CN219393759U - Aviation connector and vacuum drying oven with same - Google Patents
Aviation connector and vacuum drying oven with same Download PDFInfo
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- CN219393759U CN219393759U CN202320621814.1U CN202320621814U CN219393759U CN 219393759 U CN219393759 U CN 219393759U CN 202320621814 U CN202320621814 U CN 202320621814U CN 219393759 U CN219393759 U CN 219393759U
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- connector
- air connector
- fixing member
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Abstract
The application discloses aviation connector and have its vacuum drying oven relates to connector technical field, and wherein aviation connector includes: the wire harness device comprises a shell, a supporting plate, a metal contact pin and a wire harness part, wherein a flange ring is arranged on the outer wall of a first end of the shell, the first end is used for being fixed at an opening of industrial equipment through the flange ring, and a second end of the shell is used for being connected with an external cable; the supporting plate is matched with the inner diameter of the shell, is arranged in the shell, and is provided with a plurality of jacks; the number of the metal pins is matched with that of the jacks, and the metal pins are correspondingly penetrated in the jacks one by one; the wire harness part is detachably connected with the second end and is used for arranging external cables. The stability of communication connection between industrial equipment and external cable can be improved to this application.
Description
Technical Field
The application relates to the technical field of connectors, in particular to an aviation connector and a vacuum drying oven with the same.
Background
The aviation connector is one of connectors, and is derived from the military industry, and along with the development of society, the aviation connector is gradually applied to the fields of automobiles, computers and peripheral equipment thereof, communication, industrial equipment and the like. Generally, aviation connector is including connecting public head and connecting female seat, among the prior art, aviation plug when connecting, need dock the public head of connection with connect female seat together, can accomplish the communication connection between industrial equipment and the outside cable, but in a lot of large-scale equipment at present, just seldom even can not break after connecting public head and connecting female seat dock, and connect public head and connect female seat and easily be bumped or pull out when connecting, and the while plug many times leads to the communication pin rupture or the break contact between the two easily, causes the poor problem of communication.
Disclosure of Invention
The present application aims to solve at least one of the technical problems existing in the prior art. Therefore, the application provides an aviation connector and a vacuum drying oven with the aviation connector, which can improve the stability of communication connection between industrial equipment and an external cable.
In a first aspect, the present application provides an aircraft connector comprising:
the outer wall of the first end of the shell is provided with a flange ring, the first end is used for being fixed at an opening of industrial equipment through the flange ring, and the second end of the shell is used for being connected with an external cable;
the supporting plate is matched with the inner diameter of the shell, is arranged in the shell and is provided with a plurality of jacks;
the number of the metal pins is matched with that of the jacks, and the metal pins are correspondingly penetrated in the jacks one by one;
and the wire harness part is detachably connected with the second end and is used for arranging external cables.
The aviation connector according to the embodiment of the first aspect of the application has at least the following beneficial effects: this application provides an aviation connector does not set up to connect public head and connect female seat, be equipped with the layer board in the casing is inside, the layer board is worn to locate by the metal contact pin, the casing can be fixed in industrial equipment's trompil department through the flange circle, industrial equipment's inside cable can directly be wired with the metal contact pin that is close to first end, outside cable can directly be wired with the metal contact pin that is close to the second end, can realize industrial equipment and outside cable's lug connection through this application provided aviation connector, need not be connected through the mode of connecting public head and connecting female seat butt joint, in order to avoid connecting public head and connect female seat and easily be bumped or pull out the problem when connecting, also avoided the plug to lead to connecting public head's communication pin rupture simultaneously many times, on the other hand, directly replace the communication current between connecting public head and the outside cable with the mode of same metal contact pin butt joint can improve industrial equipment, can also arrange outside cable through the wire portion of restrainting, make things convenient for the centralized management of outside cable. The stability of communication connection between industrial equipment and external cable can be improved.
According to some embodiments of the first aspect of the present application, the metal pin is provided with a plurality of metal pins, and the metal pins are provided with a plurality of metal pins, each metal pin is provided with a plurality of metal pins, and each metal pin is provided with a plurality of metal pins.
According to some embodiments of the first aspect of the present application, the insulating seal is a glass seal supported by a glass sintering process, the number of the glass seals is twice the number of the metal pins, and the glass seals are respectively located at two sides of each jack in the supporting plate and are combined with the corresponding metal pins.
According to some embodiments of the first aspect of the present application, both ends of the metal pin are provided with solder cups.
According to some embodiments of the first aspect of the present application, an O-shaped avoidance groove is formed in one side, which is located outside the flange ring, and the O-shaped avoidance groove is used for providing an avoidance space for industrial equipment and when the metal pins are welded.
According to some embodiments of the first aspect of the present application, the pallet and the housing are of an integrally formed structure.
