CN212695388U - Novel aviation connector tail clamp fixing device - Google Patents

Novel aviation connector tail clamp fixing device Download PDF

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Publication number
CN212695388U
CN212695388U CN202021847624.4U CN202021847624U CN212695388U CN 212695388 U CN212695388 U CN 212695388U CN 202021847624 U CN202021847624 U CN 202021847624U CN 212695388 U CN212695388 U CN 212695388U
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ring
tail clamp
pipe
wall
fixing device
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CN202021847624.4U
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Chinese (zh)
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葛恒江
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Shaanxi Sanhang Technology Co ltd
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Shaanxi Sanhang Technology Co ltd
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Abstract

The utility model provides a novel aviation connector tail clamp fixed device, including spliced pole, end fishplate bar, the tail presss from both sides, and first twisting connects the ring, and well takeover, rotatable rotation hang a structure, and the fixer structure is inhaled to slidable centre gripping magnetism, and the rotatable protection network tube structure that cup joints, the type of falling L dwang, the second is twisted and is connect the ring, the sponge circle, the outer jacket ring sum insert the lagging, the spliced pole peg graft in the lower part between end fishplate bar. The utility model is provided with the magnetic attraction fixer, the sleeve pipe, the square head bolt, the jacking plate and the tail clamp, which is beneficial to the fixation of the tail clamp through the magnetic attraction fixer in the using process and is convenient for the fixation and support of the tail clamp in the working process; the fixing base, U type connecting seat, bolt and nut, the bracing piece, the angle of plug socket and plug socket is favorable to adjusting at the in-process that uses to the setting of plug socket and spliced eye, conveniently installs the work at fixed in-process.

