CN214768414U - Closing-in machine for aviation male head - Google Patents
Closing-in machine for aviation male head Download PDFInfo
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- CN214768414U CN214768414U CN202120769061.XU CN202120769061U CN214768414U CN 214768414 U CN214768414 U CN 214768414U CN 202120769061 U CN202120769061 U CN 202120769061U CN 214768414 U CN214768414 U CN 214768414U
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Abstract
The utility model discloses a closing machine for public head of aviation for produce public head of aviation, include wherein: the rotating assembly is arranged in an intermittent rotating mode, a plurality of accommodating parts are formed in the rotating assembly, and the accommodating parts are used for accommodating the aviation male heads; the power assembly is respectively connected with the pushing part, the closing part and the forming part on the power assembly; the pushing part, the closing part and the forming part are positioned above the rotating assembly; the pushing part is driven by the power assembly to press the inner support of the aviation male head, the closing part is driven by the power assembly to retract the opening of the aviation male head, and the forming part is driven by the power assembly to form a boss on the inner wall of the opening of the aviation male head. The problems of low manual closing-in efficiency and difficulty in quality guarantee in the existing production and processing technology are solved.
Description
Technical Field
The utility model relates to a connector production field especially relates to a binding off machine for public head of aviation.
Background
In the prior art, an aviation male connector in a connector generally comprises a housing and an inner support arranged in the housing, a contact pin is inserted into the inner support, the inner support is installed into the housing through an opening at one side of the housing, and after the inner support is installed into the housing, the opening of the housing needs to be closed. The prior art processes close up manually.
The production mode still needs more manpower to complete the mass production of the connectors, has extremely high labor cost and extremely low efficiency, and can continuously prolong the whole production period; in addition, the subjective factors finished manually are more, and the product quality and precision are difficult to guarantee.
Accordingly, the prior art is yet to be improved and developed.
SUMMERY OF THE UTILITY MODEL
In view of the not enough of above-mentioned prior art, the utility model aims at providing a binding off machine for public head of aviation aims at solving the problem that artifical binding off inefficiency, quality are difficult to guarantee among the current production and processing technique.
The technical scheme of the utility model as follows:
a necking machine for an aerospace male, for producing an aerospace male, comprising: the rotating assembly is arranged in an intermittent rotating mode, a plurality of accommodating parts are formed in the rotating assembly, and the accommodating parts are used for accommodating the aviation male heads;
the power assembly is respectively connected with the pushing part, the closing part and the forming part on the power assembly; the pushing part, the closing part and the forming part are positioned above the rotating assembly;
the pushing part is driven by the power assembly to press the inner support of the aviation male head, the closing part is driven by the power assembly to retract the opening of the aviation male head, and the forming part is driven by the power assembly to form a boss on the inner wall of the opening of the aviation male head.
Further, the necking machine also comprises a rack, and the power assembly is arranged on the rack;
the power assembly includes:
the power part is arranged on the rack;
a connecting table, one end of which is connected to an output shaft of the power part and the other end of which is connected to the pushing part, the closing part and the forming part;
the guide sliding part is connected to the rack, and the connecting table is connected to the guide sliding part and slides directionally through the guide of the guide sliding part.
Further, the pressing portion includes: the pressure pipe, the one end of pressure pipe is connected connect on the connection platform, the external diameter of pressure pipe orientation the one end of holding portion is less than the opening internal diameter of aviation public head.
Further, the closing-in portion includes: the one end of tang pipe is connected connect on the connection bench, the tang pipe orientation first chamfer has been seted up to the inner wall edge of the one end of holding portion, first chamfer orientation the internal diameter of the one end of holding the chamber is greater than the outer wall of the tang end of aviation, first chamfer deviates from the internal diameter of the one end of holding the chamber is less than the outer wall of the tang end of aviation.
