CN205704468U - A kind of perforating device - Google Patents

A kind of perforating device Download PDF

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Publication number
CN205704468U
CN205704468U CN201620528570.2U CN201620528570U CN205704468U CN 205704468 U CN205704468 U CN 205704468U CN 201620528570 U CN201620528570 U CN 201620528570U CN 205704468 U CN205704468 U CN 205704468U
Authority
CN
China
Prior art keywords
translation stage
punching unit
main shaft
collet
drill bit
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Fee Related
Application number
CN201620528570.2U
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Chinese (zh)
Inventor
苏琳
初巧妹
吕东喜
游峰
李芳�
李娃
冯建鸿
黄勇
李波
张占文
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Laser Fusion Research Center China Academy of Engineering Physics
Original Assignee
Laser Fusion Research Center China Academy of Engineering Physics
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Filing date
Publication date
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Priority to CN201620528570.2U priority Critical patent/CN205704468U/en
Application granted granted Critical
Publication of CN205704468U publication Critical patent/CN205704468U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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  • Drilling Tools (AREA)

Abstract

This utility model provides a kind of perforating device.The described positioning baffle in device is fixed on optical table.Punching unit I, punching unit II that structure is identical are symmetricly set on optical table, and the translation stage in punching unit I, punching unit II is fixing with optical table respectively to be connected.Being fixedly connected with spindle drum on translation stage in punching unit I, punching unit II, main shaft is fixing with spindle drum to be connected, and collet is arranged on main shaft, and drill bit is arranged on collet.Translation stage III is fixing with optical table to be connected, and described adaptor is fixed on translation stage III, and adaptor is fixedly installed fixture.This utility model is particularly suited for arbitrarily the most symmetrically or non-symmetrically structure and workpiece that material is carbon fibre composite are carried out drilling.This utility model avoids the problem that punching exit burr occurs, tears and be layered, and not only can complete the making of high-quality single hole, and be capable of the making of high-quality stepped hole.This utility model is simple to operate, and cost of manufacture is low, and production efficiency is high.