According to some embodiments of the first aspect of the present application, an outer wall of the second end is provided with an external thread, and an inner cavity of the wire harness portion is provided with an internal thread matched with the external thread.
According to some embodiments of the first aspect of the present application, an outer wall of the wire harness portion is provided with anti-skid patterns.
According to some embodiments of the first aspect of the present application, the wire harness portion further includes a first arc-shaped member and a second arc-shaped member, the wire harness portion includes a small opening end and a large opening end, the large opening end is detachably connected with the second end, the small opening end is provided with a through hole for an external cable to pass through and a first fixing member and a second fixing member located on two sides of the through hole, one end of the first arc-shaped member passes through the first fixing member and one end of the second arc-shaped member through a first screw, the other end of the second arc-shaped member passes through the second fixing member and the other end of the first arc-shaped member through a second screw, and a channel for the external cable to pass through is formed between the first fixing member and the second fixing member.
In a second aspect, the present application also provides a vacuum drying oven comprising an air connector according to any one of the embodiments of the first aspect.
Additional aspects and advantages of the application will be set forth in part in the description which follows, and in part will be obvious from the description, or may be learned by practice of the application.
Drawings
Additional aspects and advantages of the present application will become apparent and readily appreciated from the following description of the embodiments, taken in conjunction with the accompanying drawings, in which:
FIG. 1 is a schematic view of an aircraft connector of the prior art;
FIG. 2 is a schematic structural view of an aircraft connector according to some embodiments of the present application;
fig. 3 is a schematic structural view of an aircraft connector from another perspective in accordance with some embodiments of the present application.
The reference numerals are as follows:
a connection male 110; a connection female socket 120; a housing 210; a flange ring 211; external threads 212; an O-shaped escape groove 213; a pallet 220; an insulating seal 221; a metal pin 230; a solder cup 231; a harness portion 240; an internal thread 241; anti-skid threads 242; a first fixing member 243; a second fixing member 244; a first arcuate member 245; a second arcuate member 246; a first screw 247; a second screw 248.
Detailed Description
Embodiments of the present application are described in detail below, examples of which are illustrated in the accompanying drawings, wherein the same or similar reference numerals refer to the same or similar elements or elements having the same or similar functions throughout. The embodiments described below by referring to the drawings are exemplary only for the purpose of explaining the present application and are not to be construed as limiting the present application.
In the description of the present application, it should be understood that references to orientation descriptions, such as directions of up, down, front, back, left, right, etc., are based on the orientation or positional relationship shown in the drawings, are merely for convenience of describing the present application and simplifying the description, and do not indicate or imply that the apparatus or element referred to must have a specific orientation, be configured and operated in a specific orientation, and thus should not be construed as limiting the present application.
In the description of the present application, the description of the first and second is only for the purpose of distinguishing technical features, and should not be construed as indicating or implying relative importance or implying the number of technical features indicated or the precedence of the technical features indicated.
In the description of the present application, unless explicitly defined otherwise, terms such as arrangement, installation, connection, etc. should be construed broadly and the specific meaning of the terms in the present application can be reasonably determined by a person skilled in the art in combination with the specific contents of the technical solution.
Referring to fig. 1, an aviation connector is one type of connector, and is derived from the military industry, and is increasingly applied to the fields of automobiles, computers and peripherals thereof, communication, industrial equipment and the like along with the development of society. Generally, the aviation connector comprises a connection male head 110 and a connection female seat 120, in the prior art, when an aviation plug is connected, the connection male head 110 and the connection female seat 120 are required to be butted together to complete communication connection between industrial equipment and an external cable, but in many large-scale equipment at present, the connection male head 110 and the connection female seat 120 are rarely or even not disconnected after being butted, and the connection male head 110 and the connection female seat 120 are easy to be bumped or pulled out when being connected, and meanwhile, the communication pins between the connection male head 110 and the connection female seat 120 are easy to break or break to cause poor communication due to repeated plugging.
Based on the technical problem, the application provides an aviation connector and a vacuum drying oven with the aviation connector, which can improve the stability of communication connection between industrial equipment and an external cable.