Further, the molding portion includes:
the one end of forming tube is connected connect the bench, the forming tube orientation the one end of portion of holding is provided with a word and presses the platform, the most advanced orientation that the platform was pressed to a word the public binding off terminal surface of aviation.
Further, the frame is including the horizontal stand, and rotating assembly includes:
the rotary power part is arranged on the lower surface of the horizontal table;
the transmission part is arranged on the lower surface of the horizontal table, one end of the transmission part is connected to the rotary power part, and the other end of the transmission part penetrates through the horizontal table;
the rotating disc is connected to one end, penetrating through the horizontal table, of the transmission part, and the accommodating part is arranged on the rotating disc.
Further, the accommodating portion includes: the accommodating cavity faces the orifice of one end of the power assembly, a second chamfer is arranged at the orifice, and the aviation male head is arranged in the accommodating cavity.
Further, the necking machine still includes blank pressing portion, blank pressing portion includes:
the support table is arranged on the rack;
the one end of the edge pressing plate is connected to the supporting table, the other end of the edge pressing plate is suspended above the rotating disc, and when the aviation male head rotates to the pressing portion, the closing portion and the forming portion, the outer circle baffle of the aviation male head is located between the edge pressing plate and the upper surface of the rotating disc.
Further, the necking machine still includes ejection of compact subassembly, ejection of compact subassembly includes:
the upper jacking cylinder is arranged on the lower surface of the horizontal table;
the upper ejection column is connected to an output shaft of the upper ejection cylinder and is arranged on the horizontal table and the accommodating cavity in a penetrating manner, and the upper ejection column is positioned below one accommodating cavity;
the material guide pipe is arranged corresponding to the upper top column, penetrates through the horizontal table, and an upper opening of the material guide pipe faces the rotating disc.
Further, 12 accommodating parts are arranged, and the 12 accommodating parts are uniformly distributed at the periphery of the rotating disc around the rotating center of the rotating disc.
Compared with the prior art, the utility model has the advantages that the aviation male head is inserted into the containing part of the rotating component, the rotating component drives the aviation male head to rotate obliquely in the rotating process, when the aviation male head rotates to the position below the pushing part, the pushing part moves towards the aviation male head under the driving of the power component, the pushing part pushes the inner support in the shell of the aviation male head down, the inner support is pressed to ensure that the position of the inner support in the shell is pressed in place, after the pushing part is removed, the aviation male head pressed in place is rotated to the position below the closing part, the closing part is pressed towards the aviation male head through the driving of the power component, the opening of the aviation male head is retracted, the orifice of the shell of the aviation male head is reduced, the inner support cannot be loosened, after the closing part is removed, the aviation male head after being retracted rotates to the position below the forming part, and the forming part moves towards the aviation male head through the driving of the power component, and the extrusion is on the end surface of the opening of the aviation male head, the end surface of the opening of the compressed aviation male head can deform towards the inner cavity of the opening, the deformation can enable the end surface of the inner cavity of the opening to form a boss, the boss enables the inner support not to be separated from the opening, and the inner support is fixed more firmly. The automatic closing-in of the aviation male head is realized, the labor is saved, the efficiency is improved, the product consistency is good, and the product quality is improved.
Drawings
FIG. 1 is a schematic structural diagram of a conventional aircraft male connector;
fig. 2 is a schematic structural diagram of an embodiment of a necking machine for an aviation male head of the present invention;
FIG. 3 is an enlarged view of portion A of FIG. 2;
fig. 4 is a schematic structural view of another view angle of an embodiment of a necking machine for an aviation male of the present invention;
fig. 5 is a cross-sectional view of an embodiment of a necking machine for an aviation male of the present invention;
FIG. 6 is an enlarged view of the portion B of FIG. 5;
fig. 7 is a schematic structural view of a forming tube according to an embodiment of the closing machine for an aviation male plug of the present invention.