Description

A kind of perforating device
Technical field
This utility model belongs to hole fabrication techniques field, is specifically related to a kind of perforating device, it is possible to for carbon fiber composite The drilling of material.
Background technology
Owing to carbon fibre composite (CFRP) has, specific strength is high, specific stiffness is big, can significantly reduce aerospace vehicle The superior character that other traditional materials such as weight, anti-fatigue performance that designability is strong and good and corrosion resistance are incomparable, Therefore it is used widely at aerospace field.Composite consumption aboard and application site have become measurement aircraft One of important indicator that structure is advanced.Composite is not only used widely on big aircraft manufacturing at present, and respectively Application in model unmanned plane manufacture also presents a rapidly rising trend.
In the connection of Carbon-fiber Reinforced Plastics Component, mechanical connection is topmost type of attachment, and hole machined by , difficulty many in quantity is greatly operation particularly important in carbon fibre composite post-treatment.The quality of its quality, is directly connected to Carbon fibre composite product, so that the quality of whole aircraft.The crudy of connecting hole is directly connected to the assembling matter of aircraft Amount and Aircraft life.Owing to carbon fibre composite is heterogeneous body and anisotropic, and the hardness of carbon fiber is the highest, thus multiple The machining of condensation material is essentially different with metal material, therefore uses traditional drilling gold when composite drilling The method belonged to will produce more problem.During drilling, any quality problems all can form the defect of product, causes part rejection.According to Statistics, aircraft is when finally assembling, and drilling disqualification rate to account for more than the 60% of whole composite material parts scrappage.
During carbon fibre composite drilling, the size of axial force directly affects drilling quality, is to cause hole wall week Enclosing layers of material, hole enters, outlet tears, the principal element of the significant deficiency such as burr.Use the high speed of mainshaft and low feeding Speed is conducive to reducing axial force, but this otherwise lathe is proposed higher requirement, or working (machining) efficiency can be reduced.
During drilling, along with cutting depth increases, the non-thickness of cutting of material reduces, carbon fibre composite critical Axial force declines the most therewith, when the axial force that drilling produces exceedes its axis critical force, the outlet side in hole is occurred layering Deng manufacturing deficiency, exit remains the more fiber burr not cut off, and the crudy of incision position is relatively rough, has some fibre It is exposed near bore edges, additionally, excessive axial force also results in the generation of outlet tearing defect.Generally, carbon fiber is combined The veining defect of material can pass through file or elimination of reaming further, but, tear and lamination defect are even more serious, once Occur, it is virtually impossible to repair.
Summary of the invention
For asking of solving in carbon fibre composite drilling exit, burr to occur in prior art, tear and be layered Topic, this utility model provides a kind of perforating device, it is possible to for the drilling of carbon fibre composite.
A kind of perforating device of the present utility model, is characterized in, described device include punching unit I, punching unit II, Workpiece, workpiece adjust parts, positioning baffle and optical table, and described punching unit I includes drill bit I, collet I, main shaft I, spindle drum I and translation stage I, described punching unit II includes drill bit II, collet II, main shaft II, spindle drum II peace Moving stage II, described workpiece adjusts parts and includes fixture, adaptor and translation stage III.Its annexation is that positioning baffle is fixed On optical table.Punching unit I, punching unit II that structure is identical are symmetricly set on optical table, in punching unit I Translation stage I, the translation stage II of punching unit II are fixed with optical table respectively and are connected, translation stage I, the difference of translation stage II Overlap with the inner edge of positioning baffle.Translation stage I is provided with the translation with D translation function with the midpoint of translation stage II line Platform III, translation stage III is fixing with optical table to be connected.Spindle drum I, main shaft I and main shaft it is fixedly connected with on described translation stage I Seat I is fixing to be connected, and collet I is arranged on main shaft I, and drill bit I is arranged on collet I.On described translation stage II admittedly Determining connection and have spindle drum II, main shaft II is fixing with spindle drum II to be connected, and collet II is arranged on main shaft II, and drill bit II is installed On collet II.Described adaptor is fixed on translation stage III, adaptor is fixedly installed fixture (12), treats drilling Workpiece is fixed on fixture.
Described drill bit I is arranged for concentric with drill bit II.
Described main shaft I and main shaft II use the one in pneumatically or electrically main shaft.
This utility model is particularly suited for arbitrarily symmetrically or non-symmetrically structure and material are the work of carbon fibre composite Part carries out drilling.
Perforating device of the present utility model provides the benefit that, this utility model avoids carbon fibre composite and punches out Burr, the problem tearing and being layered occur at Kou.This utility model has been possible not only to the most symmetrically or non-symmetrically structure Carbon fibre composite carries out the making of high-quality single hole, and is capable of the making of high-quality stepped hole.This utility model Simple to operation, cost of manufacture is low, and production efficiency is high.
Accompanying drawing explanation
Fig. 1 is the structural representation of this utility model perforating device;
Fig. 2 is the top view of this utility model perforating device;
1. drill bit I 2. collet I 3. main shaft I 4. spindle drum I 5. translation stage I 6. drill bit II 7. in figure Collet II 8. main shaft II 9. spindle drum II 10. translation stage II 11. workpiece 12. fixture 13. adaptor 14. translation stage III 15. positioning baffle 16. optical tables.
Detailed description of the invention
Below in conjunction with the accompanying drawings this utility model is described in detail.
Embodiment 1
Fig. 1 is the structural representation of this utility model perforating device, and Fig. 2 is the top view of this utility model perforating device. In Fig. 1, Fig. 2, perforating device of the present utility model includes that described device includes punching unit I, punching unit II, workpiece 11, workpiece adjusts parts, positioning baffle 15 and optical table 16, described punching unit I include drill bit I 1, collet I 2, Main shaft I 3, spindle drum I 4 and translation stage I 5, described punching unit II include drill bit II 6, collet II 7, main shaft II (8), Spindle drum II 9 and translation stage II 10, described workpiece adjusts parts and includes fixture 12, adaptor 13 and translation stage III 14.It is even The relation of connecing is, positioning baffle 15 is fixed on optical table 16.Punching unit I, punching unit II that structure is identical are symmetrical arranged On optical table 16, translation stage I 5, the translation stage II 10 of punching unit II in punching unit I are solid with optical table 16 respectively Fixed connecting, translation stage I 5, the inner edge with positioning baffle 15 respectively of translation stage II 10 overlap.Translation stage I 5 and translation stage II The midpoint of 10 lines is provided with the translation stage III 14 with D translation function, and translation stage III 14 is fixing with optical table 16 even Connect.Being fixedly connected with spindle drum I 4 on described translation stage I 5, main shaft I 3 is fixing with spindle drum I 4 to be connected, and collet I 2 is installed On main shaft I 3, drill bit I 1 is arranged on collet I 2.Spindle drum II 9 it is fixedly connected with on described translation stage II 10, main Axle II 8 is fixing with spindle drum II 9 to be connected, and collet II 7 is arranged on main shaft II 8, and drill bit II (6) is arranged on collet II On 7.Described adaptor 13 is fixed on translation stage III 14, and adaptor 13 is fixedly installed fixture 12, treats drilling workpiece 11 It is fixed on fixture 12.
Described drill bit I 1 is arranged for concentric with drill bit II 6.
Described main shaft I 3 all uses pneumatic main shaft with main shaft II 8.
This utility model is particularly suited for arbitrarily symmetrically or non-symmetrically structure and material are the work of carbon fibre composite Part 11 carries out drilling.
The specific operation process of perforating device of the present utility model is: first fixed by the workpiece 11 of tactical rule or abnormity On appropriate fixture.Adjust translation stage III 14 and make at workpiece 11 drilling and drill bit I 1 position consistency, translation stage I 5 stroke is set It is 2/3 hole depth, opens punching unit I and carry out drilling, complete backed off after random punching unit I.Arranging translation stage II 10 stroke again is 1/2 Hole depth, opens punching unit II and carries out drilling until through hole backed off after random punching unit II i.e. completes carbon fibre composite high-quality Drilling.
Only the drill bit I 1 during above-mentioned drilling need to be installed smaller hole when carbon fibre composite is prepared stepped hole Drill bit, arranging translation stage I 5 stroke is minor diameter hole depth;Drill bit II 6 during above-mentioned drilling is installed large hole drill bit, if Horizontalization moving stage II 10 stroke is that major diameter hole depth can prepare the high-quality stepped hole meeting condition.
Embodiment 2
The present embodiment is identical with the structure of embodiment 1, is a difference in that, described main shaft I 3 all uses electricity with main shaft II 8 Dynamic main shaft.

