CN104607556A - Aviation plug assembling machine - Google Patents
Aviation plug assembling machine Download PDFInfo
- Publication number
- CN104607556A CN104607556A CN201510055871.8A CN201510055871A CN104607556A CN 104607556 A CN104607556 A CN 104607556A CN 201510055871 A CN201510055871 A CN 201510055871A CN 104607556 A CN104607556 A CN 104607556A
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- CN
- China
- Prior art keywords
- body base
- main body
- aviation plug
- bolster
- base
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Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21D—WORKING OR PROCESSING OF SHEET METAL OR METAL TUBES, RODS OR PROFILES WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21D39/00—Application of procedures in order to connect objects or parts, e.g. coating with sheet metal otherwise than by plating; Tube expanders
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Portable Nailing Machines And Staplers (AREA)
- Manufacturing Of Electrical Connectors (AREA)
- Footwear And Its Accessory, Manufacturing Method And Apparatuses (AREA)
Abstract
The invention discloses an aviation plug assembling machine. The aviation plug assembling machine comprises a mold assembly and a body base. The mold assembly comprises an upper mold base, a lower mold base, an upper mold fixing plate, an upper base plate, a lower mold fixing plate and a lower base plate, wherein the upper mold base, the lower mold base, the upper mold fixing plate, the upper base plate, the lower mold fixing plate and the lower base plate are connected. A first spring is installed between the upper mold base and the lower mold base, a second spring is installed between the upper mold fixing plate and the upper mold base, a first mold cavity and a second mold cavity are formed in the upper mold base and the lower mold base respectively, and stamping heads are installed in the upper base plate, penetrate through the upper mold fixing plate and extend into the first mold cavity in the upper mold base. The body base comprises a channel, a first sliding rail and a second sliding rail. The mold assembly is arranged on the first sliding rail, and a first power device and a second power device are arranged on the left side and the right side of the body base. A valve device used for closing the channel and a discharging device used for ejecting out an assembled aviation plug terminal assembly are installed at the upper end and the lower end of the body base respectively. A discharging hole is formed in the upper end of the body base. The aviation plug assembling machine is safe, easy and convenient to operate, good in assembling quality and high in working efficiency.
Description
Technical field:
The present invention relates to mounting equipment product technical field, refer in particular to a kind of easy and simple to handle, safety, assembling quality is good, and the aviation plug kludge that operating efficiency is high.
Background technology:
Aviation plug is a kind of quick plug be used in aviation, current aviation plug terminal uses the punching press of hand hydraulic cutting presser to fix by artificial, but the deficiency had by the punching press of hand hydraulic cutting presser is comprised: the aviation plug terminal poor quality that punching press is formed, there is the phenomenon loosened, in addition, hand labor intensity is large, there is security risk, and operating efficiency is low.
Summary of the invention:
The object of the invention is to overcome the deficiencies in the prior art, provide a kind of easy and simple to handle, safety, assembling quality is good, and the aviation plug kludge that operating efficiency is high.
In order to solve the problems of the technologies described above, present invention employs following technical proposals: this aviation plug kludge comprises: a die assembly, it comprises: a upper bolster, be installed on upper bolster and side and with the die shoe of upper bolster adaptation, be installed on upper mould fixed plate and the upper padding plate of upper bolster opposite side, be installed on the counterdie fixed head outside die shoe and lower bolster, wherein, first spring is installed between upper bolster and die shoe, second spring is installed between upper mould fixed plate and upper bolster, be respectively arranged with in described upper bolster and die shoe and cooperatively interact and supply aviation plug terminal assemblies to place first, second die cavity, at least two staking punch are installed in described upper padding plate, this staking punch passes upper mould fixed plate successively and stretches in the first die cavity in upper bolster, one main body base, be provided with the passage that passes through for described die assembly in this main body base and be positioned at main body base front and back end and first, second slide rail docked with this passage, described die assembly is positioned on the first slide rail, this main body base left and right sides is provided with first, second power set, and first, second drive rod in these first, second power set all stretches in described passage, the upper and lower two ends of described main body base are separately installed with one for closing the valving of described passage and the drawing mechanism for ejecting the aviation plug terminal assemblies assembled, wherein, this main body base upper end in the side of valving be provided with one with the discharge opening of described channel connection, this discharge opening is corresponding with drawing mechanism.
