterproof function, and the connection firmness and vibration buffering function between the aircraft buckle and the sheet metal part still need to be further improved. Utility Model Content
[0005] In order to overcome the above-mentioned defects of the prior art, the inventors conducted in-depth research and completed the present utility model after paying a lot of creative work.
[0006] Specifically, the technical problem to be solved by the utility model is to provide an aircraft buckle with a waterproof function to solve the technical problem that the current aircraft buckle structure has no waterproof function.
[0007] In order to solve the above technical problems, the technical solution of the utility model is:
[0008] An aircraft buckle with waterproof function, comprising a plug-in connector and a connector connected to the plug-in connector, wherein the plug-in connector comprises a plug connector and an elastic baffle, wherein the elastic baffle is located between the plug connector and the connector, and the elastic baffle is an umbrella-like structure extending relative to the connector in a direction toward the plug connector;
[0009] Wherein, one end of the plug connector close to the elastic baffle is sleeved with a foam component, and the foam component is fixedly connected to the elastic baffle.
[0010] As an improved technical solution, the plug connector is located within the orthographic projection range of the elastic baffle and the foam component.
[0011] As an improved technical solution, the plug connector includes an integrally formed plug rod, a guide arm and a positioning support sheet, one end of the plug rod is fixedly connected to the elastic baffle, two guide arms are provided, and the two guide arms are respectively located on both sides of the other end of the plug rod, one end of the guide arm is connected to the plug rod, and the other end of the guide arm extends in a direction toward the elastic baffle and away from the plug rod, and a gradually widening V-shaped gap is formed between the guide arm and the plug rod, one end of the positioning support sheet is connected to the other end of the guide arm, and the other end of the positioning support sheet extends in a direction close to the elastic baffle, and the positioning support sheet is arranged parallel to the plug rod.
[0012] As an improved technical solution, the insertion rod is an integrally formed structure with the elastic blocking piece, and the cross section of the insertion rod is an I-shaped structure.
[0013] As an improved technical solution, the connecting piece is a structure integrally formed with the plug-in piece, and the connecting piece is provided with a slot adapted to the plastic shell of the JST connector.
[0014] As an improved technical solution, the foam component includes an EPDM foam layer and a back glue layer, the side of the EPDM foam layer close to the elastic baffle is a curved surface structure adapted to the elastic baffle, the back glue layer is located between the EPDM foam layer and the elastic baffle, and the EPDM foam layer is fixedly bonded to the elastic baffle by using the back glue layer.
[0015] As an improved technical solution, the EPDM foam layer is provided with a first avoidance hole adapted to the plug connector, the adhesive backing layer is provided with a second avoidance hole adapted to the plug connector, the second avoidance hole corresponds to the first avoidance hole, and the foam component is mounted on the plug connector through the first avoidance hole and the second avoidance hole.
[0016] As an improved technical solution, the outer periphery of the EPDM foam layer extends outside the elastic baffle.
[0017] After adopting the above technical solution, the beneficial effects of the utility model are:
[0018] When the aircraft buckle with waterproof function is used, the plug connector is pressed into the sheet metal hole of the sheet metal part to achieve the connection between the plug connector and the sheet metal part. After the plug connector is pressed into the sheet metal hole, under the action of the elastic baffle, a firm connection between the aircraft buckle and the sheet metal part can be achieved, and the connection has high tightness and stability, and the foam component is pressed against the surface of the sheet metal part. The foam component can effectively seal the sheet metal hole to achieve the purpose of waterproofing, thereby achieving good waterproof performance. The combined position of the aircraft buckle and the sheet metal part can achieve IPX6 waterproofness, and the foam component has a vibration buffering function, which can effectively relieve the fatigue generated during the vibration process and achieve vibration reduction and buffering. BRIEF DESCRIPTION OF THE DRAWINGS
[0019] In order to more clearly illustrate the specific implementation of the utility model or the technical solution in the prior art, the following is a brief introduction to the drawings required for the specific implementation or the prior art description. In all the drawings, similar elements or parts are generally identified by similar reference numerals. In the drawings, each element or part is not necessarily drawn according to the actual scale.
