CN217589587U - Electric connector for aircraft - Google Patents
Electric connector for aircraft Download PDFInfo
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- CN217589587U CN217589587U CN202122542893.0U CN202122542893U CN217589587U CN 217589587 U CN217589587 U CN 217589587U CN 202122542893 U CN202122542893 U CN 202122542893U CN 217589587 U CN217589587 U CN 217589587U
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- insert
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- threaded
- barrel
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Abstract
The utility model discloses an electric connector for aviation aircraft, the utility model relates to the technical field of electric connectors, which comprises a socket insulating shell and an inserting cylinder, wherein the socket insulating shell is positioned on the left side of the inserting cylinder; the outer side surface of the socket insulating shell is fixedly connected with a threaded sleeve, the outer side surface of the insert barrel is sleeved with a threaded insert barrel, threads are arranged on the inner side surface of the threaded sleeve and the outer side surface of the threaded insert barrel, and the threaded insert barrel is inserted into the threaded sleeve and is in threaded connection with the threaded sleeve; the right side surface of the socket insulating shell is provided with a slot, the upper end of the slot is provided with a positioning slot, the upper side surface of the left end of the inserting cylinder is fixedly connected with a positioning inserting block, and the inserting cylinder is inserted into the slot and is in sliding connection with the inner wall of the slot; the beneficial effects of the utility model reside in that: the two wires can be rapidly spliced with the correct splicing positions, the effect of improving the connection efficiency of the electric connector is achieved, and the effect of strengthening the connection stability of the electric connector can be achieved.
Description
Technical Field
The utility model belongs to the technical field of the electric connector technique and specifically relates to an electric connector for aviation aircraft is related to.
Background
The electric connector has the characteristics of good contact, reliable work and convenient maintenance, and is particularly applied to the electric connector in an aviation equipment circuit, and the normal operation of the electric connector for the aviation aircraft is related to the safety of the aviation aircraft.
Because the complexity of aerospace vehicle inner structure is higher, each part in aerospace vehicle's inside needs to pass through the various signal of telecommunication of circuit conduction, wherein electric connector is the device that is used for linking up different electric wire circuit, it has many littleer electric wires to integrate in the electric wire of transmission signal of telecommunication, the electric wire of transmission signal of telecommunication is connected and needs to ensure every small wire one-to-one switch-on, electric connector structure is too simple for current aerospace vehicle many, when needs connect through electric connector, be difficult to quick fix a position every small wire position, every small wire corresponds the switch-on and needs operating personnel carefully to distinguish the small wire and carry out the one-to-one and just can connect, need consume plenty of time, it is very inconvenient to use.
SUMMERY OF THE UTILITY MODEL
The utility model aims at the problem that above-mentioned exists with not enough, provide an electric connector for aircraft, can make two electric wires quick peg graft with correct grafting position, improve the effect of electric connector connection efficiency, and can play the effect of strengthening electric connector connection stability.
In order to achieve the purpose, the adopted technical scheme is as follows:
an electrical connector for an aircraft comprises a socket insulating shell and an insert barrel, wherein the socket insulating shell is positioned on the left side of the insert barrel;
the outer side surface of the socket insulating shell is fixedly connected with a threaded sleeve, the outer side surface of the inserting barrel is sleeved with a threaded inserting barrel, threads are arranged on the inner side surface of the threaded sleeve and the outer side surface of the threaded inserting barrel, and the threaded inserting barrel is inserted into the threaded sleeve and is in threaded connection with the threaded sleeve;
the socket comprises a socket insulating shell, and is characterized in that a slot is formed in the right side face of the socket insulating shell, a positioning slot is formed in the upper end of the slot, a positioning insertion block is fixedly connected to the upper side face of the left end of an insertion barrel, the insertion barrel is inserted into the slot and is in sliding connection with the inner wall of the slot, and the positioning insertion block is inserted into the positioning slot and is in sliding connection with the inner wall of the positioning slot.
