CN212070030U - Bending die for aircraft wire harness support - Google Patents
Bending die for aircraft wire harness support Download PDFInfo
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- CN212070030U CN212070030U CN202020246221.8U CN202020246221U CN212070030U CN 212070030 U CN212070030 U CN 212070030U CN 202020246221 U CN202020246221 U CN 202020246221U CN 212070030 U CN212070030 U CN 212070030U
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- 238000005452 bending Methods 0.000 title claims abstract description 21
- 230000008878 coupling Effects 0.000 claims abstract description 13
- 238000010168 coupling process Methods 0.000 claims abstract description 13
- 238000005859 coupling reaction Methods 0.000 claims abstract description 13
- 230000007246 mechanism Effects 0.000 claims description 16
- 238000000034 method Methods 0.000 abstract description 9
- 230000008859 change Effects 0.000 abstract description 4
- 230000007105 physical stamina Effects 0.000 abstract description 3
- 230000008569 process Effects 0.000 description 6
- 230000008901 benefit Effects 0.000 description 4
- 230000033228 biological regulation Effects 0.000 description 3
- 230000005611 electricity Effects 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 230000004075 alteration Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000000295 complement effect Effects 0.000 description 1
- 230000003993 interaction Effects 0.000 description 1
- 210000001503 joint Anatomy 0.000 description 1
- 238000003754 machining Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
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- 238000006467 substitution reaction Methods 0.000 description 1
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Abstract
The utility model discloses an aircraft wire harness support mould of bending, comprising a base plate, the roof is installed to the top of bottom plate, the lower surface center rigid coupling of roof has the pneumatic cylinder, the bottom rigid coupling of pneumatic cylinder has the square plate, the lower surface mounting of square plate has the mould, the below of lower mould is equipped with the lower mould subassembly. This aircraft wire harness support mould of bending, through the bottom plate, the roof, the pneumatic cylinder, the square slab, go up the cooperation between mould and the lower module, run into in the course of working when suppressing different angle work pieces, operating personnel can reciprocate the screw rod, can make two down tubes rotate relatively, then can make the horizontal pole carry out the application of force to the layer board, can make two layer boards use the round pin hinge to rotate as the center, then can make the contained angle between two layer boards adjust, then make the contained angle of lower mould adjust, this in-process need not to dismantle the change with the lower mould, can reduce operating personnel's physical stamina consumption.
Description
Technical Field
The utility model relates to a mould technical field of bending specifically is an aircraft wire harness support mould of bending.
Background
Along with the rapid development of the industry in China, the appearance of an industrial product is more and more complex while meeting the performance requirement, the product can not be manufactured without a mould, and a bending machine mould is divided into an upper mould and a lower mould of a bending machine and is used for a mould for stamping and forming and separating a plate material.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide an aircraft wire harness support mould of bending to the aircraft wire harness support mould of bending among the present disclosed technology who proposes in solving above-mentioned background still has certain drawback in the use, for example the location angle of its lower mould is the definite value, can't carry out the regulation on the angle, once meet the work piece that needs the different angles of suppression, need dismantle the change with the lower mould, it is great to need operating personnel's work physical stamina consumption, is unfavorable for the high-efficient processing problem of work piece.
In order to achieve the above object, the utility model provides a following technical scheme: the bending die for the aircraft wire harness support comprises a bottom plate, wherein a top plate is mounted above the bottom plate, a hydraulic cylinder is fixedly connected to the center of the lower surface of the top plate, a square plate is fixedly connected to the bottom end of the hydraulic cylinder, an upper die is mounted on the lower surface of the square plate, and a lower die assembly is mounted below the upper die;
the lower die assembly comprises a supporting plate, hinges, a cross rod, a telescopic rod, a lantern ring, an inclined rod, a long slat and a screw rod;
the layer board is located the below of last mould, two the layer board rotates through the hinge and links to each other, the outside of layer board is rotated and is connected with the horizontal pole, horizontal pole other end rigid coupling has the telescopic link, the top of telescopic link links to each other with the lower fixed surface of roof, the outer wall of horizontal pole has cup jointed the lantern ring, the outer wall bottom of the lantern ring is rotated and is connected with the down tube, two it is connected with the rectangular board to rotate between the down tube bottom, the lower surface center rigid coupling of rectangular board has the screw rod, a part of screw rod runs through the bottom plate.