Referring to fig. 2 and 3, in a first aspect, the present application provides an aircraft connector comprising: the wire harness device comprises a shell 210, a supporting plate 220, a metal contact pin 230 and a wire harness part 240, wherein a flange ring 211 is arranged on the outer wall of a first end of the shell 210, the first end is used for being fixed at an opening of industrial equipment through the flange ring 211, and a second end of the shell 210 is used for being connected with an external cable; the supporting plate 220 is matched with the inner diameter of the shell 210 and is arranged inside the shell 210, and the supporting plate 220 is provided with a plurality of jacks; the number of the metal pins 230 is matched with that of the jacks, and the metal pins penetrate through the jacks in a one-to-one correspondence manner; the wire harness portion 240 is detachably connected to the second end, and the wire harness portion 240 is used for arranging external cables. The aviation connector that this application provided does not set up and connect public head 110 and connect female seat 120, be equipped with layer board 220 in the inside layer board 220 that is equipped with of casing 210, metal contact pin 230 wears to locate layer board 220, casing 210 can be fixed in industrial equipment's trompil department through flange 211, industrial equipment's inside cable can directly be wired with the metal contact pin 230 that is close to first end, outside cable can directly be wired with the metal contact pin 230 that is close to the second end, can realize the direct connection of industrial equipment and outside cable through the aviation connector that this application provided, need not be connected through the mode of connecting public head 110 and connecting female seat 120 butt joint, in order to avoid connecting public head 110 and connect female seat 120 and easily be bumped or pulled out the problem when connecting, also avoided the communication pin rupture of connecting public head 110 simultaneously to have avoided the plug many times, on the other hand, the mode that directly uses same root metal contact pin 230 replaces and connects the communication current between inside cable and the outside cable in the industrial equipment, can also arrange outside cable through wire portion 240, convenient management concentrated cable. The stability of communication connection between industrial equipment and external cable can be improved.
In the embodiment of the present application, the number of the metal pins 230 may be 12, and the number of the specific pins may be 4, 8, 10, etc., which is not limited in this application.
With continued reference to fig. 2 and 3, it can be appreciated that the aviation connector provided herein further includes at least two insulating seals 221, where the insulating seals 221 are disposed on two sides of the supporting plate 220, respectively, and are used for fixing the positions of the metal pins 230 and sealing the gaps between the metal pins 230 and the jacks. When the insulating seals 221 are provided with two insulating seals 221, each side of the supporting plate 220 is provided with one insulating seal 221, the insulating seals 221 are sleeved on the 12 metal pins 230 at the same time, the positions of the 12 metal pins 230 are fixed at the same time, gaps between each metal pin 230 and the corresponding jack are sealed, meanwhile, the number of the insulating seals 221 can be twice that of the insulating seals 221, and each insulating seal 221 is responsible for sealing the gap between one side of one metal pin 230 and the jack, which is not limited in the application.
With continued reference to fig. 2 and 3, it can be appreciated that the insulating seal 221 is a glass seal supported by a glass sintering process, the number of glass seals being twice the number of metal pins 230, the glass seals being located on either side of each receptacle in the tray 220 and being associated with a corresponding metal pin 230. The glass sealing member formed by the glass sintering process can achieve an insulating effect, and the glass can fully flow into the gap between the metal pin 230 and the jack when melting, so that a better sealing effect is achieved.
With continued reference to fig. 2 and 3, it may be understood that the two ends of the metal pin 230 are both provided with the welding cup 231, the industrial equipment and the external cable are both connected with the metal pin 230 in a welding manner, and the two ends of the metal pin 230 are both provided with the welding cup 231, so as to improve the welding effect of the cable.
Referring to fig. 2, it can be understood that an O-shaped avoidance groove 213 is formed on the outer side of the flange ring 211, and the O-shaped avoidance groove 213 is used for providing an avoidance space for welding industrial equipment with the metal pin 230, so that the welding effect between the metal pin 230 and the cable is further improved.
It can be appreciated that the support plate 220 and the housing 210 are integrally formed, which improves the overall sealing effect of the air connector provided herein.
Referring to fig. 2 and 3, it can be appreciated that the outer wall of the second end is provided with external threads 212, and the inner cavity of the wire harness portion 240 is provided with internal threads 241 that mate with the external threads 212. The wire harness portion 240 and the shell 210 are in threaded connection to achieve the detachable effect, and the wire harness portion 240 cannot damage the shell 210 in the process of installation and detachment in the threaded connection mode, so that the service life of the aviation connecting seat is prolonged. Meanwhile, the outer wall of the wire harness portion 240 is provided with the anti-slip patterns 242, so that the anti-slip performance of the wire harness portion 240 during taking can be improved.
Referring to fig. 2, it can be understood that the aviation connector provided in the present application further includes a first arc-shaped member 245 and a second arc-shaped member 246, the harness portion 240 includes a small opening end and a large opening end, the large opening end is detachably connected with the second end, the small opening end is provided with a through hole for an external cable to pass through, and a first fixing member 243 and a second fixing member 244 located at two sides of the through hole, one end of the first arc-shaped member 245 passes through one end of the first fixing member 243 and one end of the second arc-shaped member 246 through a first screw 247, the other end of the second arc-shaped member 246 passes through the second fixing member 244 and the other end of the first arc-shaped member 245 through a second screw 248, and a channel for the external cable to pass through is formed between the first arc-shaped member 245, the second arc-shaped member 246, the first fixing member 243 and the second fixing member 244. By screwing the first screw 247 and the second screw 248, the first arc-shaped member 245 and the second arc-shaped member 246 can be made to approach or separate from each other, thereby changing the size of the passage through which the external cables pass, and enabling a better arrangement of the external cables.