The reference numbers in the figures: 100. aviation male heads; 110. a housing; 120. an inner support; 130. inserting a pin; 140. an outer circle baffle plate; 200. a frame; 210. a horizontal table; 220. a frame body; 300. a rotating assembly; 310. an accommodating portion; 311. an accommodating chamber; 312. a second chamfer; 320. a rotary power unit; 330. a transmission section; 340. rotating the disc; 400. a power assembly; 410. a power section; 420. a connecting table; 430. a guide sliding part; 500. a pressing section; 510. pushing the pipe; 600. a closing-in part; 610. a mouth-closing tube; 620. a first chamfer; 700. a molding section; 710. forming a tube; 720. a linear pressing table; 800. pressing edge parts; 810. a support table; 820. pressing an edge plate; 900. a discharge assembly; 910. an upper jacking cylinder; 920. an upper top pillar; 930. a material guide pipe.
Detailed Description
The utility model provides a necking machine for public head of aviation, for making the utility model discloses a purpose, technical scheme and effect are clearer, make clear and definite, and it is right that the following refers to the drawing and lifts the example the utility model discloses further detailed description. It should be understood that the specific embodiments described herein are merely illustrative of the invention and are not intended to limit the invention.
As shown in fig. 2, a necking machine for an aircraft male head is used for producing an aircraft male head 100, as shown in fig. 1, the aircraft male head 100 produced in the embodiment includes a shell 110, an opening is provided at one end of the shell 110, an inner support 120 installed into the shell 110 through the opening, a pin 130 is fixed on the inner support 120, and a circle of outer circular baffle 140 is provided on an outer wall of the shell 110. Wherein, for convenient structure description, use the direction of closing in machine orientation operator as preceding, with preceding opposite direction be the back, use operator's left and right directions as the left and right directions of closing in machine, the vertical placing of closing in machine to the vertical direction when the vertical placing of closing in machine is the upper and lower direction. As shown in fig. 2 and 3, the necking machine for the aviation male head in the scheme comprises: the rotating unit 300, the power unit 400, the pushing part 500, the closing part 600, and the forming part 700 connected to the power unit 400, respectively. The rotary member 300 is intermittently rotated, as shown in fig. 5, a plurality of accommodating portions 310 are formed on the rotary member 300, the accommodating portions 310 are used for accommodating the aviation male 100, and the pushing portion 500, the closing portion 600, and the forming portion 700 are located above the rotary member 300. The pushing portion 500 presses the inner bracket 120 of the aircraft male 100 by the driving of the power assembly 400, the closing portion 600 retracts the opening of the aircraft male 100 by the driving of the power assembly 400, and the forming portion 700 forms a boss on the inner wall of the opening of the aircraft male 100 by the driving of the power assembly 400.
With the above structure, by inserting the aviation male 100 into the accommodating portion 310 of the rotating assembly 300, the rotating assembly 300 rotates to drive the aviation male 100 to rotate obliquely, when the aviation male is rotated to the position below the pushing portion 500, the pushing portion 500 moves towards the aviation male 100 under the driving of the power assembly 400, the pushing portion presses the inner support 120 in the housing 110 of the aviation male 100 downwards, the inner support 120 is pressed to the position in the housing 110, after the pushing portion 500 is removed, the aviation male 100 pressed to the position by the inner support 120 rotates to the position below the closing portion 600, the closing portion 600 is pressed to the aviation male 100 by the driving of the power assembly 400 to retract the opening of the aviation male 100, the opening of the housing 110 of the aviation male 100 becomes small, the inner support 120 does not loosen, after the closing portion 600 is removed, the closed aviation male 100 rotates to the position below the forming portion 700, the forming part 700 moves towards the aviation male head 100 through the driving of the power assembly 400 and presses the end face of the opening of the aviation male head 100, the end face of the opening of the compressed aviation male head 100 deforms towards the inner cavity of the opening, the deformation enables the end face of the inner cavity of the opening to form a boss, the boss enables the inner support 120 not to be separated from the opening, and the inner support 120 is fixed more firmly. The automatic closing of the aviation male head 100 is realized, the labor is saved, the efficiency is improved, the product consistency is good, and the product quality is improved.
