CN213717164U - Aviation plug butt joint auxiliary device - Google Patents
Aviation plug butt joint auxiliary device Download PDFInfo
- Publication number
- CN213717164U CN213717164U CN202023222620.XU CN202023222620U CN213717164U CN 213717164 U CN213717164 U CN 213717164U CN 202023222620 U CN202023222620 U CN 202023222620U CN 213717164 U CN213717164 U CN 213717164U
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- plug
- sleeve
- socket
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Abstract
The utility model relates to an aviation plug butt joint auxiliary device, which comprises a first auxiliary joint part and a second auxiliary joint part, wherein the first auxiliary joint part comprises an auxiliary pipe structure, a plug driving mechanism is connected on the auxiliary pipe structure, and the plug driving mechanism can drive the auxiliary pipe structure to slide along the axial direction; one end of the auxiliary pipe structure is provided with a guide plug, an aviation plug is sleeved in the guide plug, and the guide plug and the aviation plug can slide and swing under the driving of the auxiliary pipe structure; the second auxiliary joint part comprises a guide socket, an aviation socket is sleeved in the guide socket, and the guide socket can be connected with the movable vehicle body; the plugging stroke length of the guide plug and the guide socket is greater than that of the aviation plug and the aviation socket. The utility model discloses a plug actuating mechanism direct drive butt joint realizes the automatic butt joint of aviation joint, and the device simple structure makes, installs and maintains the convenience, uses reliably.
Description
Technical Field
The utility model relates to a metallurgical industry aviation connector technical field especially relates to an aviation plug butt joint auxiliary device.
Background
Currently, the known aviation plug is widely applied to various electric lines and plays a role in connecting or disconnecting a circuit.
At present, the aviation plugs are manually butted, and an aviation connector butt joint auxiliary device for realizing automatic butt joint by using an actuating mechanism is not available.
Therefore, the inventor provides an aviation plug butt joint auxiliary device by virtue of experience and practice of related industries for many years so as to realize automatic butt joint of aviation connectors.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide an aviation plug docks auxiliary device, the device adopt plug actuating mechanism direct drive to dock, realize aviation connector's automatic butt joint, the device simple structure, and it is convenient to make, install and maintain, uses reliably.
The utility model aims at realizing the effect, an aviation plug butt joint auxiliary device comprises a first auxiliary joint part and a second auxiliary joint part, wherein the first auxiliary joint part comprises an auxiliary pipe structure which is used for being connected with a fixed platform, and a plug driving mechanism is connected on the auxiliary pipe structure and can drive the auxiliary pipe structure to slide along the axial direction; a guide plug is arranged at one end of the auxiliary pipe structure, an aviation plug is sleeved in the guide plug, and the guide plug and the aviation plug can slide and swing under the driving of the auxiliary pipe structure; the second auxiliary joint part comprises a guide socket which can be plugged with or separated from the guide plug, an aviation socket which can be plugged with or separated from the aviation plug is sleeved in the guide socket, and the guide socket is used for being connected with the movable vehicle body; the plug-in stroke length of the guide plug and the guide socket is greater than that of the aviation plug and the aviation socket.
In a preferred embodiment of the present invention, the auxiliary tube structure includes a swinging sleeve, the swinging sleeve is sleeved in the sliding block, and the swinging sleeve can swing in the sliding block; the swing sleeve is sleeved on the telescopic sleeve, the swing sleeve can be axially fixed with the telescopic sleeve and can axially slide along the telescopic sleeve, and one end of the telescopic sleeve is connected with the guide plug; the sliding block is connected with the plug driving mechanism, and the plug driving mechanism can drive the sliding block, the swinging sleeve, the telescopic sleeve and the guide plug to axially slide along the telescopic sleeve.
In a preferred embodiment of the present invention, the outer wall of the telescopic sleeve is provided with a key along the axial direction thereof, and one side of the inner wall of the swing sleeve, which is close to the guide plug, is provided with a key groove that can be slidably sleeved on the key, and the swing sleeve can slide along the key; the spring is sleeved on the telescopic sleeve, a first connecting flange with the diameter being increased is arranged at one end of the telescopic sleeve, two ends of the spring respectively abut against the end face of the swing sleeve and the first connecting flange, and the first connecting flange is connected with the guide plug.
In a preferred embodiment of the present invention, the end of the swinging sleeve close to the guiding plug is connected with an outer sleeve with an increased diameter and extending toward the guiding plug, and the outer sleeve is disposed outside the spring.
In a preferred embodiment of the present invention, a positioning nut is disposed on an end of the swinging sleeve away from the guiding plug.