In a second aspect, the present application provides a vacuum drying oven comprising an air connector according to any one of the embodiments of the first aspect. In the air connector of vacuum drying oven, it does not set up and connects public head 110 and connect female seat 120, be equipped with layer board 220 in the inside of casing 210, metal contact pin 230 wears to locate layer board 220, casing 210 can be fixed in industrial equipment's trompil department through flange circle 211, industrial equipment's inside cable can directly wire with the metal contact pin 230 that is close to first end, outside cable can directly wire with the metal contact pin 230 that is close to the second end, can realize industrial equipment and outside cable's direct connection through the air connector that this application provided, need not be connected through the mode of connecting public head 110 and connecting female seat 120 butt joint, in order to avoid connecting public head 110 and connecting female seat 120 and easily be bumped or unplug the problem when being connected, also avoided the communication pin rupture of connecting public head 110 to lead to simultaneously to plug many times, on the other hand, the mode that directly uses same metal contact pin 230 replaces the mode of connecting public head 110 and connecting female seat 120 butt joint can improve the communication current between inside cable and the outside cable in the industrial equipment, can also arrange outside cable through wire portion 240, the centralized management of outside cable is convenient. The stability of communication connection between industrial equipment and external cable can be improved.
The embodiments of the present application have been described in detail above with reference to the accompanying drawings, but the present application is not limited to the above embodiments, and various changes can be made within the knowledge of one of ordinary skill in the art without departing from the spirit of the present application.
Claims (10)
1. An aircraft connector, comprising:
the outer wall of the first end of the shell is provided with a flange ring, the first end is used for being fixed at an opening of industrial equipment through the flange ring, and the second end of the shell is used for being connected with an external cable;
the supporting plate is matched with the inner diameter of the shell, is arranged in the shell and is provided with a plurality of jacks;
the number of the metal pins is matched with that of the jacks, and the metal pins are correspondingly penetrated in the jacks one by one;
and the wire harness part is detachably connected with the second end and is used for arranging external cables.
2. The air connector of claim 1, further comprising at least two insulating seals disposed on both sides of the carrier for fixing the position of the metal pins and sealing the gap between the metal pins and the sockets.
3. The air connector of claim 2, wherein the insulating seals are glass seals supported by a glass sintering process, the number of the glass seals being twice the number of the metal pins, the glass seals being respectively located on both sides of each of the receptacles in the carrier and combined with the corresponding metal pins.
4. The air connector of claim 1, wherein both ends of the metal pins are provided with solder cups.
5. The air connector of claim 1, wherein an O-shaped avoidance groove is formed in an outer side of the flange ring, and the O-shaped avoidance groove is used for providing an avoidance space for industrial equipment to weld with the metal pin.
6. The aircraft connector of claim 1, wherein the blade is of unitary construction with the housing.
7. The air connector of claim 1, wherein the outer wall of the second end is provided with external threads and the inner cavity of the harness portion is provided with internal threads that mate with the external threads.
8. The air connector of claim 1, wherein the outer wall of the harness portion is provided with anti-slip corrugations.
9. The air connector of claim 1, further comprising a first arcuate member and a second arcuate member, wherein the harness portion includes a small mouth end and a large mouth end, wherein the large mouth end is detachably connected to the second end, the small mouth end is provided with a through hole through which an external cable passes, and a first fixing member and a second fixing member located at both sides of the through hole, one end of the first arcuate member passes through the first fixing member and one end of the second arcuate member by a first screw, the other end of the second arcuate member passes through the second fixing member and the other end of the first arcuate member by a second screw, and a passage through which the external cable passes is formed between the first arcuate member, the second arcuate member, the first fixing member, and the second fixing member.
10. A vacuum drying oven comprising an air connector according to any one of claims 1 to 9.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202320621814.1U CN219393759U (en) | 2023-03-24 | 2023-03-24 | Aviation connector and vacuum drying oven with same |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202320621814.1U CN219393759U (en) | 2023-03-24 | 2023-03-24 | Aviation connector and vacuum drying oven with same |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN219393759U true CN219393759U (en) | 2023-07-21 |
Family
ID=87164566
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202320621814.1U Active CN219393759U (en) | 2023-03-24 | 2023-03-24 | Aviation connector and vacuum drying oven with same |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN219393759U (en) |
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2023
- 2023-03-24 CN CN202320621814.1U patent/CN219393759U/en active Active
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