Furthermore, in technique scheme, described upper bolster end is also provided with one handle.
Furthermore, in technique scheme, described die shoe, upper mould fixed plate, upper padding plate, counterdie fixed head and lower bolster lower surface flush, and described upper bolster lower end protrudes from outside the lower surface of die shoe and upper mould fixed plate, upper padding plate, counterdie fixed head and lower bolster, and dock with the chute on described first slide rail.
Furthermore, in technique scheme, described upper padding plate is also provided with short contour cover, this short contour cover stretches in upper mould fixed plate; Described lower bolster is also provided with long contour cover, the contour cover of this length stretches in counterdie fixed head.
Furthermore, in technique scheme, described main body base lower end is provided with low oblique riser and the oblique riser of height, makes main body base inclination 15-20 ° along the longitudinal direction, inclination 5-10 ° in left-right direction.
Furthermore, in technique scheme, first, second power set described are cylinder assembly.
Furthermore, in technique scheme, described valving comprises: be installed on the first cylinder of main body base upper end by some first pillars and be installed on the valve of piston rod end in the first cylinder, this valve stretches into the exit of passage in main body base.
Furthermore, in technique scheme, described drawing mechanism comprises: by some second pillars be installed on main body base lower end the second cylinder, be installed on piston rod end in the second cylinder needle plate, be installed on thimble in needle plate and thimble guide pillar, described upper bolster upwards offers through first die cavity and the pin hole position passed for thimble along its lower end.
Furthermore, in technique scheme, described main body base is provided with a discharge cover, this discharge cover port docks with described discharge opening.
After adopting technique scheme, the present invention has following beneficial effect compared with prior art: when the present invention uses, first of upper bolster and die shoe in die assembly is positioned over by needing the scattered aviation plug terminal assemblies of assembling, in second die cavity, subsequently this die assembly is positioned over after on the first slide rail on main body base and unclamps die assembly, this die assembly under its Action of Gravity Field along the first slide rail landing in the passage of main body base, now, described valving work, the outlet of passage in main body base is lived by valve blockage, die assembly is made to rest in the passage of main body base, subsequently first, in second power set first, second drive rod is respectively to the upper padding plate in die assembly and lower bolster, die assembly is made to be clamped, wherein, staking punch in die assembly is bored a hole to aviation plug terminal assemblies, and form riveted joint, scattered aviation plug terminal assemblies is made to form an aviation plug terminal assemblies be fixed together.First, second drive rod subsequently in first, second power set resets, and the thimble in drawing mechanism penetrates in die assembly, and ejects aviation plug terminal assemblies, makes aviation plug terminal assemblies eject from discharge opening, and along discharge cover discharging.Above-mentioned whole operating process is very simple, and there is not security risk, and its hand labor intensity is low, so that operating efficiency is high, and assembling effect is fabulous, and has the high market competitiveness.
Accompanying drawing illustrates:
Fig. 1 is stereogram of the present invention;
Fig. 2 is the stereogram of die assembly in the present invention;
Fig. 3 is three-dimensional exploded view of the present invention;
Fig. 4 is the stereogram of drawing mechanism in the present invention;
Fig. 5 is the stereogram having assembled rear aviation plug terminal assemblies.
Detailed description of the invention:
Below in conjunction with specific embodiments and the drawings, the present invention is further described.
See shown in Fig. 1-4, be a kind of aviation plug kludge, it comprises: a die assembly 1, main body base 2, be installed on first, second power set 3,4 on this main body base 2 and valving 6 and drawing mechanism 5.