The utility model discloses an in a preferred embodiment, link up along swing sheathed tube axial in the sliding block and set up swing pipe passageway, set up the rubber sleeve in the swing pipe passageway, the swing sleeve pipe wears to establish through the rubber sleeve, the swing sleeve pipe can follow swing sheathed tube radial swing in the rubber sleeve.
The utility model discloses an in a preferred embodiment, the direction plug includes the plug casing, the first end of plug casing with telescopic tube connects, the second end of plug casing can insert and close in the direction socket, the first end of aviation plug is established to the inboard cover of first end of plug casing, the second end protrusion of plug casing sets up in aviation plug's second end.
The utility model discloses an in a preferred embodiment, link up along the axial in the plug casing and set up first through-hole, first fixed cover is established to the first pot head of first through-hole, and aviation plug's first pot head is located in the first fixed cover.
In a preferred embodiment of the present invention, the guide socket includes a socket housing, the socket housing is internally sleeved with an aviation socket, a second end of the aviation socket can be connected to an inner wall of the socket housing, and the second end of the socket housing can be connected to the moving vehicle body; the first end of the socket shell protrudes out of the first end of the aviation socket, and the second end of the plug shell can be inserted into the socket shell.
The utility model discloses an in a preferred embodiment, link up along the axial in the socket casing and set up the second through-hole, set up the fixed cover of second that the diameter is and reduces the setting in the second through-hole, aviation socket's second end cover is located in the fixed cover of second.
From above, the utility model provides an aviation plug docks auxiliary device has following beneficial effect:
the utility model provides an aviation plug docking auxiliary device, through the plug actuating mechanism direct drive control direction plug and direction socket, aviation plug and aviation socket insert or separate, degree of automation is high; the auxiliary pipe connected with the fixed platform is telescopic and can swing, so that certain axial, radial and angle deviations can be eliminated, and automatic butt joint is realized; the plugging stroke length of the guide plug and the guide socket is greater than that of the aviation plug and the aviation socket, so that the guiding effect in the plugging process is ensured; the utility model discloses an aviation plug butt joint auxiliary device, simple structure makes and simple to operate, uses reliably, and it is convenient to maintain.
Drawings
The drawings are only intended to illustrate and explain the present invention and do not limit the scope of the invention. Wherein:
FIG. 1: do the utility model discloses a schematic diagram when aviation plug docks auxiliary device is in the detached state.
FIG. 2: do the utility model discloses a schematic diagram when aviation plug docks auxiliary device is in the plug-in state.
FIG. 3: do the schematic view of the second auxiliary joint part of the present invention.
In the figure:
100. an aviation plug docking auxiliary device;
1. a first auxiliary joint part;
11. a guide plug; 111. a plug housing; 112. a first fixing sleeve; 113. a second connecting flange;
12. swinging the casing; 121. a keyway; 122. an outer sleeve;
13. a slider;
14. a telescopic sleeve; 141. a key; 142. a first connecting flange;
15. a spring;
16. positioning a nut;
17. a rubber sleeve;
2. a second auxiliary joint part;
21. a guide socket; 211. a socket housing; 212. a second fixing sleeve; 22. a third connecting flange;
41. an aviation plug; 42. an aviation socket.
Detailed Description
In order to clearly understand the technical features, objects, and effects of the present invention, embodiments of the present invention will be described with reference to the accompanying drawings.
The specific embodiments of the present invention described herein are for the purpose of explanation only and should not be construed as limiting the invention in any way. Given the teachings of the present invention, the skilled person can conceive of any possible variants based on the invention, which should all be considered as belonging to the scope of the invention. It will be understood that when an element is referred to as being "disposed on" another element, it can be directly on the other element or intervening elements may also be present. When an element is referred to as being "connected" to another element, it can be directly connected to the other element or intervening elements may also be present. The terms "mounted," "connected," and "connected" are to be construed broadly and may include, for example, mechanical or electrical connections, communications between two elements, direct connections, indirect connections through intermediaries, and the like. The terms "vertical," "horizontal," "upper," "lower," "left," "right," and the like as used herein are for illustrative purposes only and do not denote a unique embodiment.
Unless defined otherwise, 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 application belongs. The terminology used herein in the description of the present application is for the purpose of describing particular embodiments only and is not intended to be limiting of the application. As used herein, the term "and/or" includes any and all combinations of one or more of the associated listed items.
