Needle withdrawing device for aviation plug

By designing a detachable aero plug needle retractor, the problem of inability to replace the pin when the pin is damaged is solved, and the individual replacement of the pin is realized, which avoids waste of resources and improves the service life of the equipment and the convenience of the user.

CN222261709UActive Publication Date: 2024-12-27XUZHOU CHINA RESOURCES POWER CO LTD +1
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Patent Information

Application Number
CN202420913282.3
Authority / Receiving Office
CN · China
Patent Type
Utility models(China)
Current Assignee / Owner
Filing Date
2024-04-28
Publication Date
2024-12-27
Estimated Expiration
2034-04-28

AI Technical Summary

Technical Problem

The pins of the existing aviation plug needle retractor are easily deformed due to excessive extrusion, which cannot be continued to be used, resulting in waste of resources, and the pins cannot be replaced separately.

Method used

An aviation plug needle retractor including handle and pin is designed. The mounting cavity and through hole are formed through the movable connection between the handle and the locking member. When the pin is damaged, the locking state of the locking member and the holder can be unlocked and separated. Position the block and pull the needle out of the through hole to separate the pin from the handle, allowing for separate replacement of the pin.

Benefits of technology

It realizes that the pin can be replaced separately when the pin is damaged, avoiding waste of resources, improving the service life of the equipment and user convenience.

✦ Generated by Eureka AI based on patent content.

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Abstract

The utility model relates to the technical field of circuit wiring, and discloses an aviation plug pin withdrawing device, which comprises a handle and a pin, and is characterized in that the handle comprises a holding piece and a locking piece, and the holding piece is movably connected with the locking piece; a mounting cavity is defined by the holding piece and the locking piece; a through hole communicated with the mounting cavity is formed in the locking piece; the contact pin comprises a pin head and a positioning block. The positioning block abuts against and is limited to the inner wall of the mounting cavity. The needle head is connected with the positioning block and penetrates through the through hole. And when the wire of the pin is withdrawn, the locking piece and the holding piece are locked, the positioning block is limited in the mounting cavity, and a user holds the holding piece to push out the wire on the aviation plug by using the pin head. According to the technical scheme of the utility model, when the contact pin is damaged, the locking piece and the holding piece are unlocked, the positioning block is withdrawn from the mounting cavity, and then the pin head is pulled out from the through hole of the locking piece, so that the contact pin is separated from the handle, and therefore, when the contact pin is damaged, the contact pin can be independently replaced, the use of a user is facilitated, and the waste of resources is avoided.
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Description

Technical Field

[0001] The utility model relates to the technical field of circuit wiring, in particular to an aviation plug needle remover. Background Art

[0002] The existing pin extractor used on the aviation plug consists of a pin and a handle. The pin is inserted into the hole of the aviation plug, and the handle drives the pin to squeeze the aviation plug to squeeze out the wire in the plug, thereby completing the wire extraction operation.

[0003] In actual use, the pin may be deformed due to excessive squeezing, making it unusable. Since the pin and the handle are fixedly connected, when the pin is damaged and cannot be used, the entire needle extractor can only be scrapped, resulting in a waste of resources. Utility Model Content

[0004] The main purpose of the utility model is to provide an aviation plug pin remover, which aims to solve the problem that the pins cannot be replaced separately when they are damaged.

[0005] In order to achieve the above-mentioned purpose, the aviation plug needle remover proposed by the utility model comprises:

[0006] A handle, the handle comprising a gripping member and a locking member, the gripping member being movably connected to the locking member; the gripping member and the locking member enclose a mounting cavity; the locking member is formed with a through hole communicating with the mounting cavity; and

[0007] The plug pin includes a needle head and a positioning block, wherein the positioning block abuts against the inner wall of the mounting cavity; the needle head is connected to the positioning block and penetrates into the through hole.

[0008] Optionally, an internal thread is formed at one end of the holding piece close to the locking piece; the locking piece includes a threaded section and a tightening section, and the threaded section is threadedly connected to the holding piece; the positioning block abuts against an end of the threaded section facing the holding piece, and the tightening section is connected to an end of the threaded section away from the positioning block.

