CN209709274U - A kind of aviation socket with dust reduction capability - Google Patents

A kind of aviation socket with dust reduction capability Download PDF

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Publication number
CN209709274U
CN209709274U CN201920874520.3U CN201920874520U CN209709274U CN 209709274 U CN209709274 U CN 209709274U CN 201920874520 U CN201920874520 U CN 201920874520U CN 209709274 U CN209709274 U CN 209709274U
Authority
CN
China
Prior art keywords
fixedly connected
cover board
jack body
aviation socket
reduction capability
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Fee Related
Application number
CN201920874520.3U
Other languages
Chinese (zh)
Inventor
刘卫民
李安良
臧杰
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Zhengzhou Hanglian Rui Electronic Technology Co Ltd
Original Assignee
Zhengzhou Hanglian Rui Electronic Technology Co Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Zhengzhou Hanglian Rui Electronic Technology Co Ltd filed Critical Zhengzhou Hanglian Rui Electronic Technology Co Ltd
Priority to CN201920874520.3U priority Critical patent/CN209709274U/en
Application granted granted Critical
Publication of CN209709274U publication Critical patent/CN209709274U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Abstract

The utility model relates to aviation socket technical fields, and disclose a kind of aviation socket with dust reduction capability, including jack body, the side hinge connection of the jack body has cover board, the cover board is fixedly connected with positioning plate far from the side at hinge connection, the side wall of the jack body is fixedly connected with L shape snap-gauge corresponding with positioning plate, the L shape snap-gauge opens up fluted close to the side of positioning plate, thrust spring is equipped in the groove, one end of the thrust spring is fixedly connected with the slot bottom of groove, the other end of the thrust spring is fixedly connected with locating rod, the side wall of the positioning plate offers locating slot corresponding with locating rod.The utility model, which avoids dust and is easily accessible in the jack of jack body, influences the problem of using.