As shown in fig. 1 to 3, the utility model provides an aviation plug docking auxiliary device 100, which comprises a first auxiliary joint part 1 and a second auxiliary joint part 2, wherein the first auxiliary joint part 1 comprises an auxiliary pipe structure, the auxiliary pipe structure is used for being connected with a fixed platform, a plug driving mechanism is connected on the auxiliary pipe structure, and the plug driving mechanism can drive the auxiliary pipe structure to slide along the axial direction; a guide plug 11 is arranged at one end of the auxiliary pipe structure, an aviation plug 41 is sleeved in the guide plug 11, and the guide plug 11 and the aviation plug 41 can slide and swing under the driving of the auxiliary pipe structure; the second auxiliary joint part 2 comprises a guide socket 21 capable of being plugged in or separated from a guide plug, an aviation socket 42 capable of being plugged in or separated from an aviation plug is sleeved in the guide socket 21, and the guide socket 21 is used for being connected with a movable vehicle body. The plugging stroke length L2 of the guide plug 11 and the guide socket 21 is greater than the plugging stroke length L1 of the aviation plug 41 and the aviation socket 42, so that the guiding effect in the plugging process is ensured.
The utility model provides an aviation plug docking auxiliary device, through the plug actuating mechanism direct drive control direction plug and direction socket, aviation plug and aviation socket insert or separate, degree of automation is high; the auxiliary pipe connected with the fixed platform is telescopic and can swing, so that certain axial, radial and angle deviations can be eliminated, and automatic butt joint is realized; the plugging stroke length of the guide plug and the guide socket is greater than that of the aviation plug and the aviation socket, so that the guiding effect in the plugging process is ensured; the utility model discloses an aviation plug butt joint auxiliary device, simple structure makes and simple to operate, uses reliably, and it is convenient to maintain.
Further, as shown in fig. 1, the auxiliary tube structure includes a swing sleeve 12, the swing sleeve 12 is sleeved in a sliding block 13, and the swing sleeve 12 can swing in the sliding block 13; the swing sleeve 12 is sleeved on the telescopic sleeve 14, the swing sleeve 12 can be axially fixed with the telescopic sleeve 14 and can axially slide along the telescopic sleeve 14, and one end of the telescopic sleeve 14 is connected with the guide plug 11; the sliding block 13 is connected with a plug driving mechanism, and the plug driving mechanism can drive the sliding block 13, the swing sleeve 12, the telescopic sleeve 14 and the guide plug 11 to axially slide along the telescopic sleeve. In order to meet the requirement that the sliding block 13 slides stably, a fixed sliding rail is arranged on the fixed platform, and the plug driving mechanism drives the sliding block 13 and all parts mounted on the sliding block to slide along the fixed sliding rail.
Further, as shown in fig. 1, a key 141 is arranged on the outer wall of the telescopic sleeve 14 along the axial direction thereof, a key groove 121 which can be slidably sleeved on the key is arranged on one side of the inner wall of the swinging sleeve 12 close to the guiding plug 11, and the swinging sleeve 12 can slide along the key 141; the telescopic tube 14 is sleeved with a spring 15, one end of the telescopic tube 14 is provided with a first connecting flange 142 with an increased diameter, two ends of the spring 15 respectively prop against the end face of the swing sleeve 12 and the first connecting flange 142, and the first connecting flange 142 is connected with the guide plug 11. The plug-in stroke length of the guide plug 11 and the guide socket 21 is greater than the plug-in stroke length of the aviation plug 41 and the aviation socket 42,
as shown in fig. 2, after the aviation plug 41 is inserted into the aviation socket 42 in place, the guide plug 11 is inserted into the guide socket 21 in place at the same time, so that damage to the aviation plug 41 and the aviation socket 42 due to external force can be avoided; at this time, the plugging drive mechanism drives the slide block 13 to slide forward (in the direction close to the aviation socket 42), so as to push the telescopic sleeve 14 to slide on the swinging sleeve 12 through the key 141 and the key slot 121 on the swinging sleeve 12, and the spring 15 is compressed at the same time, thereby buffering the impact of external force.
Further, as shown in fig. 1, an outer sleeve 122 having an enlarged diameter and extending toward the guide plug is connected to one end of the swing sleeve 12 close to the guide plug 11, and the outer sleeve 122 is fitted to the outside of the spring 15.
As shown in fig. 1, in the present embodiment, a positioning nut 16 is fitted to an end of the swing sleeve 12 remote from the pilot pin 11.
Further, as shown in fig. 1, a swinging pipe passage is provided in the sliding block 13 so as to penetrate in the axial direction of the swinging sleeve 12, a rubber sleeve 17 is provided in the swinging pipe passage, the swinging sleeve 12 is inserted through the rubber sleeve 17, and the swinging sleeve 12 can swing in the rubber sleeve 17 in the radial direction of the swinging sleeve 12. The oscillating sleeve 12 can produce certain radial displacement and angular oscillation through the rubber sleeve 17 to eliminate deviation.