Described die assembly 1 comprises: a upper bolster 11, be installed on upper bolster 11 with side and with the die shoe 12 of upper bolster 11 adaptation, be installed on upper mould fixed plate 13 and the upper padding plate 14 of upper bolster 11 opposite side, be installed on the counterdie fixed head 15 outside die shoe 12 and lower bolster 16, wherein, first spring is installed between upper bolster 11 and die shoe 12, second spring is installed between upper mould fixed plate 13 and upper bolster 11, be respectively arranged with in described upper bolster 11 and die shoe 12 and cooperatively interact and supply aviation plug terminal assemblies to place first, second die cavity 111, 121, in described upper padding plate 14, at least two staking punch 141 are installed, this staking punch 141 passes upper mould fixed plate 13 successively and stretches in the first die cavity 111 in upper bolster 11.Described upper padding plate 14 is also provided with short contour cover 142, and this short contour cover 142 stretches in upper mould fixed plate 13; Described lower bolster 16 is also provided with long contour cover 161, the contour cover 161 of this length stretches in counterdie fixed head 15.
Described upper bolster 11 end is also provided with one handle 112, so that people operates use.
Described die shoe 12, upper mould fixed plate 13, upper padding plate 14, counterdie fixed head 15 and lower bolster 16 lower surface flush, and described upper bolster 11 lower end protrudes from outside the lower surface of die shoe 12 and upper mould fixed plate 13, upper padding plate 14, counterdie fixed head 15 and lower bolster 16, and dock with the chute on described first slide rail 22.
Be provided with the passage 21 that passes through for described die assembly 1 in described main body base 2 and be positioned at main body base 2 front and back end and first, second slide rail 22,23 docked with this passage 21, described die assembly 1 is positioned on the first slide rail 22, this main body base 2 left and right sides is provided with first, second power set 3,4, and first, second drive rod 31,41 in these first, second power set 3,4 all stretches in described passage 21; Described main body base about 2 two ends are separately installed with one for closing the valving 6 of described passage 21 and the drawing mechanism 5 for ejecting the aviation plug terminal assemblies assembled, wherein, this main body base 2 upper end is provided with a discharge opening 24 be communicated with described passage 21 in the side of valving 6, and this discharge opening 24 is corresponding with drawing mechanism 5.
Described main body base 2 lower end is provided with low oblique riser 25 and the oblique riser 26 of height, makes main body base 2 inclination 15-20 ° along the longitudinal direction, inclination 5-10 ° in left-right direction, and the main body base 2 of this structure can make die assembly 1 landing more smooth and easy.
First, second power set 3,4 described are cylinder assembly.
Described valving 6 comprises: be installed on the first cylinder 62 of main body base 2 upper end by some first pillars 61 and be installed on the valve 63 of piston rod end in the first cylinder 62, this valve 63 stretches into the exit of passage in main body base 2.
Described drawing mechanism 5 comprises: by some second pillars 51 be installed on main body base 2 lower end the second cylinder 52, be installed on piston rod end in the second cylinder 52 needle plate 53, be installed on thimble 54 in needle plate 53 and thimble guide pillar 55, described upper bolster 11 upwards offers through first die cavity 111 and the pin hole position passed for thimble 54 along its lower end.
Described main body base 2 is provided with a discharge cover (figure does not look), this discharge cover port docks with described discharge opening 24.