Preferably, an inner socket is installed at the center of the left side surface of the slot, the inner socket is of a structure with an opening at the right end, a plugboard is installed in the opening at the right end of the inner socket, a jack post hole is formed at the center of the side surface of the plugboard, and six jack post holes surrounding the outer side of the jack post hole are formed in the side surface of the plugboard in a surrounding manner.
Preferably, the left side surface of the inner socket is fixedly connected with a cathode metal plate, a middle insertion tube is mounted at the center of the right side surface of the cathode metal plate, and six cathode contact plates surrounding the outer side of the middle insertion tube are mounted on the right side surface of the cathode metal plate.
Preferably, the right-hand member fixedly connected with positive pole metal sheet in inserting a section of thick bamboo, positive pole metal sheet left surface center department fixedly connected with middle part inserts the post, positive pole metal sheet left surface install six ring around in the contact pin in the middle part post outside.
Preferably, six contact pins pass six contact pin holes respectively and with contact pin downthehole wall sliding connection, the middle part is inserted the post and is passed in proper order insert post hole and middle part cartridge and respectively with a middle part cartridge and cartridge downthehole wall sliding connection.
Preferably, the left side face of the cathode metal plate is fixedly connected with a left end lead, the left end of the left end lead penetrates through the left side of the socket insulating shell, and the left end of the left end lead is externally connected with an information receiving device.
Preferably, the right side surface of the anode metal plate is fixedly connected with a right end lead, the right end of the right end lead penetrates through the right side of the insertion cylinder, and the right end of the right end lead is externally connected with information transmission equipment.
By adopting the technical scheme, the beneficial effects are as follows:
the location inserted block has different shapes, and every location inserted block all is equipped with the location slot of corresponding shape, only the location inserted block agrees with the location slot shape mutually, the section of thick bamboo left end just can insert in the slot that corresponds, and six contact pins of installing around are corresponding with six negative pole contact plates position one-to-one, when the section of thick bamboo that inserts fully inserts in the slot, six contact pins also pass six contact pin holes in proper order and contact with six negative pole contact plates, the middle part that is equipped with between the six contact pins is inserted the post and can is strengthened the grafting intensity of inserting a section of thick bamboo and slot, location slot and location inserted block can make operating personnel quick correspond the right-hand member wire with exact left end wire and right-hand member wire fast, and quick correct connection, shorten operating time, play the effect that improves the availability factor, insert a screw thread section of thick bamboo and threaded connection with the section of thick bamboo after the section of thick bamboo accomplishes the grafting with the slot, above structure can play the effect of further strengthening electric connector joint strength.
Drawings
Fig. 1 is a schematic view of the overall front view disconnected state three-dimensional structure of the present invention;
fig. 2 is a schematic view of the overall broken-off state section structure of the present invention;
FIG. 3 is a schematic view of the overall insertion state section structure of the present invention;
fig. 4 is a right-view structural schematic diagram of the socket insulating housing of the present invention;
fig. 5 is a left side view structural diagram of the insertion tube of the present invention.
The mark in the figure is: the socket comprises a left end lead 1, a socket insulating shell 2, a cathode metal plate 3, a slot 4, a positioning slot 5, a threaded sleeve 6, an inner socket 7, a cathode contact plate 8, a middle plug-in barrel 9, a plug-in plate 10, a pin hole 1001, a plug-in post hole 1002, a plug-in barrel 11, a positioning plug block 12, a pin 13, a middle plug-in post 14, a threaded plug-in barrel 15, an anode metal plate 16 and a right end lead 17.