Claims (3)

1. a perforating device, it is characterised in that: described device includes punching unit I, punching unit II, workpiece (11), work Part adjusts parts, positioning baffle (15) and optical table (16), and described punching unit I includes drill bit I (1), collet I (2), main shaft I (3), spindle drum I (4) and translation stage I (5), described punching unit II includes drill bit II (6), collet II (7), main shaft II (8), spindle drum II (9) and translation stage II (10), described workpiece adjusts parts and includes fixture (12), adaptor (13) and translation stage III (14), its annexation is, positioning baffle (15) is fixed on optical table (16);Identical the beating of structure Hole parts I, punching unit II are symmetricly set on optical table (16), the translation stage I (5) in punching unit I, punching unit II Translation stage II (10) fixing with optical table (16) be respectively connected, translation stage I (5), translation stage II (10) respectively with The inner edge of positioning baffle (15) overlaps;The midpoint of translation stage I (5) and translation stage II (10) line is provided with has D translation merit The translation stage III (14) of energy, translation stage III (14) is fixing with optical table (16) to be connected;The described upper company of fixing of translation stage I (5) Being connected to spindle drum I (4), main shaft I (3) is fixing with spindle drum I (4) to be connected, and collet I (2) is arranged on main shaft I (3), drill bit I (1) is arranged on collet I (2);Spindle drum II (9), main shaft II (8) it is fixedly connected with on described translation stage II (10) Fixing with spindle drum II (9) and be connected, collet II (7) is arranged on main shaft II (8), and drill bit II (6) is arranged on collet On II (7);Described adaptor (13) is fixed on translation stage III (14), and adaptor (13) is fixedly installed fixture (12), Treat that drilling workpiece (11) is fixed on fixture (12).
Perforating device the most according to claim 1, it is characterised in that: described drill bit I (1) is coaxial with drill bit II (6) The heart is arranged.
Perforating device the most according to claim 1, it is characterised in that: described main shaft I (3) uses gas with main shaft II (8) One in dynamic or electric main shaft.
CN201620528570.2U 2016-06-03 2016-06-03 A kind of perforating device Expired - Fee Related CN205704468U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201620528570.2U CN205704468U (en) 2016-06-03 2016-06-03 A kind of perforating device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201620528570.2U CN205704468U (en) 2016-06-03 2016-06-03 A kind of perforating device

Publications (1)

Publication Number Publication Date
CN205704468U true CN205704468U (en) 2016-11-23

Family

ID=57299701

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201620528570.2U Expired - Fee Related CN205704468U (en) 2016-06-03 2016-06-03 A kind of perforating device

Country Status (1)

Country Link
CN (1) CN205704468U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106042050A (en) * 2016-06-03 2016-10-26 中国工程物理研究院激光聚变研究中心 Perforating device

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106042050A (en) * 2016-06-03 2016-10-26 中国工程物理研究院激光聚变研究中心 Perforating device

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C14 Grant of patent or utility model
GR01 Patent grant
CF01 Termination of patent right due to non-payment of annual fee
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20161123

Termination date: 20200603