Further, as shown in fig. 1, the guiding plug 11 includes a plug housing 111, a first end of the plug housing 111 is connected to the telescopic sleeve 14, a second end of the plug housing 111 can be inserted into the guiding socket 21, a first end of the aviation plug 41 is sleeved inside the first end of the plug housing 111, and a second end of the plug housing 111 protrudes out of a second end of the aviation plug 41, so as to ensure that the guiding plug 11 and the guiding socket 21 are inserted before the aviation plug 41 and the aviation socket 42 are inserted, and the guiding plug 11 and the guiding socket 21 are later than the aviation plug 41 and the aviation socket 42 are separated, so as to guide and seal the inserting and pulling processes of the aviation plug 41 and the aviation socket 42.
Further, a first through hole is axially arranged in the plug housing 111 in a through manner, a first fixing sleeve 112 is sleeved at a first end of the first through hole, and the first fixing sleeve 112 is sleeved at a first end of the aviation plug 41.
For smooth plugging, the second end of the plug housing 111 is provided with an outer chamfer. To facilitate the connection with the telescopic tube 14, the first end of the plug housing 111 is provided with a second connecting flange 113, and the second connecting flange 113 is fixedly connected with the first connecting flange 142 by bolts.
Further, as shown in fig. 3, the guide socket 21 includes a socket housing 211, the aviation socket 42 is sleeved in the socket housing 211, a second end of the aviation socket 42 can be connected with an inner wall of the socket housing 211, and a second end of the socket housing 211 can be connected with the mobile vehicle body; the first end of the socket housing 211 protrudes from the first end of the aviation socket 42, and the second end of the plug housing 111 can be inserted into the socket housing 211. The plugging stroke length of the guide plug 11 and the guide socket 21 is greater than that of the aviation plug 41 and the aviation socket 42, so that the aviation plug 41 and the aviation socket 42 can be guided and sealed in the plugging and unplugging process.
Further, a second through hole is axially arranged in the socket housing 211 in a penetrating manner, a second fixing sleeve 212 with a reduced diameter is arranged in the second through hole, and the second end of the aviation socket 42 is sleeved in the second fixing sleeve 212.
For smooth plugging, the first end of the socket housing 211 is provided with an inner chamfer. To facilitate connection to the mobile vehicle body, the second end of the socket housing 211 is provided with a third connection flange 22.
The utility model discloses an aviation plug docks auxiliary device 100's working process as follows:
the joint connection process is as follows: the plugging driving mechanism pushes the sliding block 13 to slide towards the direction close to the second auxiliary joint part 2, the guide plug 11 is inserted into the socket shell 211 of the guide socket 21 under the action of the sliding block 13 and the swinging sleeve 12 and the telescopic sleeve 14 connected to the sliding block 13 and continues to slide, after the aviation plug 41 is inserted into the aviation socket 42 in place, the guide plug 11 is inserted into the guide socket 21 and is also in place at the same time, the plugging driving mechanism drives the sliding block 13 to slide forwards (towards the aviation socket 42), and the spring 15 is compressed at the same time to buffer external force impact;
the joint disconnecting process is opposite to the connecting process, the plugging driving mechanism pushes the sliding block 13 to slide in the direction away from the second auxiliary joint part 2, and after the aviation plug 41 leaves the aviation socket 42, the plugging driving mechanism pushes the sliding block 13 to continue sliding until the guide plug 11 leaves the guide socket 21.
From above, the utility model provides an aviation plug docks auxiliary device has following beneficial effect:
the utility model provides an aviation plug docking auxiliary device, through the plug actuating mechanism direct drive control direction plug and direction socket, aviation plug and aviation socket insert or separate, degree of automation is high; the auxiliary pipe connected with the fixed platform is telescopic and can swing, so that certain axial, radial and angle deviations can be eliminated, and automatic butt joint is realized; the plugging stroke length of the guide plug and the guide socket is greater than that of the aviation plug and the aviation socket, so that the guiding effect in the plugging process is ensured; the utility model discloses an aviation plug butt joint auxiliary device, simple structure makes and simple to operate, uses reliably, and it is convenient to maintain.
The above description is only exemplary of the present invention, and is not intended to limit the scope of the present invention. Any person skilled in the art should also realize that such equivalent changes and modifications can be made without departing from the spirit and principles of the present invention.