As shown in fig. 2, in the specific structure of this embodiment, the necking machine further includes a frame 200, where the frame 200 includes a horizontal platform 210, the horizontal platform 210 is laid along a horizontal direction, and a frame body 220 located at one side of the horizontal platform 210 and extending upward. The power assembly 400 is disposed on the frame 200, specifically, the power assembly 400 is disposed on the frame body 220 and provides power in the vertical direction.
As shown in fig. 4 and 5, the rotating assembly 300 in this embodiment specifically includes: a rotary power part 320, a transmission part 330, and a rotary disk 340. The rotary power part 320 is disposed on the lower surface of the horizontal stage 210, and the rotary power part 320 in this embodiment is a motor, which may be a stepping motor or a servo motor, so as to facilitate the control of the intermittent motion and the more accurate positioning. The transmission part 330 is disposed on the lower surface of the horizontal stage 210, one end of the transmission part 330 is connected to the rotary power part 320, and the other end penetrates through the horizontal stage 210. The transmission part 330 in this embodiment is a speed reducer, a power input end of the speed reducer is disposed along a horizontal direction and connected to an output shaft of the rotary power part 320, and a power output end of the speed reducer penetrates through the horizontal table 210 along an up-down direction. The rotating plate 340 is connected to the transmission part 330 and penetrates one end of the horizontal stage 210, and the receiving part 310 is disposed on the rotating plate 340. Specifically, the rotating disc 340 is fixedly connected to the power output end of the transmission part 330. The rotary power unit 320 is powered on and then starts to transmit a rotary torque to the rotary disk 340 through the transmission unit 330, so that the rotary disk 340 on the horizontal stage 210 rotates. The speed reducer can change the rotating direction while reducing the speed.
As shown in fig. 5 and 6, the accommodating portion 310 in this embodiment includes an accommodating cavity 311, a second chamfer 312 is disposed at an aperture of the accommodating cavity 311 facing one end of the power assembly 400, and the aviation male 100 is disposed in the accommodating cavity 311. The opening at the upper end of the accommodating cavity 311 is provided with a chamfer, so that the aviation male head 100 can be conveniently placed into the accommodating cavity 311. The number of the receiving portions 310 is 12, and 12 receiving portions 310 are uniformly distributed around the rotation center of the rotating disk 340 at the periphery of the rotating disk 340.
As shown in fig. 5, the power assembly 400 specifically includes: a power part 410, a connection stage 420, and a guide sliding part 430. The power part 410 is disposed on the frame 200, and the power part 410 in this embodiment is a push-down cylinder, and after the push-down cylinder is started, an output shaft of the push-down cylinder moves from top to bottom. One end of the connecting table 420 is connected to an output shaft of the power unit 410, and the other end is connected to the pressing unit 500, the receiving unit 600, and the molding unit 700. The upper end of the connecting table 420 is connected to the output shaft of the push-down cylinder, the lower end face of the connecting table 420 is fixedly connected with the pushing portion 500, the closing portion 600 and the forming portion 700 through pressing blocks and screws, when the power portion 410 is started, the connecting table 420 is driven to move in the vertical direction, the pushing portion 500, the closing portion 600 and the forming portion 700 can be driven to work simultaneously, and the pushing portion 500, the closing portion 600 and the forming portion 700 respectively complete respective process procedures. The guide sliding part 430 is connected to the frame 200, and the connection stage 420 is connected to the guide sliding part 430 and is guided by the guide sliding part 430 to be slid in a direction. Specifically, the guide sliding portion 430 is disposed along the vertical direction, and the guide sliding portion 430 disposed along the vertical direction can guide the movement of the connection stage 420, so that the connection stage 420 can move up and down more stably. The pushing part 500, the closing part 600 and the forming part 700 are driven by the same power part 410, and then different aviation male heads 100 reach corresponding stations through rotation of the rotating disc 340, so that different aviation male heads 100 can be processed at the same time, and the processing efficiency is improved.