Description

Novel aviation connector tail clamp fixing device
Technical Field
The utility model belongs to the technical field of fixing device, especially, relate to a novel aviation connector tail press from both sides fixing device.
Background
In the prior art, when an aviation wire harness is processed, the aviation connector tail clamp is fixed and screwed directly by manual work, the connector is generally round, so that the reliability of the connector tail clamp in the manual screwing process has certain problems, and if other auxiliary tools such as sharp-nose pliers are used, the surface of the connector tail clamp is scratched, so that a tail clamp fixing device is designed for the situation.
However, the existing tail clamp fixing device also has the problems that the fixing work is inconvenient in the using process, the angle adjustment in the fixing process is inconvenient, and the protection is inconvenient in the using process.
Therefore, the invention is necessary to invent a novel aviation connector tail clamp fixing device.
SUMMERY OF THE UTILITY MODEL
In order to solve the technical problem, the utility model provides a novel aviation connector tail presss from both sides fixing device to solve current tail clamp fixing device and having the in-process inconvenient work of fixing that uses, inconvenient angle regulation and inconvenient in-process at fixed in-process protect the problem of using. A novel aviation connector tail clamp fixing device comprises a connecting column, bottom connecting plates, an upper connecting plate, a tail clamp, a first screwing ring, a middle connecting pipe, a rotatable and rotatable suspension seat structure, a slidable clamping magnetic suction fixing device structure, a rotatable sleeved protective net structure, an inverted L-shaped rotating rod, a second screwing ring, a sponge ring, an outer protective sleeve ring and an insertion sleeve plate, wherein the connecting column is inserted in the lower part between the bottom connecting plates; the bottom connecting plate is respectively connected with the lower part of the front surface and the lower part of the rear surface of the upper connecting plate in a bolted mode; the right side of the tail clamp is connected to the middle position of the left side of the first screwing ring through a bolt; the left side of the middle connecting pipe is glued at the middle position of the right side of the first screwing ring; the rotatable rotary suspension seat structure is arranged at the upper end of the upper connecting plate; the slidable clamping magnetic suction fixer structure is arranged on the left side of the outer wall of the tail clamp; the rotatable sleeved protective net pipe structure is arranged on the outer wall of the middle connecting pipe; the lower end of the inverted L-shaped rotating rod is respectively coupled to the left side and the right side of the upper end of the upper connecting plate; the lower end of the middle connecting pipe is glued at the middle position of the upper end of the second screwing ring; the sponge ring is glued at the lower end of the second screwing ring; the upper end of the outer protective sleeve ring is glued to the middle position of the top end of the second screwing ring; the upper end of the insertion sleeve plate is glued to the top end of the inner part of the outer protective sleeve ring; the rotatable rotary suspension seat structure comprises a fixed seat, a U-shaped connecting seat, a bolt and a nut, a supporting rod, an inserting seat and an inserting hole, wherein the U-shaped connecting seat is respectively connected to the left side and the right side of the lower end of the fixed seat through bolts; a bolt in the bolt nut penetrates through a threaded connection nut at the middle position inside the lower side of the U-shaped connecting seat; the upper end of the supporting rod is inserted in the middle position inside the lower side of the U-shaped connecting seat; the lower end of the supporting rod is respectively bolted at the middle positions of the left side and the right side of the upper end of the socket; the plug hole is arranged in the middle of the inner part of the plug seat.
Preferably, the slidable clamping magnetic attraction fixer structure comprises a magnetic attraction fixer, a sleeve pipe, a square-head bolt, a jacking plate and a deep groove ball bearing, wherein the sleeve pipe is connected to the middle position of the front surface of the magnetic attraction fixer through the bolt; the square-head bolts are respectively in threaded connection with the middle positions of the left side and the right side of the front surface of the sleeve pipe; the deep groove ball bearings are respectively embedded in the middle positions of the left side and the right side of the front surface of the jacking plate; the rear ends of the square head bolts are respectively inserted into the inner rings of the deep groove ball bearings.
Preferably, the rotatable sleeved protective screening pipe structure comprises a sleeved ring, a puller bolt, a silica gel ring, a net pipe and a rubber layer, wherein the puller bolt is respectively in threaded connection with the middle position of the front surface of the sleeved ring; the silica gel ring is respectively glued to the left side of the sleeve joint ring and the lower end of the sleeve joint ring; one end of the net pipe is glued at the middle position of the right side of the splicing ring; the other end of the net pipe is glued at the middle position of the upper end of the splicing ring; the rubber layer is glued on the inner wall of the net tube.
