CN106217046A - A kind of drilling-tapping machine - Google Patents
A kind of drilling-tapping machine Download PDFInfo
- Publication number
- CN106217046A CN106217046A CN201610788960.8A CN201610788960A CN106217046A CN 106217046 A CN106217046 A CN 106217046A CN 201610788960 A CN201610788960 A CN 201610788960A CN 106217046 A CN106217046 A CN 106217046A
- Authority
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- China
- Prior art keywords
- crossbeam
- drilling
- fuselage
- parts
- tapping machine
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Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23P—METAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
- B23P23/00—Machines or arrangements of machines for performing specified combinations of different metal-working operations not covered by a single other subclass
- B23P23/02—Machine tools for performing different machining operations
-
- C—CHEMISTRY; METALLURGY
- C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
- C08L—COMPOSITIONS OF MACROMOLECULAR COMPOUNDS
- C08L23/00—Compositions of homopolymers or copolymers of unsaturated aliphatic hydrocarbons having only one carbon-to-carbon double bond; Compositions of derivatives of such polymers
- C08L23/02—Compositions of homopolymers or copolymers of unsaturated aliphatic hydrocarbons having only one carbon-to-carbon double bond; Compositions of derivatives of such polymers not modified by chemical after-treatment
- C08L23/10—Homopolymers or copolymers of propene
- C08L23/12—Polypropene
-
- C—CHEMISTRY; METALLURGY
- C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
- C08L—COMPOSITIONS OF MACROMOLECULAR COMPOUNDS
- C08L2201/00—Properties
- C08L2201/02—Flame or fire retardant/resistant
-
- C—CHEMISTRY; METALLURGY
- C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
- C08L—COMPOSITIONS OF MACROMOLECULAR COMPOUNDS
- C08L2205/00—Polymer mixtures characterised by other features
- C08L2205/02—Polymer mixtures characterised by other features containing two or more polymers of the same C08L -group
-
- C—CHEMISTRY; METALLURGY
- C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
- C08L—COMPOSITIONS OF MACROMOLECULAR COMPOUNDS
- C08L2205/00—Polymer mixtures characterised by other features
- C08L2205/03—Polymer mixtures characterised by other features containing three or more polymers in a blend
- C08L2205/035—Polymer mixtures characterised by other features containing three or more polymers in a blend containing four or more polymers in a blend
-
- C—CHEMISTRY; METALLURGY
- C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
- C08L—COMPOSITIONS OF MACROMOLECULAR COMPOUNDS
- C08L2205/00—Polymer mixtures characterised by other features
- C08L2205/14—Polymer mixtures characterised by other features containing polymeric additives characterised by shape
- C08L2205/16—Fibres; Fibrils
Abstract
nullThe open a kind of drilling-tapping machine of the present invention，Including fuselage、Crossbeam、Drive motor and turret head，Described crossbeam is located on fuselage，Described crossbeam is fixing with fuselage to be connected，Described driving motor is arranged on crossbeam，Described turret head is arranged on crossbeam front end，Described turret head is hinged with crossbeam，Described fuselage side is provided with drilling equipment and tapping device，Described drilling equipment and merit tooth device are fixing with fuselage respectively to be connected，Described fuselage bottom is provided with workbench，Described workbench is connected with sliding machine body，Described turret head side is provided with spring，Described spring end is provided with hook，Described spring is connected with crossbeam by hook，Screw rod is installed bottom described workbench and drives motor，The drilling-tapping machine work efficiency of the present invention is high，Easily it is adjusted，It is high that the crossbeam used has structural strength，The high advantage with good flame retardation effect of elongation percentage.
Description
Technical field
Present invention relates particularly to a kind of drilling-tapping machine.
Background technology
Drilling-tapping machine is a kind of Metal Cutting Machine Tool, numerically controlled processing equipment, and pattern is similar with machining center with function, only
It is more smaller than machining center.Screw and nut are the most universal and that structure is simple fixation kits, with regard to portable type hands
As a example by machine, just it appeared that number of modules or template utilize screw to interfix after carefully tearing portable type mobile phone open, say, that
Screw by substantial amounts of use among portable type mobile phone, but reality is in addition to portable type mobile phone uses screw the most in a large number, the most greatly
The slightest device or system etc., it can be seen that screw and the utilization of nut.The universal use of screw makes its demand increase, for
, also can change from the semi-automatic processing that former times is past for manufacturing the working and forming machine (being referred to as screw processing machine) of screw in response to demand
Enter and process for full-automation.But along with the precision of electronic product develops, the requirement to screw is the most accurate, and some electronics produces
Product need special screw, nut, need the screw thread on less nut and nut to reach certain requirement, in actual production,
For this nut, may often be such that the manual lathe spindle that the half-formed nut of processing is put into one by one nut shaping machine of workman,
Then lathe carries out the drilling operation of nut.After drilling operation, nut is put into tooth machining unit tapping by workman again.This adopt
By the method inefficiency of artificial loading processing, and a chassis bed need to be equipped with an employee, if leaving the post such as employee or asking for leave, and machine
Platform will be unable to run.Simultaneously because easily fatigue also results in production capacity reduction when employee operates long
Current existing drilling-tapping machine work efficiency is the highest, it is not easy to being adjusted, the crossbeam of employing does not have structure
Intensity is high, the high advantage with good flame retardation effect of elongation percentage.