Preferably, the two diagonal rods are bilaterally symmetrical with respect to the center point of the long slat.
Preferably, the screw is connected with the bottom plate through an adjusting force application mechanism;
the adjusting force application mechanism comprises a circular groove, a cylinder, a disc, a square rod, a support plate and an upright rod;
the circular groove is arranged at the center of the lower surface of the bottom plate, the circular groove is connected with the cylinder in a rotating mode, the disc is fixedly connected to the bottom end of the inner wall of the cylinder, the inner wall of the disc is connected with the outer wall of the screw in a threaded mode, one part of the square rod is inserted into the screw, the outer wall of the square rod is in clearance fit with the inner wall of the screw, the support plate is fixedly connected to the bottom end of the square rod, the vertical rods are fixedly connected to the left side and the right side of the upper surface of the support plate, and the top end of the vertical rod is.
Preferably, the left side and the right side of the outer wall of the cylinder are fixedly connected with handles.
Preferably, the square rod and the screw form a sliding limiting structure.
Preferably, the left side and the right side of the upper surface of the strip plate are provided with auxiliary mechanisms;
the auxiliary mechanism comprises an electric push rod, a U-shaped plate and a roller;
two the bottom of electricity push rod is the rigid coupling respectively in the upper surface left and right sides of rectangular slab, the top rigid coupling of electricity push rod has the U template, the top of U template is rotated and is connected with the roller, the outer wall of roller is laminated with the lower surface of layer board mutually.
Compared with the prior art, the beneficial effects of the utility model are that: this aircraft wire harness support mould of bending for traditional technology, has following advantage:
through the bottom plate, the roof, the pneumatic cylinder, the square plate, go up the cooperation between mould and the lower mould subassembly, run into in the course of working and suppress different angle work pieces, operating personnel can reciprocate the screw rod, can make two down tubes carry out relative rotation, then can make the horizontal pole carry out the application of force to the layer board, can make two layer boards use the round pin hinge to rotate as the center, then can make the contained angle between two layer boards adjust, then make the contained angle of lower mould adjust, this in-process need not to dismantle the lower mould and change, can reduce operating personnel's physical stamina consumption, do benefit to the high-efficient processing of work piece.
Through the cooperation between bottom plate, screw rod and the regulation application of force mechanism, when needs go on the screw rod when lower regulation, operating personnel can rotate the drum, because of the square pole to the spacing of screw rod and the threaded connection relation of disc and screw rod, can make the screw rod reciprocate the process of adjusting comparatively simple, do benefit to operating personnel and operate.
Through the cooperation between rectangular board, layer board and the complementary unit, after the contained angle adjustment is accomplished between two layer boards, operating personnel control electric push rod makes the U template upwards remove, stops the control to electric push rod after making the lower surface of roller and layer board laminate mutually, and the roller can play certain supporting role to the layer board, can improve the stability of pressing process layer board.
Drawings
FIG. 1 is a schematic structural view of the present invention;
FIG. 2 is a schematic view of the connection structure of the supporting plate and the long slat of FIG. 1;
FIG. 3 is a schematic view showing a coupling structure of the base plate, the screw, and the disk of FIG. 2;
fig. 4 is a schematic view of the connection structure of the slat, pallet, and assist mechanism of fig. 2.
In the figure: 1. the device comprises a bottom plate, a top plate, a hydraulic cylinder, a square plate, a top die, a lower die assembly, a supporting plate, 602, a hinge, 603, a cross bar, 604, an expansion bar, 605, a lantern ring, 606, a diagonal bar, 607, a long strip plate, 608, a screw rod, 7, an adjusting force application mechanism, 701, a circular groove, 702, a cylinder, 703, a disc, 704, a square bar, 705, a supporting plate, 706, a vertical bar, 8, an auxiliary mechanism, 801, an electric push rod, 802, a U-shaped plate, 803, a roller, 9 and a handle.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.