[0020] Figure 1 This is a schematic diagram of the structure of the aircraft buckle with waterproof function of the utility model;
[0021] Figure 2 It is a left-side structural schematic diagram of the aircraft buckle with waterproof function of the utility model;
[0022] Figure 3 It is a three-dimensional structural schematic diagram of the plug-in connector and the connecting member of the utility model;
[0023] Figure 4 Another three-dimensional structural schematic diagram of the plug connector and the connecting member of the utility model;
[0024] Figure 5 It is a cross-sectional structural schematic diagram of the plug-in connector and the connecting member of the utility model;
[0025] Figure 6 This is a schematic diagram of the explosion structure of the foam component of the utility model;
[0026] Figure 7 It is a three-dimensional structural schematic diagram of the JST connector of the utility model in the state of plastic shell insertion;
[0027] Figure 8Another three-dimensional structural schematic diagram of the JST connector of the utility model in the state of plastic shell insertion;
[0028] Reference numerals: 1-connector; 11-connector; 111-insertion rod; 112-guide arm; 113-positioning support sheet; 114-V-shaped gap; 12-elastic baffle;
[0029] 2-connector; 21-slot;
[0030] 3-foam component; 31-EPDM foam layer; 311-first avoidance hole; 32-adhesive layer; 321-second avoidance hole;
[0031] 4-JST connector plastic case. DETAILED DESCRIPTION
[0032] The following will be combined with the drawings in the embodiments of the utility model to clearly and completely describe the technical solutions in the embodiments of the utility model. Obviously, the described embodiments are only part of the embodiments of the utility model, not all of the embodiments. Based on the embodiments of the utility model, all other embodiments obtained by ordinary technicians in this field without creative work are within the scope of protection of the utility model.
[0033] It should be noted that all directional indications (such as up, down, left, right, front, back...) in the embodiments of the present invention are only used to explain the relative position relationship, movement status, etc. between the various components under a certain specific posture (as shown in the accompanying drawings). If the specific posture changes, the directional indication will also change accordingly.
[0034] At the same time, the meaning of "and / or" or "and / or" appearing in the full text includes three options. Taking "A and / or B" as an example, it includes option A, or option B, or a option in which both A and B are satisfied.
[0035] In addition, in the present utility model, descriptions such as "first", "second", etc. are only used for descriptive purposes and cannot be understood as indicating or implying their relative importance or implicitly indicating the number of the indicated technical features. Therefore, the features defined as "first" and "second" may explicitly or implicitly include at least one of the features. In addition, the technical solutions between the various embodiments can be combined with each other, but they must be based on the ability of ordinary technicians in the field to implement them. When the combination of technical solutions is contradictory or cannot be implemented, it should be deemed that such a combination of technical solutions does not exist and is not within the scope of protection required by the present utility model.
[0036] like Figures 1 to 8As shown together, the present embodiment provides an aircraft buckle with waterproof function, including a plug-in connector 1 and a connector 2 connected to the plug-in connector 1, the plug-in connector 1 includes a plug connector 11 and an elastic baffle 12, the elastic baffle 12 is located between the plug connector 11 and the connector 2, and the elastic baffle 12 is an umbrella-like structure extending relative to the connector 2 in a direction toward the plug connector 11; wherein, a foam component 3 is mounted on one end of the plug connector 11 close to the elastic baffle 12, and the foam component 3 is fixedly connected to the elastic baffle 12.
[0037] When the aircraft buckle with waterproof function is used, the plug connector 11 is pressed into the sheet metal hole of the sheet metal part to achieve the connection between the plug connector 1 and the sheet metal part. After the plug connector 11 is pressed into the sheet metal hole, under the action of the elastic baffle 12, a firm connection between the aircraft buckle and the sheet metal part can be achieved, and the connection has high tightness and stability, and the foam component 3 is pressed against the surface of the sheet metal part; the foam component 3 can effectively seal the sheet metal hole to achieve the purpose of waterproofing, and then achieve good waterproof performance. The combined position of the aircraft buckle and the sheet metal part can achieve IPX6 waterproofness, and the foam component 3 has a vibration buffering function, which can effectively relieve the fatigue generated during the vibration process and achieve vibration reduction and buffering.