Preferably, the sponge ring is arranged in the middle of the outer wall of the outer protective sleeve ring; the bottom connecting plate is arranged at the lower part of the outer wall of the tail clamp; the upper connecting plate is respectively arranged on the upper part of the outer wall of the tail clamp.
Preferably, the lower ends of the supporting rods are respectively arranged at the left side and the right side of the upper end of the inserting hole; and the bolt in the bolt nut penetrates through the middle position of the upper side inside the supporting rod.
Preferably, the upper end of the upper connecting plate penetrates through the inserting holes respectively; the upper end of the inverted L-shaped rotating rod penetrates through the plug hole respectively and is hung on the left side and the right side of the upper end of the plug seat.
Preferably, the jacking plate is arranged in the middle of the inner wall of the front surface of the sleeve pipe; the outer wall of the rear end of the square head bolt is in interference fit with the inner ring of the deep groove ball bearing.
Preferably, the sleeve is sleeved on the outer wall of the left side of the tail clamp; the middle positions of the left sides of the front surfaces of the jacking plate and the tail clamp are in contact arrangement.
Preferably, the network management is arranged between the socket rings; the socket ring is a PVC ring.
Preferably, the sleeve ring and the net pipe are sleeved on the outer wall of the middle connecting pipe; the sleeve rings are respectively arranged on the left side of the outer wall of the middle connecting pipe and the lower part of the outer wall; the puller bolt is respectively contacted with the outer wall of the middle connecting pipe.
Compared with the prior art, the beneficial effects of the utility model are that:
1. the utility model discloses in, the fixer is inhaled to magnetism, the bell and spigot joint pipe, the square head bolt, the setting that top tie plate and tail pressed from both sides is favorable to carrying out tail clamp fixing work through magnetism the fixer at the in-process that uses, conveniently carries out tail clamp fixed stay work at work.
2. The utility model discloses in, fixing base, U type connecting seat, bolt and nut, the bracing piece, the setting of socket and spliced eye is favorable to adjusting the angle of bracing piece and socket at the in-process that uses, conveniently installs the work at fixed in-process.
3. The utility model discloses in, the fishplate bar, the type of falling L dwang, the setting of bayonet socket and spliced eye is favorable to running through the spliced eye to the type of falling L dwang at the in-process that uses, then rotates the type of falling L dwang, makes the upper end of the type of falling L dwang articulate in the left and right sides of bayonet socket, conveniently installs at the in-process that uses.
4. The utility model discloses in, cup joint the ring, the silica gel circle, the setting on network management and rubber layer is favorable to taking over through network management and rubber layer centering at the in-process that uses and carrying out protection work, prevents to take over and receive damage influence work at the in-process that uses.
5. The utility model discloses in, the fixer is inhaled to magnetism, the bell and spigot joint, the square head bolt, the setting of top tight board and deep groove ball bearing is favorable to promoting the tight board in the in-process rotation square head bolt that uses and removes in top, then make top tight board and bell and spigot joint press from both sides to the tail and carry out centre gripping work, conveniently carry out tail clamp fixed work at work.
6. The utility model discloses in, cup joint the ring, the puller bolt, the network management, first wrong ring that connects, well takeover and second are twisted the setting that connects the ring, are favorable to carrying out network management dismantlement work at the in-process that uses, the convenience is installed and is changed work at the in-process of protection.
7. The utility model discloses in, the fixer is inhaled to magnetism, the bell and spigot joint pipe, the square head bolt, the setting that top grip block and deep groove ball bearing and tail pressed from both sides is favorable to carrying out magnetism at the in-process that uses and inhale the fixer installation and dismantle work, conveniently carries out tail and presss from both sides fixed work.
Drawings
Fig. 1 is a schematic structural diagram of the present invention.
Fig. 2 is a schematic structural view of the rotatable suspension base structure of the present invention.
Fig. 3 is a schematic structural view of the slidable magnetic clamping fixer of the present invention.
Fig. 4 is a schematic structural diagram of the rotatable sleeved protective screening pipe structure of the present invention.
Fig. 5 is a side view of the slidable magnetic clamping fixer of the present invention.
In the figure:
1. connecting columns; 2. an underpinning plate; 3. an upper connecting plate; 4. a tail clip; 5. a first screw-on ring; 6. a middle connecting pipe; 7. the rotary suspension seat structure can be rotated; 71. a fixed seat; 72. a U-shaped connecting seat; 73. a bolt and a nut; 74. a support bar; 75. a socket; 76. inserting holes; 8. a slidable clamping magnetic fixer structure; 81. a magnetic attraction fixer; 82. sleeving a pipe; 83. a square head bolt; 84. a jacking plate; 85. a deep groove ball bearing; 9. a protective net pipe structure can be rotatably sleeved; 91. a sleeving connection ring; 92. jacking the bolt; 93. a silica gel ring; 94. network management; 95. a rubber layer; 10. an inverted L-shaped rotating rod; 11. a second screw-on ring; 12. a sponge ring; 13. an outer jacket ring; 14. the sleeve plate is inserted.
Detailed Description
The utility model is described in detail with reference to the accompanying drawings, as shown in fig. 1 and fig. 2, a novel aviation connector tail clamp fixing device comprises a connecting column 1, a bottom connecting plate 2, a top connecting plate 3, a tail clamp 4, a first screwing ring 5, a middle connecting pipe 6, a rotatable and rotatable suspension seat structure 7, a slidable clamping magnetic suction fixer structure 8, a rotatable sleeved protective screening pipe structure 9, an inverted L-shaped rotating rod 10, a second screwing ring 11, a sponge ring 12, an outer protective screening ring 13 and an insertion screening plate 14, wherein the connecting column 1 is inserted in the lower part between the bottom connecting plates 2; the bottom connecting plate 2 is respectively connected with the lower part of the front surface and the lower part of the rear surface of the upper connecting plate 3 in a bolted mode; the right side of the tail clamp 4 is in bolted connection with the middle position of the left side of the first screwing ring 5; the left side of the middle connecting pipe 6 is glued at the middle position of the right side of the first screwing ring 5; the rotatable rotary suspension seat structure 7 is arranged at the upper end of the upper connecting plate 3; the slidable clamping magnetic suction fixer structure 8 is arranged on the left side of the outer wall of the tail clamp 4; the rotatable sleeved protective screening pipe structure 9 is arranged on the outer wall of the middle connecting pipe 6; the lower end of the inverted L-shaped rotating rod 10 is respectively connected with the left side and the right side of the upper end of the upper connecting plate 3 in a shaft mode; the lower end of the middle connecting pipe 6 is glued at the middle position of the upper end of the second screwing ring 11; the sponge ring 12 is glued at the lower end of the second screwing ring 11; the upper end of the outer protective sleeve ring 13 is glued to the middle position of the top end inside the second screwing ring 11; the upper end of the insert sleeve plate 14 is glued to the top end of the inner part of the outer protective sleeve ring 13; the rotatable and rotatable suspension seat structure 7 comprises a fixed seat 71, a U-shaped connecting seat 72, a bolt and a nut 73, a support rod 74, an inserting seat 75 and an inserting hole 76, wherein the U-shaped connecting seat 72 is respectively bolted at the left side and the right side of the lower end of the fixed seat 71; the bolt in the bolt nut 73 penetrates through a threaded connection nut at the middle position inside the lower side of the U-shaped connecting seat 72; the upper end of the supporting rod 74 is inserted in the middle position inside the lower side of the U-shaped connecting seat 72; the lower end of the supporting rod 74 is respectively bolted at the middle positions of the left side and the right side of the upper end of the socket 75; the plug hole 76 is arranged in the middle of the inside of the plug seat 75; fix fixing base 71 in suitable position when using, then will insert the lagging 14 fixed, after fixing to insert the lagging 14, rotate the type of falling L dwang 10, then make the type of falling L dwang 10 run through spliced eye 76, at the type of rotating the type of falling L dwang 10, the upper end that makes the type of falling L dwang 10 articulates respectively in the left and right sides inner wall of spliced eye 76 and articulates in the upper end left and right sides of bayonet socket 75, conveniently carry out tail clamp 4 fixed work at the in-process that uses.
In this embodiment, referring to fig. 3, the slidable clamping magnetic attraction fixture structure 8 includes a magnetic attraction fixture 81, a sleeve 82, a square-head bolt 83, a tightening plate 84 and a deep groove ball bearing 85, wherein the sleeve 82 is bolted to the middle position of the front surface of the magnetic attraction fixture 81; the square-head bolts 83 are respectively in threaded connection with the middle positions of the left side and the right side of the front surface of the sleeve pipe 82; the deep groove ball bearings 85 are respectively embedded in the middle positions of the left side and the right side of the front surface of the jacking plate 84; the rear ends of the square head bolts 83 are respectively inserted into the inner rings of the deep groove ball bearings 85; then use the socket pipe 82 to cup joint in the outer wall left side that the tail pressed from both sides 4, conveniently install work at fixed in-process, then rotate the socket pipe 82, make the suitable position of magnetism fixer 81 installation, at rotatory square head bolt 83, promote the tight board 84 in top and remove, make the tight board 84 in top press from both sides 4 centre gripping in the inside of socket pipe 82 with the tail, conveniently carry out the fixed work of tail clamp 4 in work.