Detailed Description
Referring to fig. 1 to 5, the present application is an electrical connector for an aircraft, including a receptacle insulating housing 2 and a plug barrel 11, where the receptacle insulating housing 2 is located on the left side of the plug barrel 11;
the outer side surface of the socket insulating shell 2 is fixedly connected with a threaded sleeve 6, the outer side surface of the inserting cylinder 11 is sleeved with a threaded inserting cylinder 15, the threaded inserting cylinder 15 can slide left and right on the outer side surface of the inserting cylinder 11, threads are respectively arranged on the inner side surface of the threaded sleeve 6 and the outer side surface of the threaded inserting cylinder 15, and the threaded inserting cylinder 15 is inserted into the threaded sleeve 6 and is in threaded connection with the threaded sleeve 6;
a slot 4 is formed in the right side surface of the socket insulating shell 2, a positioning slot 5 is formed in the upper end of the slot 4, a positioning insertion block 12 is fixedly connected to the upper side surface of the left end of the insertion cylinder 11, the insertion cylinder 11 is inserted into the slot 4 and is in sliding connection with the inner wall of the slot 4, the positioning insertion block 12 is inserted into the positioning slot 5 and is in sliding connection with the inner wall of the positioning slot 5, and two corresponding left-end lead 1 and right-end lead 17 can be rapidly distinguished through the positioning slot 5 and the positioning insertion block 12;
an inner socket 7 is installed at the center of the left side surface of the slot 4, the inner socket 7 is of a structure with an opening at the right end, a plug board 10 is installed in the opening at the right end of the inner socket 7, a plug column hole 1002 is formed at the center of the side surface of the plug board 10, and six plug pin holes 1001 surrounding the plug column hole 1002 are formed in the side surface of the plug board 10 in a surrounding manner;
the left side surface of the inner insert seat 7 is fixedly connected with a cathode metal plate 3, the center of the right side surface of the cathode metal plate 3 is provided with a middle insertion cylinder 9, and the right side surface of the cathode metal plate 3 is provided with six cathode contact plates 8 surrounding the outer side of the middle insertion cylinder 9;
an anode metal plate 16 is fixedly connected to the inner right end of the insert barrel 11, a middle insert column 14 is fixedly connected to the center of the left side face of the anode metal plate 16, and six insert pins 13 surrounding the outer side of the middle insert column 14 are mounted on the left side face of the anode metal plate 16;
the six pins 13 respectively penetrate through the six pin holes 1001 and are in sliding connection with the inner walls of the pin holes 1001, and the middle insertion column 14 sequentially penetrates through the insertion column hole 1002 and the middle insertion column 9 and is in sliding connection with the inner walls of the middle insertion column 9 and the insertion column hole 1002;
the left side surface of the cathode metal plate 3 is fixedly connected with a left end lead 1, the left end of the left end lead 1 penetrates through the left side of the socket insulating shell 2, and the left end of the left end lead 1 is externally connected with information receiving equipment;
the right side surface of the anode metal plate 16 is fixedly connected with a right end lead 17, the right end of the right end lead 17 penetrates through the right side of the insertion cylinder 11, and the right end of the right end lead 17 is externally connected with information transmission equipment;
the positioning plug 12 and the slot 4 can have various shapes, when the electric connector is connected, the socket insulating shell 2 and the plug barrel 11 corresponding to the positioning plug 12 and the slot 4 in shapes are found quickly, the plug barrel 11 is inserted into the slot 4, the positioning plug 12 with the same shape is embedded into the slot 4, six pins 13 respectively pass through six pin holes 1001 and are respectively contacted with six cathode contact plates 8, a right end lead 17 and a left end lead 1 are in circuit connection, data transmission is started, a middle plug 14 passes through a plug hole 1002 and is inserted into a middle plug barrel 9, the middle plug barrel 9 can strengthen the plug strength of the electric connector, the connector is prevented from being bent or shaken, the effect of protecting the six pins 13 is achieved, an operator can quickly group different left end leads 1 and right end leads 17 quickly through the positioning plug 12 and the positioning slot 5, the time required for connection is shortened, the effect of improving the electric wire connection efficiency is achieved, after the plug barrel 11 is plugged into the slot 4, the threaded sleeve 6 is fixedly connected to the outer side face of the socket insulating shell 2, the threaded plug barrel 15 is sleeved on the outer side face of the threaded plug barrel, the threaded plug barrel 11 can further strengthen the effect of the threaded connection of the plug barrel 6 and the threaded sleeve 6, and the threaded connection effect of the plug barrel 15 can be further improved.