[0038] like Figure 1 and Figure 2 As shown, in this embodiment, the plug connector 11 is located within the positive projection range of the elastic baffle 12 and the foam component 3. The elastic baffle 12 can realize the firm installation of the plug connector 1 on the sheet metal part, which has a good fastening and stabilizing effect, and the foam component 3 has an effective waterproof function.
[0039] like Figures 1 to 5As shown together, in this embodiment, the plug connector 11 includes an integrally formed plug rod 111, a guide arm 112 and a positioning support piece 113, one end of the plug rod 111 is fixedly connected to the elastic baffle 12, two guide arms 112 are provided, and the two guide arms 112 are respectively located on both sides of the other end of the plug rod 111, one end of the guide arm 112 is connected to the plug rod 111, and the other end of the guide arm 112 extends in a direction toward the elastic baffle 12 and away from the plug rod 111, and a gradually widening V-shaped gap 114 is formed between the guide arm 112 and the plug rod 111, one end of the positioning support piece 113 is connected to the other end of the guide arm 112, and the other end of the positioning support piece 113 extends in a direction close to the elastic baffle 12, and the positioning support piece 113 is arranged parallel to the plug rod 111. When the plug connector 11 is pressed into the sheet metal hole of the sheet metal part, the guide arm 112 will be squeezed and deformed. The guide arm 112 plays a guiding role when pressing into the sheet metal hole. After the plug connector 11 is pressed into the sheet metal hole of the sheet metal part, the guide arm 112 is reset and works together with the elastic blocking piece 12 to achieve a firm installation of the plug connector 11 and prevent it from falling out of the sheet metal hole. The positioning support piece 113 abuts against the hole wall of the sheet metal hole, which can achieve the positioning of the plug connector 11 and prevent the plug connector 11 from shaking left and right in the sheet metal hole.
[0040] like Figures 1 to 5 As shown together, in this embodiment, the insertion rod 111 is an integrally formed structure with the elastic baffle 12, has high structural strength, is convenient for integral injection molding, and has low production cost; the cross-section of the insertion rod 111 is an I-shaped structure, requires less consumables, and has high structural strength.
[0041] like Figures 1 to 5 As shown together, in this embodiment, the connector 2 is an integrally formed structure with the plug connector 1, which has high structural strength, is easy to be integrally injection molded, and has low production cost; Figure 3 , Figure 4 , Figure 7 and Figure 8 As shown in the figure, the connector 2 is provided with a slot 21 adapted to the JST connector plastic shell 4. When in use, the JST connector plastic shell 4 can be directly plugged into the connector 2. The assembly and connection operation is simple and convenient, and it is easy to realize the plug-in connection between the JST connector and the connector 2.
[0042] like Figure 1 , Figure 2 and Figure 6As shown, in this embodiment, the foam component 3 includes an EPDM foam layer 31 and a back adhesive layer 32. The side of the EPDM foam layer 31 close to the elastic baffle 12 is a curved surface structure adapted to the elastic baffle 12. The back adhesive layer 32 is located between the EPDM foam layer 31 and the elastic baffle 12, and the EPDM foam layer 31 is fixedly bonded to the elastic baffle 12 by the back adhesive layer 32. The foam component 3 provided is simple and convenient to install and connect on the plug connector 1. After the plug connector 11 of the plug connector 1 is pressed into the sheet metal hole of the sheet metal part, the EPDM foam layer 31 will be tightly attached to the surface of the sheet metal part, realizing effective sealing of the sheet metal hole and playing a good waterproof function.
[0043] like Figure 6 As shown, in this embodiment, the EPDM foam layer 31 is provided with a first avoidance hole 311 adapted to the plug connector 11, and the adhesive layer 32 is provided with a second avoidance hole 321 adapted to the plug connector 11, the second avoidance hole 321 corresponds to the first avoidance hole 311, and the foam component 3 is sleeved on the plug connector 11 through the first avoidance hole 311 and the second avoidance hole 321, and is located between the guide arm 112 and the elastic baffle 12.