In this embodiment, as shown in fig. 4, the rotatable sleeved protective screening structure 9 includes a sleeved ring 91, a tightening bolt 92, a silicone ring 93, a mesh tube 94 and a rubber layer 95, wherein the tightening bolt 92 is respectively screwed in the middle of the front surface of the sleeved ring 91; the silica gel ring 93 is respectively glued to the left side of the socket ring 91 and the lower end of the socket ring 91; one end of the net pipe 94 is glued at the middle position of the right side of the socket ring 91; the other end of the mesh tube 94 is glued at the middle position of the upper end of the socket ring 91; the rubber layer 95 is glued on the inner wall of the mesh tube 94; in the using process, the sleeve ring 91 and the network pipe 94 are sleeved on the outer wall of the middle connecting pipe 6, so that the sleeve ring 91 is respectively fixed at two ends of the middle connecting pipe 6, the middle connecting pipe 6 is protected through the network pipe 94 and the rubber layer 95, the connecting pipe 6 is prevented from being damaged and affecting work in the using process, and the protection function is increased.
In this embodiment, specifically, the sponge ring 12 is disposed in the middle of the outer wall of the outer sheath ring 13; the bottom connecting plate 2 is arranged at the lower part of the outer wall of the tail clamp 4; the upper connecting plate 3 is respectively arranged on the upper part of the outer wall of the tail clamp 4.
In this embodiment, specifically, the lower ends of the support rods 74 are respectively disposed at the left and right sides of the upper end of the insertion hole 76; the bolt of the bolt and nut 73 penetrates through the middle position of the upper inner part of the support rod 74.
In this embodiment, specifically, the upper ends of the upper connecting plates 3 respectively penetrate through the inserting holes 76; the upper end of the inverted-L-shaped rotating rod 10 penetrates through the insertion holes 76 respectively and is hung on the left and right sides of the upper end of the insertion seat 75.
In this embodiment, specifically, the tightening plate 84 is disposed at the middle position of the inner wall of the front surface of the ferrule 82; the outer wall of the rear end of the square head bolt 83 is in interference fit with the inner ring of the deep groove ball bearing 85.
In this embodiment, specifically, the sleeve 82 is sleeved on the outer wall of the left side of the tail clamp 4; the jacking plate 84 is arranged in contact with the middle position on the left side of the front surface of the tail clamp 4.
In this embodiment, specifically, the network management pipe 94 is disposed between the socket rings 91; the socket ring 91 is a PVC ring.
In this embodiment, specifically, the socket ring 91 and the network pipe 94 are sleeved on the outer wall of the middle adapter tube 6; the sleeve ring 91 is respectively arranged on the left side of the outer wall of the middle connecting pipe 6 and the lower part of the outer wall; the puller bolts 92 are respectively arranged in contact with the outer wall of the middle adapter 6.
Principle of operation
In the utility model, when in use, the fixed seat 71 is fixed at a proper position, then the inserting sleeve plate 14 is fixed, after the inserting sleeve plate 14 is fixed, the inverted L-shaped rotating rod 10 is rotated, then the inverted L-shaped rotating rod 10 penetrates through the inserting hole 76, when the inverted L-shaped rotating rod 10 is rotated, the upper end of the inverted L-shaped rotating rod 10 is respectively hung on the inner walls of the left side and the right side of the inserting hole 76 and hung on the left side and the right side of the upper end of the inserting seat 75, the tail clamp 4 is conveniently fixed in the using process, then the sleeve 82 is sleeved on the left side of the outer wall of the tail clamp 4, the installation work is conveniently carried out in the fixing process, then the sleeve 82 is rotated, the proper position for installing the magnetic absorption fixer 81 is enabled, the rotating square head bolt 83 pushes the jacking plate 84 to move, the jacking plate 84 clamps the tail clamp 4 in the sleeve 82, the tail clamp 4 is conveniently fixed in the work, in the using process, the sleeve ring 91 and the network pipe 94 are sleeved on the outer wall of the middle connecting pipe 6, so that the sleeve ring 91 is respectively fixed at two ends of the middle connecting pipe 6, the middle connecting pipe 6 is protected through the network pipe 94 and the rubber layer 95, the connecting pipe 6 is prevented from being damaged and affecting work in the using process, and the protection function is increased.
Utilize technical scheme, or technical personnel in the field are in the utility model discloses under technical scheme's the inspiration, design similar technical scheme, and reach above-mentioned technological effect, all fall into the utility model discloses a protection scope.