As shown in fig. 2 and 3, the pressing unit 500 in the present embodiment includes: a push pipe 510, one end of the push pipe 510 being connected to the connection platform 420, an outer diameter of one end of the push pipe 510 facing the accommodating part 310 being smaller than an inner diameter of an opening of the aviation male 100. When the pushing pipe 510 is pressed down, the inner cavity of the pushing pipe 510 can accommodate the insertion pin 130 of the aviation male 100, and the pipe body of the pushing pipe 510 is located in the opening of the aviation male 100, so as to push the inner support 120 of the aviation male 100, and push the inner support 120 of the aviation male 100 in place.
As shown in fig. 3 and 5, the mouth portion 600 in the present embodiment includes: a closing-in pipe 610, the one end of closing-in pipe 610 is connected on the joint block 420, closing-in pipe 610 orientation first chamfer 620 has been seted up to the inner wall edge of the one end of holding portion 310, first chamfer 620 towards the internal diameter that holds the one end of chamber 311 is greater than the outer wall of the closing-in end of aviation male 100, first chamfer 620 deviates from the internal diameter that holds the one end of chamber 311 is less than the outer wall of the closing-in end of aviation male 100. Specifically, a first chamfer 620 is arranged at the inner circle of the lower end of the closing-in pipe 610, the inner diameter of the lower end of the first chamfer 620 is large, and the inner diameter of the upper end is small. Thus, when the closing pipe 610 is pressed downwards, the outer wall of the opening side of the aviation male 100 is located in the first chamfer 620 of the closing pipe 610, the opening of the aviation male 100 is integrally retracted through the pressing of the closing pipe 610, the hole of the outer shell 110 of the aviation male 100 is reduced, and the inner support 120 cannot loosen.
As shown in fig. 2 and 7, the forming portion 700 in this embodiment includes a forming tube 710, one end of the forming tube 710 is connected to the connecting platform 420, an end of the forming tube 710 facing the accommodating portion 310 is provided with a linear pressing platform 720, and a tip of the linear pressing platform 720 faces a closing end surface of the aircraft male tip 100. Specifically, two sides of the lower end of the forming tube 710 are symmetrically beveled, two tips are respectively formed at two sides of the lower end of the beveled forming tube 710, and the tips are in a shape of a straight line along the left-right direction, that is, the two sides can both form a straight pressing platform 720. When the forming pipe 710 is pressed downwards, the linear pressing platforms 720 on two sides extrude the end surface of the opening of the aviation male 100, the end surface of the opening of the compressed aviation male 100 deforms towards the inner cavity of the opening, the deformation can enable the end surface of the opening inner cavity to form a boss, the boss on the inner wall of the opening enables the inner support 120 not to be separated from the opening, and the inner support 120 is fixed more firmly.
As shown in fig. 1 and fig. 6, the necking machine in the present embodiment further includes a beading portion 800, where the beading portion 800 includes: a support stage 810, and an edge plate 820. The supporting platform 810 and the edge pressing plate 820 are arc-shaped, and the supporting platform 810 is disposed on the frame 200 and located outside the rotating disc 340. One end of the edge pressing plate 820 is connected to the supporting platform 810, and the other end is suspended above the rotating disc 340. The supporting platform 810 and the edge pressing plate 820 are only arc-shaped structures and are located in the area range where the rotary disk 340 drives the aviation male head 100 to rotate to the pushing part 500, the closing part 600 and the forming part 700. Thus, when the aircraft male 100 is rotated to a position below the pressing portion 500, the receiving portion 600, and the molding portion 700, the outer circular baffle 140 of the aircraft male 100 is positioned between the edge pressing plate 820 and the upper surface of the rotating disk 340. When the pushing portion 500, the closing portion 600, and the forming portion 700 respectively push down the aviation male tip 100, the pressing portion 800 limits the position of the aviation male tip 100, and does not drive the processed aviation male tip 100 to be separated from the accommodating portion 310 when the pushing portion 500, the closing portion 600, and the forming portion 700 return.