Description

A kind of aviation socket with dust reduction capability
Technical field
The utility model relates to aviation socket technical field more particularly to a kind of aviation sockets with dust reduction capability.
Background technique
Aviation plug is one kind of connector, is derived from military industry, therefore is gained the name, abbreviation air plug.Aviation plug is connection electricity The electromechanical compo of gas route, therefore the electric parameter of its own is that selection aviation plug first has to consider the problems of.Correctly choosing Select and using aviation plug be guarantee circuit reliability an importance.
Current aviation socket can make jack be exposed to external environment when being not connected to plug, be easy to make adherency ash in jack Dirt is not easy to be cleared up, and dust is easy to influence the accuracy of electrical grafting.
Utility model content
Purpose of the utility model is to solve aviation sockets in the prior art can make jack when being not connected to plug It is exposed to external environment, is easy to make adhering dust in jack, is not easy to be cleared up, and dust is easy to influence the standard of electrical grafting The problem of true property, and a kind of aviation socket with dust reduction capability proposed.
To achieve the goals above, the utility model adopts the technical scheme that
The side hinge connection of a kind of aviation socket with dust reduction capability, including jack body, the jack body has Cover board, the cover board are fixedly connected with positioning plate far from the side at hinge connection, and the side wall of the jack body is fixedly connected There is a L shape snap-gauge corresponding with positioning plate, the L shape snap-gauge opens up fluted close to the side of positioning plate, is equipped in the groove Thrust spring, one end of the thrust spring are fixedly connected with the slot bottom of groove, and the other end of the thrust spring is fixedly connected There is locating rod, the side wall of the positioning plate offers locating slot corresponding with locating rod, and the locating rod is located at one in groove End is fixedly connected with pull rod, and one end of the remotely located bar of pull rod through the surface of L shape snap-gauge and is fixedly connected by through-hole There is pulling plate, the side of the cover board is fixedly connected with multiple rubber plugs corresponding with jack body is equipped with jack, described Side of the cover board far from jack body is fixedly connected with the same protective plate by multiple buffer springs.
Preferably, the surface of the pulling plate is fixedly connected with drawstring.
Preferably, the locating rod is set as inclined-plane close to a side lever wall of positioning plate.
Preferably, the four corners of the protective plate and lid surface are fixedly connected to limit telescopic bar.
Preferably, the protective plate is fixedly connected with one layer of buffer rubber gasket far from the side of cover board.
Preferably, the locating rod is located at the side pole wall in groove and is symmetrically fixedly connected there are two position limiting slide block, described The inner wall of groove offers the limit sliding chutes to match with position limiting slide block.
Compared with prior art, the utility model provides a kind of aviation socket with dust reduction capability, and having following has Beneficial effect:
1, the aviation socket with dust reduction capability, by the cover board being equipped with, when not needing using jack body, overturning Cover board blocks cover board by the opening of jack body, and positioning plate squeezes the inclined-plane of locating rod at this time, and locating rod stress is mobile certainly Dynamic to retract in groove, when the locating slot on positioning plate is moved at locating rod, thrust spring pushes locating rod, and locating rod is pushed away Groove is outer out and locating rod is made to engage the firm limit that can be realized to cover board with locating slot, can be to the opening of jack body Be effectively protected avoiding dust and being easily accessible in the jack of jack body and influence the problem of using, and is needing to open lid When plate, pulling plate is pulled by drawstring, locating rod is pulled out to the relative limit lock that can be released outside locating slot to cover board using pull rod It is fixed, it is easy to operate, it is easy to use.
2, the aviation socket with dust reduction capability, by the rubber plug being equipped on the inside of cover board, rubber plug is plugged on Further proofing dust and protecting can be carried out to jack in the jack of jack body, adhering dust in jack is avoided to influence electrical grafting The problem of.
3, aviation socket with dust reduction capability, by the protective plate being equipped with, in jack body opening by the external world When impact, protective plate stress carries out first-level buffer shock-absorbing protecting using buffer rubber gasket, and protective plate squeezes buffer spring again, Level 2 buffering damping is carried out using the screen resilience that buffer spring deformation generates, there is preferable safety to jack body.
And be not directed to part in the device and be the same as those in the prior art or can be realized by using the prior art, this is practical The novel dust that avoids is easily accessible in the jack of jack body the problem of influencing use.
Detailed description of the invention
Fig. 1 be the utility model proposes a kind of aviation socket with dust reduction capability structural schematic diagram;
Fig. 2 be the utility model proposes a kind of aviation socket part A with dust reduction capability structural schematic diagram;
Fig. 3 be the utility model proposes the cover board of the aviation socket with dust reduction capability a kind of connected with rubber plug Structural schematic diagram.
In figure: 1 jack body, 2 cover boards, 3 positioning plates, 4L shape snap-gauge, 5 grooves, 6 thrust springs, 7 locating rods, 8 positioning Slot, 9 pull rods, 10 pulling plates, 11 rubber plugs, 12 buffer springs, 13 protective plates, 14 limit telescopic bars, 15 buffer rubber gaskets.
Specific embodiment
The following will be combined with the drawings in the embodiments of the present invention, carries out the technical scheme in the embodiment of the utility model Clearly and completely describe, it is clear that the described embodiments are only a part of the embodiments of the utility model, rather than whole Embodiment.
In the description of the present invention, it should be understood that term " on ", "lower", "front", "rear", "left", "right", The orientation or positional relationship of the instructions such as "top", "bottom", "inner", "outside" is to be based on the orientation or positional relationship shown in the drawings, and is only For ease of description the utility model and simplify description, rather than the device or element of indication or suggestion meaning must have it is specific Orientation, be constructed and operated in a specific orientation, therefore should not be understood as limiting the present invention.
Referring to Fig.1-3, it closes the side of a kind of aviation socket with dust reduction capability, including jack body 1, jack body 1 Page is connected with cover board 2, and cover board 2 is fixedly connected with positioning plate 3 far from the side at hinge connection, and the side wall of jack body 1 is fixed It is connected with L shape snap-gauge 4 corresponding with positioning plate 3, L shape snap-gauge 4 opens up fluted 5 close to the side of positioning plate 3, sets in groove 5 There is thrust spring 6, one end of thrust spring 6 is fixedly connected with the slot bottom of groove 5, and the other end of thrust spring 6 is fixedly connected with Locating rod 7, the side wall of positioning plate 3 offer locating slot 8 corresponding with locating rod 7, and it is solid that locating rod 7 is located at one end in groove 5 Surely it is connected with pull rod 9, one end of the remotely located bar 7 of pull rod 9 through the surface of L shape snap-gauge 4 and is fixedly connected with drawing by through-hole Plate 10, the side of cover board 2 are fixedly connected with the corresponding rubber plug 11 of multiple jacks being equipped with jack body 1, and cover board 2 is remote Side from jack body 1 is fixedly connected with the same protective plate 13 by multiple buffer springs 12.
The surface of pulling plate 10 is fixedly connected with drawstring.
Locating rod 7 is set as inclined-plane close to a side lever wall of positioning plate 3.
The four corners on protective plate 13 and 2 surface of cover board are fixedly connected to limit telescopic bar 14.
Protective plate 13 is fixedly connected with one layer of buffer rubber gasket 15 far from the side of cover board 2.
Locating rod 7 is located at the side pole wall in groove 5 and is symmetrically fixedly connected there are two position limiting slide block, and the inner wall of groove 5 is opened Equipped with the limit sliding chutes to match with position limiting slide block.
In the utility model, in use, when not needing using jack body 1, overturning cover board 2 by the cover board 2 being equipped with Block cover board 2 by the opening of jack body 1, positioning plate 3 squeezes the inclined-plane of locating rod 7 at this time, and 7 stress of locating rod is mobile certainly Dynamic to retract in groove 5, when the locating slot 8 on positioning plate 3 is moved at locating rod 7, thrust spring 6 pushes locating rod 7, will determine Position bar 7 is released outside groove 5 and locating rod 7 is made to engage the firm limit that can be realized to cover board 2 with locating slot 8, can be to socket The opening of ontology 1, which be effectively protected avoiding dust and being easily accessible in the jack of jack body 1, influences the problem of using, And when needing to open cover board 2, pulling plate 10 is pulled by drawstring, and locating rod 7 being pulled out using pull rod 9 can solve outside locating slot 8 It is easy to operate except the relative limit locking to cover board 2, it is easy to use, passes through the rubber plug 11 being equipped on the inside of cover board 2, rubber Plug 11, which is plugged in the jack of jack body 1, to carry out further proofing dust and protecting to jack, avoid adherency ash in jack Dirt influences the problem of electrical grafting, by the protective plate 13 being equipped with, when 1 opening of jack body is collided by foreign impacts, 13 stress of protective plate carries out first-level buffer shock-absorbing protecting using buffer rubber gasket 15, and protective plate 13 squeezes buffer spring 12 again, benefit Level 2 buffering damping is carried out with the screen resilience that 12 deformation of buffer spring generates, there is preferable safety to jack body 1.
The preferable specific embodiment of the above, only the utility model, but the protection scope of the utility model is not It is confined to this, anyone skilled in the art is within the technical scope disclosed by the utility model, practical according to this Novel technical solution and its utility model design are subject to equivalent substitution or change, should all cover the protection model in the utility model Within enclosing.