[0009] Optionally, a plurality of positioning protrusions are formed on one end of the holding piece facing the positioning block, and the positioning block is formed with a slot corresponding to each positioning protrusion, and each positioning protrusion is inserted into a slot to limit the positioning block.

[0010] Optionally, the sum of the lengths of the threaded segment and the positioning block extending along the length direction of the gripping member is greater than the depth of the mounting cavity extending along the length direction of the gripping member.

[0011] Optionally, a plurality of anti-slip strips are formed on the outer side wall of the tightening section.

[0012] Optionally, the insertion pin further includes a connector, which is inserted into the through hole and includes at least a portion extending outside the through hole; the needle head is connected to an end of the connector extending outside the through hole, and the positioning block is connected to an end of the connector away from the needle head.

[0013] Optionally, the diameter of the positioning block is larger than the diameter of the through hole, and the cross-sectional area of ​​the connecting piece is larger than the cross-sectional area of ​​the needle.

[0014] Optionally, the needle, the connecting piece and the positioning block are integrally formed.

[0015] Optionally, the handle further includes an anti-skid pad, and the anti-skid pad is sleeved on an outer side wall of the gripping member.

[0016] Optionally, the anti-slip pad is made of rubber.

[0017] In the technical solution of the utility model, the aviation plug needle remover includes a handle and a pin, the handle includes a grip and a locking piece, the grip is movably connected to the locking piece; the grip and the locking piece enclose a mounting cavity; the locking piece forms a through hole connected to the mounting cavity; the pin includes a needle and a positioning block, the positioning block abuts against the inner wall of the mounting cavity; the needle is connected to the positioning block and penetrates the through hole. When the pin is withdrawn, the locking piece and the grip are locked, the positioning block is limited in the mounting cavity, and the user holds the grip and uses the needle to push the wire on the aviation plug. In the technical solution of the utility model, when the pin is damaged, the locking state of the locking piece and the grip is unlocked, the positioning block is withdrawn from the mounting cavity, the locking piece is separated from the grip, and then the needle is pulled out from the through hole of the locking piece to complete the separation of the pin and the handle, so that the pin can be replaced separately when it is damaged, which is convenient for users to use and avoids waste of resources. BRIEF DESCRIPTION OF THE DRAWINGS

[0018] In order to more clearly illustrate the embodiments of the utility model or the technical solutions in the prior art, the drawings required for use in the embodiments or the description of the prior art will be briefly introduced below. Obviously, the drawings described below are only some embodiments of the utility model. For ordinary technicians in this field, other drawings can be obtained based on the structures shown in these drawings without paying creative work.

[0019] Figure 1 This is a three-dimensional structural diagram of an embodiment of the aviation plug ejector provided by the utility model;

[0020] Figure 2 for Figure 1 The cross-sectional view of the aviation plug ejector along AA;

[0021] Figure 3for Figure 2 A partial enlarged view of point B in the middle.

[0022] Description of Figure Numbers:

[0023] Label name Label name 1000 Aviation plug remover 1221 Anti-slip strips 1 handle 1a Mounting cavity 11 Grip 13 Anti-slip mat 111 Positioning protrusion 2 Pin 12 Locking parts 21 Needles 12a Through Hole 22 Positioning block 121 Thread segment 22a Card slot 122 Tightening section 23 Connectors

[0024] The realization of the purpose, functional features and advantages of the utility model will be further explained in conjunction with embodiments and with reference to the accompanying drawings. DETAILED DESCRIPTION

[0025] The following will be combined with the drawings in the embodiments of the utility model to clearly and completely describe the technical solutions in the embodiments of the utility model. Obviously, the described embodiments are only part of the embodiments of the utility model, not all of the embodiments. Based on the embodiments of the utility model, all other embodiments obtained by ordinary technicians in this field without creative work are within the scope of protection of the utility model.