As shown in fig. 2 and 4, the necking machine in this embodiment further includes an outfeed assembly 900, where the outfeed assembly 900 includes: an upper top cylinder 910, an upper top post 920, and a guide pipe 930. The upper top cylinder 910 is arranged on the lower surface of the horizontal table 210; the upper prop 920 is connected to an output shaft of the upper prop cylinder 910 and is disposed through the horizontal table 210 and the accommodating cavity 311, and the upper prop 920 is located below one of the accommodating cavity 311. The material guiding pipe 930 is disposed corresponding to the upper support column 920, the material guiding pipe 930 penetrates the horizontal stage 210, and an upper opening of the material guiding pipe 930 faces the rotating disc 340. Specifically, the discharging assembly 900 is located on one side of the forming portion 700, when the aviation male head 100 is brought to the discharging assembly 900 by the rotating assembly 300, the upward ejecting cylinder 910 is started, the output shaft of the upward ejecting cylinder 910 drives the upward ejecting column 920 to move, the upward moving ejecting column 920 enters the accommodating portion 310, the processed aviation male head 100 in the accommodating portion 310 is ejected, the ejected aviation male head 100 can fall into the material guide pipe 930, and the processed aviation male head 100 is guided out and concentrated through the material guide pipe 930. In addition, the material guiding pipe 930 can generate suction gas, and the ejected aviation male head 100 can be sucked into the material guiding pipe 930.
To sum up, the utility model discloses an in inserting rotatory subassembly's accommodation portion with the public head of aviation, rotatory subassembly rotation process in drive the public head of aviation rotation to one side, when rotatory bulldozing the portion below, bulldoze the portion under power component's drive, towards the public head motion of aviation, the inner support that the promotion portion pushed down to be located the public head of aviation, exert pressure to the inner support, make the position of inner support in the shell put in place, after the bulldozing portion withdraws from the place, the public head of aviation that the inner support pressed in place rotated to the department of collection below, the department of collection passes through power component's drive and presses to the public head of aviation, and makes the opening of the public head of aviation contract inwards, and the drill way of the public head of aviation diminishes, makes the inner support can not become flexible, and after the department of collection withdraws from the department of collection, the public head of aviation after the throat rotates to the department of shaping, the shaping portion passes through power component's drive and moves towards the public head of aviation, and the extrusion is on the end surface of the opening of the aviation male head, the end surface of the opening of the compressed aviation male head can deform towards the inner cavity of the opening, the deformation can enable the end surface of the inner cavity of the opening to form a boss, the boss enables the inner support not to be separated from the opening, and the inner support is fixed more firmly. The automatic closing-in of the aviation male head is realized, the labor is saved, the efficiency is improved, the product consistency is good, and the product quality is improved.
It is to be understood that the invention is not limited to the above-described embodiments, and that modifications and variations may be made by those skilled in the art in light of the above teachings, and all such modifications and variations are intended to be included within the scope of the invention as defined in the appended claims.
Claims (10)
1. A necking machine for an aviation male head, for producing an aviation male head, comprising: the rotating assembly is arranged in an intermittent rotating mode, a plurality of accommodating parts are formed in the rotating assembly, and the accommodating parts are used for accommodating the aviation male heads;
the power assembly is respectively connected with the pushing part, the closing part and the forming part on the power assembly; the pushing part, the closing part and the forming part are positioned above the rotating assembly;
the pushing part is driven by the power assembly to press the inner support of the aviation male head, the closing part is driven by the power assembly to retract the opening of the aviation male head, and the forming part is driven by the power assembly to form a boss on the inner wall of the opening of the aviation male head.