Claims (7)
1. The utility model provides an electrical connector for aerospace vehicle, includes socket insulating casing (2) and inserts a section of thick bamboo (11), socket insulating casing (2) are located insert a section of thick bamboo (11) left side, its characterized in that:
the outer side surface of the socket insulating shell (2) is fixedly connected with a threaded sleeve (6), the outer side surface of the insert barrel (11) is sleeved with a threaded insert barrel (15), threads are respectively arranged on the inner side surface of the threaded sleeve (6) and the outer side surface of the threaded insert barrel (15), and the threaded insert barrel (15) is inserted into the threaded sleeve (6) and is in threaded connection with the threaded sleeve (6);
socket insulating casing (2) right flank has seted up slot (4), positioning slot (5) have been seted up to slot (4) upper end, side fixedly connected with location inserted block (12) on inserting a section of thick bamboo (11) left end, insert a section of thick bamboo (11) insert slot (4) and with slot (4) inner wall sliding connection, location inserted block (12) insert positioning slot (5) and with positioning slot (5) inner wall sliding connection.
2. An electrical connector for an aerospace vehicle according to claim 1, wherein: an inner inserting seat (7) is installed at the center of the left side face of the inserting groove (4), the inner inserting seat (7) is of a structure with an opening at the right end, an inserting plate (10) is installed in the opening at the right end of the inner inserting seat (7), a inserting column hole (1002) is formed in the center of the side face of the inserting plate (10), and six inserting needle holes (1001) surrounding the outer side of the inserting column hole (1002) are formed in the side face of the inserting plate (10) in a surrounding mode.
3. An electrical connector for an aerospace vehicle according to claim 2, wherein: the cathode metal plate (3) is fixedly connected to the left side face of the inner inserting seat (7), a middle inserting cylinder (9) is installed at the center of the right side face of the cathode metal plate (3), and six cathode contact plates (8) surrounding the outer side of the middle inserting cylinder (9) are installed on the right side face of the cathode metal plate (3).
4. An electrical connector for an aerospace vehicle according to claim 2, wherein: insert right-hand member fixedly connected with positive pole metal sheet (16) in a section of thick bamboo (11), positive pole metal sheet (16) left surface center department fixedly connected with middle part is inserted post (14), install six rings on positive pole metal sheet (16) left surface in the contact pin (13) in the middle part is inserted the post (14) outside.
5. An electrical connector for an aerospace vehicle according to claim 4, wherein: six contact pin (13) pass six contact pin holes (1001) respectively and with contact pin hole (1001) inner wall sliding connection, middle part insert post (14) pass in proper order insert post hole (1002) and middle part insert a section of thick bamboo (9) and respectively with a middle part insert a section of thick bamboo (9) and insert post hole (1002) inner wall sliding connection.
6. An electrical connector for an aerospace vehicle according to claim 3, wherein: the left side of the cathode metal plate (3) is fixedly connected with a left end lead (1), the left end of the left end lead (1) penetrates through the left side of the socket insulating shell (2), and the left end of the left end lead (1) is externally connected with an information receiving device.
7. An electrical connector for an aerospace vehicle according to claim 4, wherein: the right side surface of the anode metal plate (16) is fixedly connected with a right end lead (17), the right end of the right end lead (17) penetrates through the right side of the inserting barrel (11), and the right end of the right end lead (17) is externally connected with information transmission equipment.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202122542893.0U CN217589587U (en) | 2021-10-21 | 2021-10-21 | Electric connector for aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202122542893.0U CN217589587U (en) | 2021-10-21 | 2021-10-21 | Electric connector for aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN217589587U true CN217589587U (en) | 2022-10-14 |
Family
ID=83526225
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202122542893.0U Active CN217589587U (en) | 2021-10-21 | 2021-10-21 | Electric connector for aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN217589587U (en) |
-
2021
- 2021-10-21 CN CN202122542893.0U patent/CN217589587U/en active Active
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