Claims (6)

1. a kind of aviation socket with dust reduction capability, including jack body (1), which is characterized in that the jack body (1) Side hinge connection has cover board (2), and the cover board (2) is fixedly connected with positioning plate (3) far from the side at hinge connection, described The side wall of jack body (1) is fixedly connected with L shape snap-gauge (4) corresponding with positioning plate (3), and the L shape snap-gauge (4) is close to positioning The side of plate (3) opens up fluted (5), is equipped with thrust spring (6) in the groove (5), one end of the thrust spring (6) with The slot bottom of groove (5) is fixedly connected, and the other end of the thrust spring (6) is fixedly connected with locating rod (7), the positioning plate (3) side wall offers locating slot (8) corresponding with locating rod (7), and it is solid that the locating rod (7) is located at one end in groove (5) Surely be connected with pull rod (9), one end of the remotely located bar of the pull rod (9) (7) by through-hole through the surface of L shape snap-gauge (4) and It is fixedly connected with pulling plate (10), the side of the cover board (2) is fixedly connected with multiple jacks pair being equipped with jack body (1) The rubber plug (11) answered, side of the cover board (2) far from jack body (1) are fixedly connected by multiple buffer springs (12) There are the same protective plate (13).
2. a kind of aviation socket with dust reduction capability according to claim 1, which is characterized in that the pulling plate (10) Surface is fixedly connected with drawstring.
3. a kind of aviation socket with dust reduction capability according to claim 1, which is characterized in that the locating rod (7) A side lever wall close to positioning plate (3) is set as inclined-plane.
4. a kind of aviation socket with dust reduction capability according to claim 1, which is characterized in that the protective plate (13) Limit telescopic bar (14) are fixedly connected to the four corners on cover board (2) surface.
5. a kind of aviation socket with dust reduction capability according to claim 1, which is characterized in that the protective plate (13) Side far from cover board (2) is fixedly connected with one layer of buffer rubber gasket (15).
6. a kind of aviation socket with dust reduction capability according to claim 1, which is characterized in that the locating rod (7) A side pole wall in groove (5) is symmetrically fixedly connected there are two position limiting slide block, and the inner wall of the groove (5) is offered and limited The limit sliding chutes that position sliding block matches.
CN201920874520.3U 2019-06-12 2019-06-12 A kind of aviation socket with dust reduction capability Expired - Fee Related CN209709274U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201920874520.3U CN209709274U (en) 2019-06-12 2019-06-12 A kind of aviation socket with dust reduction capability

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201920874520.3U CN209709274U (en) 2019-06-12 2019-06-12 A kind of aviation socket with dust reduction capability

Publications (1)

Publication Number Publication Date
CN209709274U true CN209709274U (en) 2019-11-29

Family

ID=68651571

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201920874520.3U Expired - Fee Related CN209709274U (en) 2019-06-12 2019-06-12 A kind of aviation socket with dust reduction capability

Country Status (1)

Country Link
CN (1) CN209709274U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111983266A (en) * 2020-08-21 2020-11-24 郑州德睿航联电子技术有限公司 Automatic control screen test box with aviation plug

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111983266A (en) * 2020-08-21 2020-11-24 郑州德睿航联电子技术有限公司 Automatic control screen test box with aviation plug

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Date Code Title Description
GR01 Patent grant
GR01 Patent grant
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20191129

Termination date: 20200612

CF01 Termination of patent right due to non-payment of annual fee