[0044] like Figure 1 and Figure 2 As shown, in this embodiment, the outer periphery of the EPDM foam layer 31 extends to the outside of the elastic blocking piece 12, thereby being able to effectively seal the sheet metal hole and achieving a good waterproof effect.
[0045] By using the aircraft buckle with waterproof function of the utility model, the plug-in component 1 is first pressed into the sheet metal hole of the sheet metal part, and then the JST connector is plugged and connected with the connector 2, so that the JST connector can be firmly installed and fixed on the sheet metal part. Not only is the connection operation simple and convenient, the installation tightness and stability are good, and there is a buffer space while the installation is tight, which can effectively relieve the fatigue generated during the vibration process. In addition, the waterproof function can achieve the purpose of waterproofing and prevent water from leaking onto the JST connector.
[0046] It should be understood that the purpose of these embodiments is only to illustrate the utility model and is not intended to limit the protection scope of the utility model. In addition, it should also be understood that after reading the technical content of the utility model, those skilled in the art can make various changes, modifications and / or variations to the utility model, and all of these equivalent forms also fall within the protection scope defined by the claims attached to this application.
Claims
1. An aircraft buckle with waterproof function, comprising a plug-in connector and a connector connected to the plug-in connector, characterized in that: The plug connector includes a plug connector and an elastic baffle, wherein the elastic baffle is located between the plug connector and the connector, and the elastic baffle is an umbrella-like structure extending relative to the connector in a direction toward the plug connector; Wherein, one end of the plug connector close to the elastic baffle is sleeved with a foam component, and the foam component is fixedly connected to the elastic baffle.
2. The waterproof aircraft buckle according to claim 1, characterized in that: The plug connector is located within the orthographic projection range of the elastic blocking piece and the foam component.
3. The waterproof aircraft buckle according to claim 1, characterized in that: The plug connector includes an integrally formed plug rod, a guide arm and a positioning support sheet, one end of the plug rod is fixedly connected to the elastic baffle, two guide arms are provided, and the two guide arms are respectively located on both sides of the other end of the plug rod, one end of the guide arm is connected to the plug rod, and the other end of the guide arm extends in a direction toward the elastic baffle and away from the plug rod, and a gradually widening V-shaped gap is formed between the guide arm and the plug rod, one end of the positioning support sheet is connected to the other end of the guide arm, and the other end of the positioning support sheet extends in a direction close to the elastic baffle, and the positioning support sheet is arranged parallel to the plug rod.
4. The waterproof aircraft buckle according to claim 3, characterized in that: The insert rod is an integrally formed structure with the elastic blocking piece, and the cross section of the insert rod is an I-shaped structure.
5. The waterproof aircraft buckle according to any one of claims 1 to 4, characterized in that: The connecting piece is a structure integrally formed with the plug-in piece, and the connecting piece is provided with a slot adapted to the plastic shell of the JST connector.
6. The waterproof aircraft buckle according to any one of claims 1 to 4, characterized in that: The foam component includes an EPDM foam layer and a back adhesive layer. The side of the EPDM foam layer close to the elastic baffle is a curved surface structure adapted to the elastic baffle. The back adhesive layer is located between the EPDM foam layer and the elastic baffle, and the EPDM foam layer is fixedly bonded to the elastic baffle by the back adhesive layer.
7. The waterproof aircraft buckle according to claim 6, characterized in that: The EPDM foam layer is provided with a first avoidance hole adapted to the plug connector, the adhesive backing layer is provided with a second avoidance hole adapted to the plug connector, the second avoidance hole corresponds to the first avoidance hole, and the foam component is sleeved on the plug connector through the first avoidance hole and the second avoidance hole.
8. The waterproof aircraft buckle according to claim 6, characterized in that: The outer periphery of the EPDM foam layer extends outside the elastic blocking piece.