When the present invention uses, first of upper bolster 11 and die shoe 12 in die assembly 1 is positioned over by needing the scattered aviation plug terminal assemblies of assembling, second die cavity 111, in 121, subsequently this die assembly 1 is positioned over after on the first slide rail 22 on main body base 2 and unclamps die assembly 1, this die assembly 1 under its Action of Gravity Field along the first slide rail 22 landing in the passage 21 of main body base 2, now, described valving 4 works, by the outlet of passage 21 in the clogging main body base 2 of valve 43, die assembly 1 is made to rest in the passage 21 of main body base 2, subsequently first, second power set 3, in 4 first, second drive rod 31, 41 respectively to the upper padding plate 14 in die assembly 1 and lower bolster 16, die assembly 1 is made to be clamped, wherein, the 141 pairs of aviation plug terminal assemblies perforation of staking punch in die assembly 1, and form riveted joint, scattered aviation plug terminal assemblies is made to form an aviation plug terminal assemblies 100 be fixed together, as shown in Figure 5.First, second drive rod 31,41 subsequently in first, second power set 3,4 resets, and the thimble 54 in drawing mechanism 5 penetrates in die assembly 1, and eject aviation plug terminal assemblies 100, make aviation plug terminal assemblies 100 eject from discharge opening 24, and along discharge cover discharging.Above-mentioned whole operating process is very simple, and there is not security risk, and its hand labor intensity is low, so that operating efficiency is high, and assembling effect is fabulous, and has the high market competitiveness.
Certainly, the foregoing is only specific embodiments of the invention, be not limit the scope of the present invention, all equivalences done according to structure, feature and principle described in the present patent application the scope of the claims change or modify, and all should be included in the present patent application the scope of the claims.
Claims (9)
1. an aviation plug kludge, is characterized in that, comprising:
One die assembly (1), it comprises: a upper bolster (11), be installed on upper bolster (11) and side and the die shoe (12) adaptive with upper bolster (11), be installed on upper mould fixed plate (13) and the upper padding plate (14) of upper bolster (11) opposite side, be installed on counterdie fixed head (15) and the lower bolster (16) in die shoe (12) outside, wherein, between upper bolster (11) and die shoe (12), the first spring is installed, between upper mould fixed plate (13) and upper bolster (11), the second spring is installed, be respectively arranged with in described upper bolster (11) and die shoe (12) and cooperatively interact and supply aviation plug terminal assemblies to place first, second die cavity (111, 121), at least two staking punch (141) are installed in described upper padding plate (14), this staking punch (141) passes upper mould fixed plate (13) successively and stretches in the first die cavity (111) in upper bolster (11),
One main body base (2), be provided with for described die assembly (1) passage (21) that passes through in this main body base (2) and be positioned at main body base (2) front and back end and dock with this passage (21) first, second slide rail (22, 23), described die assembly (1) is positioned on the first slide rail (22), this main body base (2) left and right sides is provided with first, second power set (3, 4), this is first years old, second power set (3, 4) first in, second drive rod (31, 41) all stretch in described passage (21), described main body base (2) is separately installed with one for closing the valving (6) of described passage (21) and the drawing mechanism (5) for ejecting the aviation plug terminal assemblies assembled in two ends up and down, wherein, this main body base (2) upper end is provided with a discharge opening (24) be communicated with described passage (21) in the side of valving (6), and this discharge opening (24) is corresponding with drawing mechanism (5).
2. a kind of aviation plug kludge according to claim 1, is characterized in that: described upper bolster (11) end is also provided with one handle (112).
3. a kind of aviation plug kludge according to claim 1, it is characterized in that: described die shoe (12), upper mould fixed plate (13), upper padding plate (14), counterdie fixed head (15) and lower bolster (16) lower surface flush, and described upper bolster (11) lower end protrudes from outside the lower surface of die shoe (12) and upper mould fixed plate (13), upper padding plate (14), counterdie fixed head (15) and lower bolster (16), and dock with the chute on described first slide rail (22).
4. a kind of aviation plug kludge according to claim 1, it is characterized in that: described upper padding plate (14) is also provided with short contour cover (142), this short contour cover (142) is stretched in upper mould fixed plate (13); Described lower bolster (16) is also provided with long contour cover (161), the contour cover of this length (161) stretches in counterdie fixed head (15).
5. a kind of aviation plug kludge according to claim 1, it is characterized in that: described main body base (2) lower end is provided with low oblique riser (25) and the oblique riser of height (26), make main body base (2) inclination 15-20 ° along the longitudinal direction, inclination 5-10 ° in left-right direction.
6. a kind of aviation plug kludge according to claim 1, is characterized in that: first, second power set described (3,4) are cylinder assembly.