Referring to fig. 1-4, the present invention provides a technical solution: an airplane wire harness support bending die comprises a bottom plate 1, a top plate 2 is installed above the bottom plate 1, a hydraulic cylinder 3 is fixedly connected to the center of the lower surface of the top plate 2, the hydraulic cylinder 3 is a HOB series light hydraulic cylinder, an oil control pipe of the hydraulic cylinder 3 is butted with an external oil supply device so as to control a push rod at the bottom end of the hydraulic cylinder 3 to stretch, a square plate 4 is fixedly connected to the bottom end of the push rod at the bottom end of the hydraulic cylinder 3, an upper die 5 is installed on the lower surface of the square plate 4, the upper die 5 is fixedly connected with the square plate 4 through a bolt so as to be convenient for an operator to detach, install, replace and maintain the upper die 5, a lower die assembly 6 is arranged below the upper die 5, the lower die assembly 6 comprises a supporting plate 601, a hinge 602, a cross rod 603, a telescopic rod 604, a lantern ring, an inclined rod 606, a long strip, the two support plates 601 are rotatably connected through a hinge 602, the two support plates 601 can rotate by taking the hinge 602 as a center, the outer sides of the support plates 601 are rotatably connected with a cross rod 603, the cross rod 603 is rotatably connected with the support plates 601 through a pin shaft, the other end of the cross rod 603 is fixedly connected with a telescopic rod 604, the telescopic rod 604 is composed of a sleeve and a vertical rod, the vertical rod can slide up and down in the sleeve, the bottom ends of the vertical rod are fixedly connected with the cross rod 603, the top end of the sleeve is fixedly connected with the lower surface of the top plate 2, the top end of the telescopic rod 604 is fixedly connected with the lower surface of the top plate 2, the outer wall of the cross rod 603 is sleeved with a sleeve ring 605, the inner wall of the sleeve ring 605 is fixedly connected with the outer wall of the cross rod 603, the bottom end of the outer wall of the sleeve ring 605 is rotatably connected with a diagonal rod 606, the diagonal rods are, part of the screw rod 608 penetrates through the bottom plate 1, the outer wall of the screw rod 608 is in clearance fit with the contact surface of the bottom plate 1, the two inclined rods 606 are bilaterally symmetrical relative to the center point of the long strip plate 607, and the two inclined rods 606 can be stressed identically in the up-and-down moving process of the long strip plate 607, so that the two inclined rods 606 can rotate relatively and synchronously.
The screw 608 is connected with the bottom plate 1 through the adjusting force applying mechanism 7, the adjusting force applying mechanism 7 comprises a circular groove 701, a cylinder 702, a disc 703, a square rod 704, a support plate 705 and a vertical rod 706, the circular groove 701 is arranged in the center of the lower surface of the bottom plate 1, the cylinder 702 is rotatably connected inside the circular groove 701, the cylinder 702 is rotatably connected with the circular groove 701 through a bearing, the disc 703 is fixedly connected with the bottom end of the inner wall of the cylinder 702, the inner wall of the disc 703 is in threaded connection with the outer wall of the screw 608, a part of the square rod 704 is inserted into the screw 608, the outer wall of the square rod 704 is in clearance fit with the inner wall of the screw 608, the support plate 705 is fixedly connected with the bottom end of the square rod 704, the vertical rods 706 are fixedly connected with the left side and the right side of the upper surface of the support plate 705, the top end of the vertical rod 706 is fixedly connected with the lower surface of the bottom plate 1, the, the square rod 704 can limit the screw 608 to ensure that the screw 608 does not rotate during moving up and down.
The left side and the right side of the upper surface of the long slat 607 are provided with auxiliary mechanisms 8, each auxiliary mechanism 8 comprises an electric push rod 801, a U-shaped plate 802 and a roller 803, the bottom ends of the two electric push rods 801 are fixedly connected to the left side and the right side of the upper surface of the long slat 607 respectively, the electric push rods 801 are XTL100 in model number, power lines of the electric push rods 801 are in butt joint with an external power supply control device, the top ends of the electric push rods 801 are fixedly connected with the U-shaped plates 802, the rollers 803 are rotatably connected with the U-shaped plates 802 through pin rods, and the outer walls of the rollers 803 are attached to the lower surface of the supporting plate 601.
