CN209635661U - A kind of coiling processing tool of aircraft engine clip resilient cushion - Google Patents
A kind of coiling processing tool of aircraft engine clip resilient cushion Download PDFInfo
- Publication number
- CN209635661U CN209635661U CN201920247980.3U CN201920247980U CN209635661U CN 209635661 U CN209635661 U CN 209635661U CN 201920247980 U CN201920247980 U CN 201920247980U CN 209635661 U CN209635661 U CN 209635661U
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- resilient cushion
- aircraft engine
- processing tool
- cylinder
- arm
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Abstract
The utility model discloses a kind of coiling processing tools of aircraft engine clip resilient cushion, belong to clip resilient cushion processing technique field.Including coil winding machine, the winding bracket of the output end connection arc of the coil winding machine, the working end of the winding bracket is equipped with the entrance hole passed through for helix, the coil winding machine opposite side is equipped with shaped support, the shaped support is connected to the end of pivoted arm, described pivoted arm one end is rotatablely connected sliding panel by rotary shaft, the output end of the hinged cylinder of the pivoted arm other end, the cylinder is hingedly located at the cylinder block on sliding panel, the sliding panel is slidably connected in linear guide by stepper motor driving, and the coil winding machine, cylinder and stepper motor are all connected with control system.The beneficial effects of the utility model are: reducing labor cost instead of manual work, working efficiency is improved, guarantees the uniformity of winding.
Description
Technical field
The utility model relates to a kind of processing unit (plant)s of aircraft engine resilient cushion, belong to clip resilient cushion processing technology
Field.
Background technique
Machine engine clip resilient cushion manufacturing process includes that the helix of spring like is carried out to horizontal and vertical winding, shape
At blank, blank passes through compacting again and forms resilient cushion, and existing blank is made by manually winding, production
Low efficiency, labor cost is high, and the elasticity and the uniformity that wind not can guarantee, and influence the matter of resilient cushion made of the later period
Amount.
Utility model content
To solve defect of the existing technology, manual work, winding are replaced the purpose of the utility model is to provide a kind of
Uniformly, work efficiency is high, the coiling processing tool of the low aircraft engine clip resilient cushion of labour cost.
The technical solution of the utility model is: a kind of coiling processing tool of aircraft engine clip resilient cushion, including around
Line machine, the winding bracket of the output end connection arc of the coil winding machine, the working end of the winding bracket is equipped with logical for helix
The entrance hole crossed, the coil winding machine opposite side are equipped with shaped support, and the shaped support is connected to the end of pivoted arm, the pivoted arm one
End is rotatablely connected sliding panel, the output end of the hinged cylinder of the pivoted arm other end by rotary shaft, and the cylinder is hingedly located at sliding panel
On cylinder block, the sliding panel by stepper motor driving be slidably connected in linear guide, the coil winding machine, cylinder and
Stepper motor is all connected with control system.
The winding bracket end is equipped with coiling elasticity regulating device, and the coiling elasticity regulating device includes, Gu
Be scheduled on the working end of winding bracket and there is externally threaded stud, be equipped with wedge cavities in the stud, the wedge cavities be connected into
String holes, wedge shape rubber block and wedge cavities plug-in type cooperate, and the outer top of wedge cavities is extended at the top of the wedge shape rubber block, described
Through there is the through-hole passed through for helix among wedge shape rubber block, stud is threadedly coupled adjusting nut, is equipped at the top of adjusting nut
Threading hole, the threading hole are connected to through-hole, are bonded at the top of adjusting nut inner top and wedge shape rubber block.
The shaped support includes that, in four screw rods that groined type is distributed, the end of adjacent screw rod is solid through L shape two-by-two
Determine the both ends of block, and be fixed by fixing bolt, shaped support is connect by L shape fixed block with pivoted arm.
The sliding panel bottom is fixed with the driving nut connecting with ball-screw, and the ball-screw is connected through shaft coupling
The stepper motor.
The linear guide is fixed on bottom plate, and stepper motor is fixed on motor fixing plate, the motor fixing plate bottom
Portion is fixed on bottom end.
The bottom plate and coil winding machine are separately fixed on the raised end face at matrix both ends.
The pivoted arm includes the slave arm of actuating arm and bending, and the output end of the hinged cylinder in actuating arm end rotates axle position
In on slave arm.
The rotational angle of the pivoted arm is 90 °.
The beneficial effects of the utility model are: reducing labor cost instead of manual work, working efficiency is improved, is guaranteed
The uniformity of winding.
Detailed description of the invention
Fig. 1 is the first state figure of the utility model；
Fig. 2 is second state diagram of the utility model；
Fig. 3 is winding bracket structure chart；
Fig. 4 is the partial enlarged view of Fig. 3.