[0026] It should be noted that all directional indications in the embodiments of the present invention (such as up, down, left, right, front, back...) are only used to explain the relative position relationship, movement status, etc. between the components under a certain specific posture (as shown in the accompanying drawings). If the specific posture changes, the directional indication will also change accordingly.

[0027] In addition, the descriptions of "first", "second", etc. in the present utility model are only used for descriptive purposes and cannot be understood as indicating or implying their relative importance or implicitly indicating the number of the indicated technical features. Therefore, the features defined as "first" and "second" may explicitly or implicitly include at least one of the features. In addition, the meaning of "and / or" appearing in the full text includes three parallel schemes. Taking "A and / or B" as an example, it includes scheme A, or scheme B, or a scheme that satisfies both A and B. In addition, the technical solutions between the various embodiments can be combined with each other, but it must be based on the ability of ordinary technicians in this field to implement. When the combination of technical solutions is contradictory or cannot be implemented, it should be deemed that such a combination of technical solutions does not exist and is not within the scope of protection required by the present utility model.

[0028] Please refer to Figure 1 , Figure 2 as well as Figure 3 In order to solve the problem that the pins cannot be replaced individually when the pins are damaged, the utility model proposes an aviation plug pin remover 1000, comprising:

[0029] The handle 1 and the plug 2, the handle 1 includes a grip 11 and a locking member 12, the grip 11 and the locking member 12 are movably connected; the grip 11 and the locking member 12 enclose a mounting cavity 1a; the locking member 12 forms a through hole 12a connected to the mounting cavity 1a; the plug 2 includes a needle 21 and a positioning block 22, the positioning block 22 abuts against the inner wall of the mounting cavity 1a; the needle 21 is connected to the positioning block 22 and penetrates the through hole 12a. When the plug 2 is withdrawn, the locking member 12 is locked with the grip 11, the positioning block 22 is limited in the mounting cavity 1a, and the user holds the grip 11 and uses the needle 21 to push the wires on the aviation plug out.

[0030] In the technical solution of the present utility model, when the pin 2 is damaged, the locking state of the locking piece 12 and the holding piece 11 is unlocked, the positioning block 22 is withdrawn from the installation cavity 1a, and the locking piece 12 is separated from the holding piece 11, and then the needle 21 is pulled out from the through hole 12a of the locking piece 12 to complete the separation of the pin 2 and the handle 1. Therefore, when the pin 2 is damaged, the pin 2 can be replaced separately, which is convenient for users to use and avoids waste of resources.

[0031] The form of the movable connection between the holding member 11 and the locking member 12 can be that buckles are respectively provided on the holding member 11 and the locking member 12, and the holding member 11 and the locking member 12 are movably connected through the buckle connection; or threads are formed on the holding member 11 and the locking member 12, and the holding member 11 and the locking member 12 are movably connected through the cooperation between the thread structures. In one embodiment, the holding member 11 and the locking member 12 are threadedly connected.

[0032] It can be understood that the threaded connection between the grip 11 and the locking member 12 can be formed by forming an external thread on the grip 11 and an internal thread on the locking member 12, so that the grip 11 and the locking member 12 are threadedly connected; or it can be formed by forming an internal thread on the grip 11 and an external thread on the locking member 12, so that the grip 11 and the locking member 12 are threadedly connected. In one embodiment, an internal thread is formed at one end of the grip 11 close to the locking member 12; the locking member 12 includes a threaded section 121 and a tightening section 122, and the threaded section 121 is threadedly connected to the grip 11; the positioning block 22 is limited to the end of the threaded section 121 facing the grip 11, and the tightening section 122 is connected to the end of the threaded section 121 away from the positioning block 22. The user can hold the tightening section 122 and rotate the locking member 12 to complete the locking and unlocking between the locking member 12 and the grip 11, which is convenient for the user.