When the bending die for the airplane wire harness support is used, firstly, a workpiece to be machined is placed above the two supporting plates 601, then the upper die 5 is used for compressing and bending the workpiece under the control of the hydraulic cylinder 3, when the workpiece with different angles is pressed in the machining process, an operator can rotate the cylinder 702, the disc 703 can rotate along with the cylinder 702, the screw 608 can be limited by the square rod 704 and the threaded connection relationship between the disc 703 and the screw 608 during the process, the process of adjusting the screw 608 in the up-and-down movement is simpler, the long strip 607 can move together during the up-and-down movement of the screw 608, the two inclined rods 606 can rotate relatively, then the cross rod 603 can apply force to the supporting plates 601, the two supporting plates 601 can rotate by taking the hinge 602 as the center, and then the included angle between the two supporting plates 601 can be adjusted, then make the contained angle of lower mould adjust, this in-process need not to dismantle the lower mould and change, do benefit to the high-efficient processing of work piece, after the contained angle adjustment is accomplished between two layer boards 601, operating personnel control electric push rod 801 makes U template 802 upwards remove, make roller 803 and layer board 601's lower surface laminate mutually the back stop the control to electric push rod 801, roller 803 can play certain supporting role to layer board 601, can improve the stability of pressing process layer board 601.
In the description of the present invention, it is to be understood that the terms "coaxial", "bottom", "one end", "top", "middle", "other end", "upper", "one side", "top", "inner", "front", "center", "both ends", and the like, indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings, and are only for convenience of description and simplicity of description, and do not indicate or imply that the device or element referred to must have a particular orientation, be constructed and operated in a particular orientation, and therefore, should not be construed as limiting the present invention.
In the present invention, unless otherwise expressly stated or limited, the terms "mounted," "disposed," "connected," "fixed," "screwed" and the like are to be construed broadly, e.g., as meaning fixedly connected, detachably connected, or integrally formed; can be mechanically or electrically connected; they may be directly connected or indirectly connected through an intermediate medium, and may be connected through the inside of two elements or in an interaction relationship between two elements, unless otherwise specifically defined, and the specific meaning of the above terms in the present invention will be understood by those skilled in the art according to specific situations.
Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.
Claims (6)
1. The utility model provides an aircraft pencil support mould of bending, includes bottom plate (1), its characterized in that: a top plate (2) is mounted above the bottom plate (1), a hydraulic cylinder (3) is fixedly connected to the center of the lower surface of the top plate (2), a square plate (4) is fixedly connected to the bottom end of the hydraulic cylinder (3), an upper die (5) is mounted on the lower surface of the square plate (4), and a lower die assembly (6) is arranged below the upper die (5);
the lower die assembly (6) comprises a supporting plate (601), a hinge (602), a cross rod (603), a telescopic rod (604), a lantern ring (605), an inclined rod (606), a long lath (607) and a screw rod (608);
the utility model discloses a top plate of a mould, including roof plate (2), layer board (601), horizontal pole (603), telescopic link (604), the outer wall of horizontal pole (603) has cup jointed lantern ring (605), the outer wall bottom of lantern ring (605) rotates and is connected with down tube (606), two it is connected with rectangular board (607) to rotate between down tube (606) bottom, the lower surface center rigid coupling of rectangular board (607) has screw rod (608), bottom plate (1) is run through to a part of screw rod (608).
2. The aircraft harness support bending die according to claim 1, wherein: the two diagonal rods (606) are symmetrical left and right relative to the center point of the long slat (607).