Appended drawing reference is as follows in figure: 1, matrix, 2, coil winding machine, 3, winding bracket, 3.1, entrance hole, 4, shaped support,
4.1, screw rod, 4.2, L shape fixed block, 4.3, fixing bolt, 5, coiling elasticity regulating device, 5.1, stud, 5.2, wedge cavities,
5.3, wedge shape rubber block, 5.4, through-hole, 5.5, adjusting nut, 5.6, threading hole, 6, pivoted arm, 7, cylinder, 8, cylinder block, 9, sliding
Plate, 10, shaft coupling, 11, motor fixing plate, 12, stepper motor, 13, linear guide, 14, bottom plate, 15, ball-screw, 16, rotation
Shaft, 17, driving nut.
Specific embodiment
1-4 is described further the utility model with reference to the accompanying drawing:
A kind of coiling processing tool of aircraft engine clip resilient cushion, including coil winding machine 2, the output of the coil winding machine 2
The winding bracket 3 of end connection arc, the working end of the winding bracket 3 are equipped with the entrance hole 3.1 passed through for helix, it is described around
2 opposite side of line machine is equipped with shaped support 4, and the shaped support 4 includes, in four screw rods 4.1 that groined type is distributed, abutting two-by-two
The both ends of L shape fixed block 4.2 are run through in the end of screw rod 4.1, and are fixed by fixing bolt 4.3, and shaped support 4 passes through L
Shape fixed block 4.2 is connect with pivoted arm 6, and the pivoted arm 6 includes the slave arm of actuating arm and bending, the hinged cylinder 7 in actuating arm end
Output end, rotary shaft 16 is located on slave arm, and is rotatablely connected sliding panel 9 by rotary shaft 16, and the rotational angle of pivoted arm 6 is
90 °, the output end of the hinged cylinder 7 of 6 other end of pivoted arm, the cylinder 7 is hingedly located at the cylinder block 8 on sliding panel 9, the sliding
9 bottom of plate is fixed with the driving nut 17 connecting with ball-screw 15, and the ball-screw 15 connects the step through shaft coupling 10
Into motor 12, sliding panel 9 is slidably connected in linear guide 13 by the driving of stepper motor 12, and linear guide 13 is fixed on bottom plate
On 14, stepper motor 12 is fixed on motor fixing plate 11, and 11 bottom of motor fixing plate is fixed on 14 end of bottom plate, bottom plate
14 and coil winding machine 2 be separately fixed on the raised end face at 1 both ends of matrix, the coil winding machine 2, cylinder 7 and stepper motor 12
It is all connected with control system；3 end of winding bracket is equipped with coiling elasticity regulating device 5, and the coiling elasticity adjusts dress
Setting 5 includes being fixed on the working end of winding bracket 3 and having externally threaded stud 5.1, is equipped with wedge cavities in the stud 5.1
5.2, the wedge cavities 5.2 are connected to entrance hole 3.1, and wedge shape rubber block 5.3 and 5.2 plug-in type of wedge cavities cooperate, and the wedge shape
It extends to the outer top of wedge cavities 5.2 at the top of rubber block 5.3, passes through for helix through having among the wedge shape rubber block 5.3
Through-hole 5.4, stud 5.1 are threadedly coupled adjusting nut 5.5, are equipped with threading hole 5.6, the threading hole 5.6 at the top of adjusting nut 5.5
It is connected to through-hole 5.4, is bonded at the top of 5.5 inner top of adjusting nut and wedge shape rubber block 5.3.
Before work, the spring like helix made first is passed through into coiling elasticity regulating device 5 and entrance hole 3.1, Gu
To determine onto screw rod 4.1, rotating adjusting nut 5.5, adjusting nut 5.5 squeezes wedge shape rubber block 5.3 into wedge cavities 5.2, with
Extruding, wedge shape rubber block 5.3 can be deformed because of the extruding of wedge cavities 5.2,5.4 size of through-hole becomes smaller, and the inner wall of through-hole 5.4 squeezes
Pressing spring shape helix, and then change active force of the inner wall to spring like helix of through-hole 5.4, realize pressing spring shape helix
By the adjustment of pull power size when pull, pull power is bigger, and winding is tighter, and pull power is smaller, winds more loose, winding elasticity tune
It is whole it is good after, start coil winding machine 2 and stepper motor 12, winding bracket 3 is rotated around the shaped support 4 under first state, by bullet
On spring shape helical wound to shaped support 4, in winding process, stepper motor drives sliding panel 9 to drive shaped support 4 mobile,
Make in helix uniform winding to shaped support 4, after shaped support 4 is wrapped over one layer in the first state, coil winding machine 2 and step
Stop into motor 12, cylinder 7 starts, and driving pivoted arm 6 drives shaped support 4 to be rotated by 90 ° second state that reaches, coil winding machine 2 and step
It is again started up into motor 12, shaped support 4 is wrapped over one layer in the first state, complete a working cycles, repeated above-mentioned
Working cycles, until blank winding is completed, equipment stops, and cuts helix, screw rod 4.1 is unloaded from L shape fixed block 4.2
Under, then screw rod 4.1 extracted out from blank, by blank centralized collection, screw rod 4.1 is loaded onto, is made into next blank
Circulation.