2. The necking machine for an aerospace male according to claim 1, further comprising a frame, the power assembly being disposed on the frame;
the power assembly includes:
the power part is arranged on the rack;
the connecting table is connected with the output shaft of the power part at one end and connected with the pushing part, the closing part and the forming part at the other end;
the guide sliding part is connected to the rack, and the connecting table is connected to the guide sliding part and slides directionally through the guide of the guide sliding part.
3. The necking machine for aerospace male according to claim 2, wherein the pushing portion comprises: the pressure pipe, the one end of pressure pipe is connected connect on the connection platform, the external diameter of pressure pipe orientation the one end of holding portion is less than the opening internal diameter of aviation public head.
4. A necking machine for aerospace male heads according to claim 2, wherein the mouth-in portion comprises: the one end of tang pipe is connected connect on the connection bench, the tang pipe orientation first chamfer has been seted up to the inner wall edge of the one end of holding portion, first chamfer orientation the internal diameter of the one end of holding portion is greater than the outer wall of the tang end of aviation, first chamfer deviates from the internal diameter of the one end of holding portion is less than the outer wall of the tang end of aviation.
5. A necking machine for aerospace male according to claim 2, wherein the forming portion comprises:
the one end of forming tube is connected connect the bench, the forming tube orientation the one end of portion of holding is provided with a word and presses the platform, the most advanced orientation that the platform was pressed to a word the public binding off terminal surface of aviation.
6. A necking machine for aerospace male heads according to claim 2, wherein the frame comprises a horizontal table and the rotating assembly comprises:
the rotary power part is arranged on the lower surface of the horizontal table;
the transmission part is arranged on the lower surface of the horizontal table, one end of the transmission part is connected to the rotary power part, and the other end of the transmission part penetrates through the horizontal table;
the rotating disc is connected to one end, penetrating through the horizontal table, of the transmission part, and the accommodating part is arranged on the rotating disc.
7. A necking machine for aerospace male heads according to claim 6, wherein the receiving portion comprises: the accommodating cavity faces the orifice of one end of the power assembly, a second chamfer is arranged at the orifice, and the aviation male head is arranged in the accommodating cavity.
8. A necking machine for aerospace male according to claim 7, further comprising a beading portion, the beading portion comprising:
the support table is arranged on the rack;
the one end of the edge pressing plate is connected to the supporting table, the other end of the edge pressing plate is suspended above the rotating disc, and when the aviation male head rotates to the pushing portion, the closing portion and the forming portion respectively, the outer circle baffle of the aviation male head is located between the edge pressing plate and the upper surface of the rotating disc.
9. The necking machine for an aerospace male head of claim 8, further comprising an outfeed assembly, the outfeed assembly comprising:
the upper jacking cylinder is arranged on the lower surface of the horizontal table;
the upper ejection column is connected to an output shaft of the upper ejection cylinder and is arranged on the horizontal table and the accommodating cavity in a penetrating manner, and the upper ejection column is positioned below one accommodating cavity;
the material guide pipe is arranged corresponding to the upper top column, penetrates through the horizontal table, and an upper opening of the material guide pipe faces the rotating disc.
10. A necking machine for aerospace male heads according to claim 6, wherein 12 pockets are provided, the 12 pockets being evenly distributed around the center of rotation of the rotating disc at the periphery of the rotating disc.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202120769061.XU CN214768414U (en) | 2021-04-14 | 2021-04-14 | Closing-in machine for aviation male head |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202120769061.XU CN214768414U (en) | 2021-04-14 | 2021-04-14 | Closing-in machine for aviation male head |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN214768414U true CN214768414U (en) | 2021-11-19 |
Family
ID=78687122
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202120769061.XU Active CN214768414U (en) | 2021-04-14 | 2021-04-14 | Closing-in machine for aviation male head |
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| Country | Link |
|---|---|
| CN (1) | CN214768414U (en) |
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2021
- 2021-04-14 CN CN202120769061.XU patent/CN214768414U/en active Active
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