Claims (10)

1. The novel aviation connector tail clamp fixing device is characterized by comprising connecting columns (1), bottom connecting plates (2), upper connecting plates (3), tail clamps (4), first screwing rings (5), middle connecting pipes (6), rotatable and rotatable suspension seat structures (7), slidable clamping magnetic suction fixing device structures (8), rotatable sleeved protective net structures (9), inverted L-shaped rotating rods (10), second screwing rings (11), sponge rings (12), outer protective sleeve rings (13) and inserting sleeve plates (14), wherein the connecting columns (1) are inserted in the lower parts between the bottom connecting plates (2); the bottom connecting plate (2) is respectively connected with the lower part of the front surface and the lower part of the rear surface of the upper connecting plate (3) through bolts; the right side of the tail clamp (4) is in bolted connection with the middle position of the left side of the first screwing ring (5); the left side of the middle connecting pipe (6) is glued at the middle position of the right side of the first screwing ring (5); the rotatable rotary suspension seat structure (7) is arranged at the upper end of the upper connecting plate (3); the slidable clamping magnetic suction fixer structure (8) is arranged on the left side of the outer wall of the tail clamp (4); the rotatable sleeved protective screening pipe structure (9) is arranged on the outer wall of the middle connecting pipe (6); the lower end of the inverted L-shaped rotating rod (10) is respectively connected with the left side and the right side of the upper end of the upper connecting plate (3) in a shaft manner; the lower end of the middle connecting pipe (6) is glued at the middle position of the upper end of the second screwing ring (11); the sponge ring (12) is glued at the lower end of the second screwing ring (11); the upper end of the outer protective sleeve ring (13) is glued to the middle position of the top end of the second screwing ring (11); the upper end of the insertion sleeve plate (14) is glued to the top end of the inner part of the outer protective sleeve ring (13); the rotatable rotary suspension seat structure (7) comprises a fixed seat (71), a U-shaped connecting seat (72), a bolt and nut (73), a supporting rod (74), an inserting seat (75) and an inserting hole (76), wherein the U-shaped connecting seat (72) is respectively connected to the left side and the right side of the lower end of the fixed seat (71) through bolts; a bolt in the bolt nut (73) penetrates through a threaded connection nut at the middle position inside the lower side of the U-shaped connecting seat (72); the upper end of the supporting rod (74) is inserted in the middle of the lower side of the U-shaped connecting seat (72); the lower end of the supporting rod (74) is respectively bolted at the middle positions of the left side and the right side of the upper end of the plug socket (75); the plug hole (76) is arranged in the middle of the inner part of the plug seat (75).
2. The novel aviation connector tail clamp fixing device as claimed in claim 1, wherein the slidable clamping magnetic suction fixer structure (8) comprises a magnetic suction fixer (81), a sleeve pipe (82), a square head bolt (83), a jacking plate (84) and a deep groove ball bearing (85), wherein the sleeve pipe (82) is bolted to the middle position of the front surface of the magnetic suction fixer (81); the square-head bolts (83) are respectively in threaded connection with the middle positions of the left side and the right side of the front surface of the sleeve pipe (82); the deep groove ball bearings (85) are respectively embedded in the middle positions of the left side and the right side of the front surface of the tightening plate (84); the rear ends of the square head bolts (83) are respectively inserted into the inner rings of the deep groove ball bearings (85).
3. The novel aviation connector tail clamp fixing device is characterized in that the rotatable sleeved protective screen structure (9) comprises a sleeved ring (91), tightening bolts (92), a silica gel ring (93), a mesh tube (94) and a rubber layer (95), wherein the tightening bolts (92) are respectively in threaded connection with the middle position of the front surface of the sleeved ring (91); the silica gel ring (93) is respectively glued to the left side of the sleeving ring (91) and the lower end of the sleeving ring (91); one end of the net pipe (94) is glued at the middle position of the right side of the sleeve ring (91); the other end of the net pipe (94) is glued at the middle position of the upper end of the splicing ring (91); the rubber layer (95) is glued on the inner wall of the mesh pipe (94).
4. The novel aviation connector tail clamp fixing device as claimed in claim 1, wherein the sponge ring (12) is arranged in the middle of the outer wall of the outer protective sleeve ring (13); the bottom connecting plate (2) is arranged at the lower part of the outer wall of the tail clamp (4); the upper connecting plate (3) is respectively arranged on the upper part of the outer wall of the tail clamp (4).
5. The aircraft connector tail clip fixing device as claimed in claim 1, wherein the lower ends of the support rods (74) are respectively arranged at the left and right sides of the upper end of the insertion hole (76); the bolt of the bolt nut (73) penetrates through the middle position of the upper inner part of the support rod (74).
6. The aircraft connector tail clip fixing device as claimed in claim 1, wherein the upper end of the upper connecting plate (3) is respectively penetrated through a plug hole (76); the upper end of the inverted L-shaped rotating rod (10) penetrates through the plug hole (76) respectively and is hung on the left side and the right side of the upper end of the plug seat (75).
7. The aircraft connector tail clip attachment device of claim 2, wherein the puller plate (84) is disposed at a position intermediate the front surface of the ferrule (82); the outer wall of the rear end of the square head bolt (83) is in interference fit with the inner ring of the deep groove ball bearing (85).
8. The novel aviation connector tail clamp fixing device as claimed in claim 2, wherein the sleeve pipe (82) is sleeved on the outer wall of the left side of the tail clamp (4); the middle positions of the left sides of the front surfaces of the jacking plate (84) and the tail clamp (4) are arranged in a contact manner.
9. The new aft clip attachment arrangement of claim 1, wherein the mesh tube (94) is disposed between the ferrules (91); the sleeving ring (91) is a PVC ring.
10. The novel aviation connector tail clamp fixing device as claimed in claim 3, wherein the sleeve ring (91) and the net pipe (94) are sleeved on the outer wall of the middle adapter pipe (6); the sleeving connection ring (91) is respectively arranged on the left side of the outer wall of the middle connection pipe (6) and the lower part of the outer wall; the puller bolt (92) is respectively contacted with the outer wall of the middle connecting pipe (6).
CN202021847624.4U 2020-08-28 2020-08-28 Novel aviation connector tail clamp fixing device Active CN212695388U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202021847624.4U CN212695388U (en) 2020-08-28 2020-08-28 Novel aviation connector tail clamp fixing device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202021847624.4U CN212695388U (en) 2020-08-28 2020-08-28 Novel aviation connector tail clamp fixing device

Publications (1)

Publication Number Publication Date
CN212695388U true CN212695388U (en) 2021-03-12

Family

ID=74903557

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202021847624.4U Active CN212695388U (en) 2020-08-28 2020-08-28 Novel aviation connector tail clamp fixing device

Country Status (1)

Country Link
CN (1) CN212695388U (en)

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