7. a kind of aviation plug kludge according to claim 1, it is characterized in that: described valving (6) comprising: be installed on first cylinder (62) of main body base (2) upper end by some first pillars (61) and be installed on the valve (63) of the middle piston rod end of the first cylinder (62), this valve (63) stretches into the exit of passage in main body base (2).
8. a kind of aviation plug kludge according to claim 1, it is characterized in that: described drawing mechanism (5) comprising: by some second pillars (51) be installed on main body base (2) lower end the second cylinder (52), be installed on piston rod end in the second cylinder (52) needle plate (53), be installed on thimble (54) in needle plate (53) and thimble guide pillar (55), described upper bolster (11) upwards offers through first die cavity (111) and the pin hole position passed for thimble (54) along its lower end.
9. a kind of aviation plug kludge according to claim 1, it is characterized in that: (2) are provided with a discharge cover to described main body base, this discharge cover port docks with described discharge opening (24).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510055871.8A CN104607556B (en) | 2015-02-03 | 2015-02-03 | A kind of aviation plug kludge |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510055871.8A CN104607556B (en) | 2015-02-03 | 2015-02-03 | A kind of aviation plug kludge |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN104607556A true CN104607556A (en) | 2015-05-13 |
| CN104607556B CN104607556B (en) | 2017-10-20 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201510055871.8A Expired - Fee Related CN104607556B (en) | 2015-02-03 | 2015-02-03 | A kind of aviation plug kludge |
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| Country | Link |
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| CN (1) | CN104607556B (en) |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4063941A (en) * | 1976-12-06 | 1977-12-20 | National Forge Company | Method for loading and unloading an isostatic press for compression of pre-formed powder objects |
| CN101450368A (en) * | 2007-12-05 | 2009-06-10 | 广东格兰仕集团有限公司 | Riveting processing device of magnetron |
| CN201405186Y (en) * | 2009-05-07 | 2010-02-17 | 宁波江北菲斯特机械有限公司 | Taper roller bearing assembly machine |
| CN103730810A (en) * | 2013-11-14 | 2014-04-16 | 苏州昌飞自动化设备厂 | Metal inserting sheet and shell assembling mechanism of USB assembling machine |
| CN103730819A (en) * | 2013-11-14 | 2014-04-16 | 苏州昌飞自动化设备厂 | Sheet iron shell and shell assembling mechanism of USB assembling machine |
| CN204524040U (en) * | 2015-02-03 | 2015-08-05 | 东莞富饶精密五金制品有限公司 | A kind of aviation plug kludge |
-
2015
- 2015-02-03 CN CN201510055871.8A patent/CN104607556B/en not_active Expired - Fee Related
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4063941A (en) * | 1976-12-06 | 1977-12-20 | National Forge Company | Method for loading and unloading an isostatic press for compression of pre-formed powder objects |
| CN101450368A (en) * | 2007-12-05 | 2009-06-10 | 广东格兰仕集团有限公司 | Riveting processing device of magnetron |
| CN201405186Y (en) * | 2009-05-07 | 2010-02-17 | 宁波江北菲斯特机械有限公司 | Taper roller bearing assembly machine |
| CN103730810A (en) * | 2013-11-14 | 2014-04-16 | 苏州昌飞自动化设备厂 | Metal inserting sheet and shell assembling mechanism of USB assembling machine |
| CN103730819A (en) * | 2013-11-14 | 2014-04-16 | 苏州昌飞自动化设备厂 | Sheet iron shell and shell assembling mechanism of USB assembling machine |
| CN204524040U (en) * | 2015-02-03 | 2015-08-05 | 东莞富饶精密五金制品有限公司 | A kind of aviation plug kludge |
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| Publication number | Publication date |
|---|---|
| CN104607556B (en) | 2017-10-20 |
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Granted publication date: 20171020 Termination date: 20220203 |
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| CF01 | Termination of patent right due to non-payment of annual fee |