[0033] A plurality of positioning protrusions 111 are formed on one end of the gripping member 11 facing the positioning block 22, and a slot 22a is formed on the positioning block 22 corresponding to each positioning protrusion 111, and each positioning protrusion 111 is inserted into a slot 22a to limit the positioning block 22. In one embodiment, two positioning protrusions 111 are formed on one end of the gripping member 11 facing the positioning block 22, and two slots 22a are formed on the positioning block 22, and each positioning protrusion 111 is inserted into a slot 22a to limit the positioning block 22. The positioning block 22 is arranged in the installation cavity 1a formed by the holding piece 11 and the locking piece 12. The inner wall of the installation cavity 1a limits the positioning block 22 to prevent the positioning block 22 from moving. Two positioning protrusions 111 are formed on the holding piece 11 and inserted into the slot 22a on the positioning block 22, which can prevent the positioning block 22 from rotating in the installation cavity 1a. In this way, the positioning block 22 can be prevented from shaking when the needle 21 withdraws the wire, making the wire pushing process of the aviation plug needle remover 1000 more stable.

[0034] In one embodiment, the sum of the lengths of the threaded section 121 and the positioning block 22 extending in the length direction of the gripping member 11 is greater than the depth of the installation cavity 1a extending in the length direction of the gripping member 11. When the gripping member 11 and the locking member 12 are locked, the length of the threaded section 121 is long enough to extend deep into the installation cavity 1a, so as to ensure that the positioning block 22 can be pushed to a position abutting against the inner wall of the installation cavity 1a, thereby ensuring that the gripping member 11 and the locking member 12 can clamp the positioning block 22 to limit the positioning block 22, thereby preventing the positioning block 22 from shaking in the installation cavity 1a and affecting the stability of the aviation plug needle remover 1000 when pushing the wire.

[0035] It can be understood that a plurality of anti-slip strips 1221 are formed on the outer wall of the tightening section 122. In one embodiment, twenty anti-slip strips 1221 are formed on the outer wall of the tightening section 122. When the user holds the tightening section 122 to rotate the locking member 12, the anti-slip strips 1221 can prevent the user's hand from sliding relative to the tightening section 122, thereby avoiding the situation where the user's strength is too small to unscrew the locking member 12, and facilitating the use of the user.

[0036] In one embodiment, the plug pin 2 further includes a connector 23, which is inserted into the through hole 12a and at least partially extends outside the through hole 12a; the needle 21 is connected to one end of the connector 23 extending outside the through hole 12a, and the positioning block 22 is connected to one end of the connector 23 away from the needle 21. Since the holes of some aviation plugs are arc-shaped or have an inclined angle, the needle 21 may bend slightly when the plug pin 2 is inserted into the aviation plug. This arrangement avoids the situation where the needle 21 abuts against the hole wall of the through hole 12a when it is bent and is broken, thereby improving the service life of the plug pin 2 to a certain extent.

[0037] Specifically, the diameter of the positioning block 22 is larger than the diameter of the through hole 12a, and the cross-sectional area of ​​the connecting piece 23 is larger than the cross-sectional area of ​​the needle 21. The diameter of the positioning block 22 is larger than the diameter of the through hole 12a, which can prevent the positioning block 22 from slipping out of the through hole 12a and causing the entire aviation plug needle remover 1000 to fail; generally, the connecting piece 23, the needle 21 and the positioning block 22 are made of the same material, and the cross-sectional area of ​​the connecting piece 23 is larger than the cross-sectional area of ​​the needle 21, so that the structural strength of the connecting piece 23 is greater than the structural strength of the needle 21, so the force required to break the connecting piece 23 is greater than the force required to break the needle 21, so that the plug is less likely to be broken by the hole wall of the through hole 12a, thereby improving the service life of the plug pin 2.

[0038] In one embodiment, the needle head 21 , the connecting member 23 and the positioning block 22 are integrally formed, so that the overall structural strength of the insertion pin 2 is higher, thereby increasing the service life of the insertion pin 2 .

[0039] In one embodiment, the handle 1 further includes an anti-skid pad 13, which is sleeved on the outer wall of the grip. When the user holds the grip to rotate the locking member 12, the anti-skid pad 13 can prevent the user's hand from sliding relative to the grip, thereby avoiding the situation where the user's strength is too small to unscrew the locking member 12, and facilitating the use of the user.