3. The aircraft harness support bending die according to claim 1, wherein: the screw (608) is connected with the bottom plate (1) through an adjusting force application mechanism (7);
the adjusting force application mechanism (7) comprises a circular groove (701), a cylinder (702), a disc (703), a square rod (704), a support plate (705) and an upright rod (706);
the lower surface center at bottom plate (1) is seted up in circular slot (701), the internal rotation of circular slot (701) is connected with drum (702), the inner wall bottom rigid coupling of drum (702) has disc (703), the inner wall of disc (703) links to each other with the outer wall screw thread of screw rod (608), the inside of screw rod (608) is inserted to some of square bar (704), the outer wall of square bar (704) and the inner wall clearance fit of screw rod (608), the bottom rigid coupling of square bar (704) has extension board (705), the equal rigid coupling in upper surface left and right sides of extension board (705) has pole setting (706), the top of pole setting (706) links to each other with the fixed surface of bottom plate (1).
4. The aircraft harness support bending die according to claim 3, wherein: the left side and the right side of the outer wall of the cylinder (702) are fixedly connected with handles (9).
5. The aircraft harness support bending die according to claim 3, wherein: the square rod (704) and the screw rod (608) form a sliding limiting structure.
6. The aircraft harness support bending die according to claim 1, wherein: auxiliary mechanisms (8) are arranged on the left side and the right side of the upper surface of the long strip plate (607);
the auxiliary mechanism (8) comprises an electric push rod (801), a U-shaped plate (802) and a roller (803);
two the bottom of electric putter (801) rigid coupling respectively is in the upper surface left and right sides of rectangular slat (607), the top rigid coupling of electric putter (801) has U template (802), the top of U template (802) is rotated and is connected with roller (803), the outer wall of roller (803) is laminated with the lower surface of layer board (601) mutually.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202020246221.8U CN212070030U (en) | 2020-03-03 | 2020-03-03 | Bending die for aircraft wire harness support |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202020246221.8U CN212070030U (en) | 2020-03-03 | 2020-03-03 | Bending die for aircraft wire harness support |
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| CN212070030U true CN212070030U (en) | 2020-12-04 |
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| CN202020246221.8U Active CN212070030U (en) | 2020-03-03 | 2020-03-03 | Bending die for aircraft wire harness support |
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Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113560377A (en) * | 2021-07-26 | 2021-10-29 | 江苏吉祥瑞合幕墙科技有限公司 | Rapid-positioning curtain wall aluminum single plate edge ridge bending device and positioning bending method |
| CN114618941A (en) * | 2022-03-16 | 2022-06-14 | 徐州三和机械零部件有限公司 | Bending device for precision machining of hydraulic fittings |
| CN117732961A (en) * | 2024-01-25 | 2024-03-22 | 开平市诚瑞丰科技有限公司 | Arc sheet metal workpiece stamping die and stamping equipment thereof |
-
2020
- 2020-03-03 CN CN202020246221.8U patent/CN212070030U/en active Active
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113560377A (en) * | 2021-07-26 | 2021-10-29 | 江苏吉祥瑞合幕墙科技有限公司 | Rapid-positioning curtain wall aluminum single plate edge ridge bending device and positioning bending method |
| CN113560377B (en) * | 2021-07-26 | 2022-07-29 | 江苏吉祥瑞合幕墙科技有限公司 | Rapid-positioning curtain wall aluminum single plate edge ridge bending device and positioning bending method |
| CN114618941A (en) * | 2022-03-16 | 2022-06-14 | 徐州三和机械零部件有限公司 | Bending device for precision machining of hydraulic fittings |
| CN114618941B (en) * | 2022-03-16 | 2024-07-05 | 徐州三和机械零部件有限公司 | Bending device for precision machining of hydraulic fittings |
| CN117732961A (en) * | 2024-01-25 | 2024-03-22 | 开平市诚瑞丰科技有限公司 | Arc sheet metal workpiece stamping die and stamping equipment thereof |
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Address after: 110000 No.23, Hongbin Road, Yuhong District, Shenyang City, Liaoning Province Patentee after: Liaoning Huatian Aviation Technology Co.,Ltd. Address before: 110000 No.23, Hongbin Road, Yuhong District, Shenyang City, Liaoning Province Patentee before: SHENZHEN HUATIAN AVIATION MACHINERY CO.,LTD. |