Claims (10)
1. An aviation plug butt joint auxiliary device is characterized by comprising a first auxiliary joint part and a second auxiliary joint part, wherein the first auxiliary joint part comprises an auxiliary pipe structure, the auxiliary pipe structure is used for being connected with a fixed platform, a plug-pull driving mechanism is connected to the auxiliary pipe structure, and the plug-pull driving mechanism can drive the auxiliary pipe structure to slide along the axial direction; a guide plug is arranged at one end of the auxiliary pipe structure, an aviation plug is sleeved in the guide plug, and the guide plug and the aviation plug can slide and swing under the driving of the auxiliary pipe structure; the second auxiliary joint part comprises a guide socket which can be plugged with or separated from the guide plug, an aviation socket which can be plugged with or separated from the aviation plug is sleeved in the guide socket, and the guide socket is used for being connected with the movable vehicle body; the plug-in stroke length of the guide plug and the guide socket is greater than that of the aviation plug and the aviation socket.
2. The aircraft plug docking aid of claim 1 wherein said accessory tube structure comprises a swinging sleeve, said swinging sleeve being nested within a sliding block, said swinging sleeve being capable of swinging within said sliding block; the swing sleeve is sleeved on the telescopic sleeve, the swing sleeve can be axially fixed with the telescopic sleeve and can axially slide along the telescopic sleeve, and one end of the telescopic sleeve is connected with the guide plug; the sliding block is connected with the plug driving mechanism, and the plug driving mechanism can drive the sliding block, the swinging sleeve, the telescopic sleeve and the guide plug to axially slide along the telescopic sleeve.
3. The aviation plug docking aid as claimed in claim 2, wherein a key is provided on the outer wall of said telescopic sleeve along the axial direction thereof, a key groove slidably fitted over the key is provided on the inner wall of said swinging sleeve on a side close to the guide plug, and said swinging sleeve is slidable along the key; the spring is sleeved on the telescopic sleeve, a first connecting flange with the diameter being increased is arranged at one end of the telescopic sleeve, two ends of the spring respectively abut against the end face of the swing sleeve and the first connecting flange, and the first connecting flange is connected with the guide plug.
4. An aviation plug docking aid as claimed in claim 3, wherein an end of said swinging sleeve adjacent to said guide plug is connected to an outer sleeve of increased diameter extending toward said guide plug, said outer sleeve being disposed outside said spring.
5. An aviation plug docking aid as claimed in claim 3, wherein a retaining nut is fitted over an end of said wobble sleeve remote from said guide plug.
6. The aircraft plug docking assistance device according to claim 2, wherein a swinging pipe passage is provided in the sliding block so as to pass through in an axial direction of a swinging sleeve, a rubber sleeve is provided in the swinging pipe passage, the swinging sleeve is inserted through the rubber sleeve, and the swinging sleeve can swing in the rubber sleeve in a radial direction of the swinging sleeve.
7. The assistant docking device as claimed in claim 2, wherein the guiding plug comprises a plug housing, a first end of the plug housing is connected to the telescopic tube, a second end of the plug housing is inserted into the guiding socket, the first end of the aviation plug is sleeved inside the first end of the plug housing, and the second end of the plug housing protrudes from the second end of the aviation plug.
8. The aircraft plug docking assistance device as claimed in claim 7, wherein a first through hole is axially provided through the plug housing, a first fixing sleeve is provided at a first end of the first through hole, and a first end of the aircraft plug is provided in the first fixing sleeve.
9. The aviation plug docking aid of claim 7, wherein said guide socket comprises a socket housing, said socket housing having an aviation socket disposed therein, a second end of said aviation socket being connectable to an interior wall of said socket housing, said second end of said socket housing being connectable to a mobile cart; the first end of the socket shell protrudes out of the first end of the aviation socket, and the second end of the plug shell can be inserted into the socket shell.
10. The aircraft plug docking assistance device as claimed in claim 9, wherein a second through hole is provided axially therethrough in said socket housing, a second retaining sleeve of reduced diameter is provided in said second through hole, and a second end of said aircraft socket is received in said second retaining sleeve.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202023222620.XU CN213717164U (en) | 2020-12-28 | 2020-12-28 | Aviation plug butt joint auxiliary device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202023222620.XU CN213717164U (en) | 2020-12-28 | 2020-12-28 | Aviation plug butt joint auxiliary device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN213717164U true CN213717164U (en) | 2021-07-16 |
Family
ID=76790254
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202023222620.XU Active CN213717164U (en) | 2020-12-28 | 2020-12-28 | Aviation plug butt joint auxiliary device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN213717164U (en) |
-
2020
- 2020-12-28 CN CN202023222620.XU patent/CN213717164U/en active Active
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