[0040] Specifically, the material of the anti-slip pad 13 can be rubber or silicone. In one embodiment, the material of the anti-slip pad 13 is rubber. Since the action of unscrewing the locking member 12 is that the user's hand rotates the grip 11, and the action of using the aviation plug needle remover 1000 to push the wire is that the user's hand applies force along the length direction of the handle 1, and the force directions of the user's hands in the two actions are inconsistent, and both require preventing the user's hands from sliding relative to the grip 11, rubber is preferably used as the material of the anti-slip pad 13. The rubber anti-slip pad 13 can provide friction for the user's hands in all directions. Therefore, the rubber anti-slip pad 13 can prevent the user's hands from sliding relative to the grip 11 in both usage scenarios.

[0041] The above description is only a preferred embodiment of the present invention, and does not limit the patent scope of the present invention. All equivalent structural changes made by using the contents of the present invention specification and drawings under the inventive concept of the present invention, or directly / indirectly applied in other related technical fields are included in the patent protection scope of the present invention.

Claims

1. An aviation plug remover (1000), characterized in that: include: A handle (1), the handle (1) comprising a gripping member (11) and a locking member (12), the gripping member (11) and the locking member (12) being movably connected; the gripping member (11) and the locking member (12) enclose a mounting cavity (1a); the locking member (12) is formed with a through hole (12a) communicating with the mounting cavity (1a); and The insertion pin (2) comprises a needle head (21) and a positioning block (22), wherein the positioning block (22) abuts against an inner wall of the mounting cavity (1a); and the needle head (21) is connected to the positioning block (22) and is inserted into the through hole (12a).

2. The aviation plug remover (1000) according to claim 1, characterized in that: An internal thread is formed at one end of the holding member (11) close to the locking member (12); the locking member (12) comprises a threaded section (121) and a tightening section (122), and the threaded section (121) is threadedly connected to the holding member (11); the positioning block (22) is abutted against an end of the threaded section (121) facing the holding member (11), and the tightening section (122) is connected to an end of the threaded section (121) away from the positioning block (22).

3. The aviation plug remover (1000) according to claim 2, characterized in that: A plurality of positioning protrusions (111) are formed on one end of the holding member (11) facing the positioning block (22), and the positioning block (22) is formed with a slot (22a) corresponding to each positioning protrusion (111), and each positioning protrusion (111) is inserted into a slot (22a) to limit the positioning block (22).

4. The aviation plug remover (1000) according to claim 2, characterized in that: The sum of the lengths of the threaded section (121) and the positioning block (22) extending in the length direction of the gripping member (11) is greater than the depth of the mounting cavity (1a) extending in the length direction of the gripping member (11).

5. The aviation plug remover (1000) according to claim 2, characterized in that: A plurality of anti-slip strips (1221) are formed on the outer side wall of the tightening section (122).

6. The aviation plug remover (1000) according to any one of claims 1 to 5, characterized in that: The insertion pin (2) further comprises a connecting piece (23), wherein the connecting piece (23) is inserted into the through hole (12a) and at least partially extends outside the through hole (12a); the needle head (21) is connected to an end of the connecting piece (23) extending outside the through hole (12a), and the positioning block (22) is connected to an end of the connecting piece (23) away from the needle head (21).

7. The aviation plug remover (1000) according to claim 6, characterized in that: The diameter of the positioning block (22) is greater than the diameter of the through hole (12a), and the cross-sectional area of ​​the connecting piece (23) is greater than the cross-sectional area of ​​the needle (21).

8. The aviation plug remover (1000) according to claim 6, characterized in that: The needle (21), the connecting piece (23) and the positioning block (22) are integrally formed.

9. The aviation plug remover (1000) according to any one of claims 1 to 5, characterized in that: The handle (1) further comprises an anti-skid pad (13), wherein the anti-skid pad (13) is sleeved on the outer side wall of the gripping member (11).

10. The aviation plug remover (1000) according to claim 9, characterized in that: The material of the anti-slip pad (13) is rubber.