The above is only the preferred embodiment of the utility model, it is noted that for the common skill of the art
For art personnel, without deviating from the technical principle of the utility model, several improvements and modifications can also be made, these change
It also should be regarded as the protection scope of the utility model into modification.
Claims (8)
1. a kind of coiling processing tool of aircraft engine clip resilient cushion, which is characterized in that including coil winding machine (2), it is described around
The winding bracket (3) of the output end connection arc of line machine (2), the working end of the winding bracket (3) is equipped with to be passed through for helix
Entrance hole (3.1), coil winding machine (2) opposite side is equipped with shaped support (4), and the shaped support (4) is connected to pivoted arm (6)
End, described pivoted arm (6) one end pass through rotary shaft (16) rotation connection sliding panel (9), the hinged cylinder of pivoted arm (6) other end (7)
Output end, the cylinder (7) is hingedly located at the cylinder block (8) on sliding panel (9), and the sliding panel (9) passes through stepper motor
(12) driving is slidably connected on linear guide (13), and the coil winding machine (2), cylinder (7) and stepper motor (12) are all connected with
Control system.
2. the coiling processing tool of aircraft engine clip resilient cushion according to claim 1, which is characterized in that it is described around
Line bracket (3) end be equipped with coiling elasticity regulating device (5), the coiling elasticity regulating device (5) include be fixed on around
The working end of line bracket (3) and there are externally threaded stud (5.1), is equipped with wedge cavities (5.2) in the stud (5.1), it is described
Wedge cavities (5.2) are connected to entrance hole (3.1), and wedge shape rubber block (5.3) and wedge cavities (5.2) plug-in type cooperate, and the wedge shape
Wedge cavities (5.2) top outside is extended at the top of rubber block (5.3), running through among the wedge shape rubber block (5.3) has for helix
By through-hole (5.4), stud (5.1) is threadedly coupled adjusting nut (5.5), threading hole is equipped at the top of adjusting nut (5.5)
(5.6), threading hole (5.6) connection through-hole (5.4), adjusting nut (5.5) inner top and wedge shape rubber block (5.3) top are pasted
It closes.
3. the coiling processing tool of aircraft engine clip resilient cushion according to claim 1, which is characterized in that it is described at
Type bracket (4) includes that, in four screw rods (4.1) that groined type is distributed, the end of adjacent screw rod (4.1) is solid through L shape two-by-two
Determine the both ends of block (4.2), and be fixed by fixing bolt (4.3), shaped support (4) is by L shape fixed block (4.2) and turns
Arm (6) connection.
4. the coiling processing tool of aircraft engine clip resilient cushion according to claim 1, which is characterized in that the cunning
Movable plate (9) bottom is fixed with the driving nut (17) connecting with ball-screw (15), and the ball-screw (15) is through shaft coupling
(10) stepper motor (12) is connected.
5. the coiling processing tool of aircraft engine clip resilient cushion according to claim 1, which is characterized in that described straight
Line guide rail (13) is fixed on bottom plate (14), and stepper motor (12) is fixed on motor fixing plate (11), the motor fixing plate
(11) bottom is fixed on bottom plate (14) end.
6. the coiling processing tool of aircraft engine clip resilient cushion according to claim 5, which is characterized in that the bottom
Plate (14) and coil winding machine (2) are separately fixed on the raised end face at matrix (1) both ends.
7. the coiling processing tool of aircraft engine clip resilient cushion according to claim 1, which is characterized in that described turn
Arm (6) includes the slave arm of actuating arm and bending, the output end of the hinged cylinder in actuating arm end (7), rotary shaft (16) be located at from
On swing arm.
8. the coiling processing tool of aircraft engine clip resilient cushion according to claim 1, which is characterized in that described turn
The rotational angle of arm (6) is 90 °.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920247980.3U CN209635661U (en) | 2019-02-27 | 2019-02-27 | A kind of coiling processing tool of aircraft engine clip resilient cushion |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920247980.3U CN209635661U (en) | 2019-02-27 | 2019-02-27 | A kind of coiling processing tool of aircraft engine clip resilient cushion |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN209635661U true CN209635661U (en) | 2019-11-15 |
Family
ID=68494687
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201920247980.3U Active CN209635661U (en) | 2019-02-27 | 2019-02-27 | A kind of coiling processing tool of aircraft engine clip resilient cushion |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN209635661U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109850703A (en) * | 2019-02-27 | 2019-06-07 | 大连萌羽机械有限公司 | A kind of coiling processing tool of aircraft engine clip resilient cushion |
-
2019
- 2019-02-27 CN CN201920247980.3U patent/CN209635661U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109850703A (en) * | 2019-02-27 | 2019-06-07 | 大连萌羽机械有限公司 | A kind of coiling processing tool of aircraft engine clip resilient cushion |
| CN109850703B (en) * | 2019-02-27 | 2023-12-01 | 大连萌羽机械有限公司 | Winding tooling for aircraft engine clamp shock pad |
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