Summary of the invention
It is high that the technical problem to be solved in the present invention is to provide a kind of work efficiency, is easily adjusted, the crossbeam tool of employing
There is structural strength high, the drilling-tapping machine of the high advantage with good flame retardation effect of elongation percentage.
For solving the problems referred to above, the present invention adopts the following technical scheme that
A kind of drilling-tapping machine, including fuselage, crossbeam, driving motor and turret head, described crossbeam is located on fuselage, described
Crossbeam is fixing with fuselage to be connected, and described driving motor is arranged on crossbeam, and described turret head is arranged on crossbeam front end, described capstan head
Head is hinged with crossbeam, and described fuselage side is provided with drilling equipment and tapping device, described drilling equipment and merit tooth device respectively
Fixing with fuselage and be connected, described fuselage bottom is provided with workbench, and described workbench is connected with sliding machine body, and described capstan head is first
Side is provided with spring, and described spring end is provided with hook, and described spring is connected with crossbeam, bottom described workbench by hook
Screw rod is installed and drives motor.
Further, described crossbeam is made up of the material of following parts by weight proportioning, including carbon fiber 45-50 part, asbestos
7-8 part, polypropylene fibre 10-15 part, polyvinyl chloride fibre 6-10 part, polyimide fiber 3-5 part, tetrafluoroethene-hexafluoro third
Alkene copolymer fibre 1-3 part, antimony oxide 8-10 part, magnesium hydroxide 5-9 part, aluminium hydroxide 3-5 part, butyl rubber 3-6 part, silicon
Ketone 10-14 part, white carbon black 7-9 part, stearic acid file 8-10 part, aluminium stearate 2-4 part, phosphorous vinegar titanium dioxide 1-2 part and boric acid
Zinc 2-5 part.
Further, described screw rod is connected with driving motor-driven.
Further, described screw rod is connected with table drive.
Further, described spring is compression spring.
Further, described fuselage bottom is provided with leg.
Further, described leg is provided with more than one.
Further, described carbon fiber is carbon nano-fiber.
Further, described butyl rubber is through being ground into 20 mesh powder.
The preparation method of a kind of crossbeam, comprises the following steps:
1) by carbon fiber 45-50 part, asbestos 7-8 part, polypropylene fibre 10-15 part, polyvinyl chloride fibre 6-10 part, polyamides
Imine fiber 3-5 part, tetrafluoro-hexafluoroethylene copolymer fiber 1-3 part and antimony oxide 8-10 part put in drying baker, protect
Hold temperature be 45-50 DEG C dry 3-5 hour, standby；
2) by step 1) raw material of gained puts in reactor, and temperature regulates to 2800-295 DEG C, and speed of agitator is
3500-3800r/min, reacts 20-25 minute, standby；
3) by magnesium hydroxide 5-9 part, aluminium hydroxide 3-5 part, butyl rubber 3-6 part, silicone 10-14 part, white carbon black 7-9 part,
Stearic acid file 8-10 part, aluminium stearate 2-4 part, phosphorous vinegar titanium dioxide 1-2 part and Firebrake ZB 2-5 part put into heating tank
In, carry out 55-65 DEG C and preheat 3 minutes, standby；
4) by step 3) gained raw material puts in blender, and holding rotating speed is 2000-2200r/min, and stirring 15-20 divides
Clock, mix homogeneously, standby；
5) by step 2) gained raw material and step 4) raw material puts in high-temperature heating case, is heated to 300-320 DEG C, standby
With；
6) by step 5) gained material injecting mould is shaped, die sinking after natural cooling, obtain blank, standby；
7) to step 6) gained blank carries out bore operation, carries out sanding and polishing operation the most again, obtains semi-finished product, standby
With；
8) in step 7) carry out nickel plating process on gained semi-finished product,.
The invention has the beneficial effects as follows: the turret head of setting easily carries out tool changing operation, keep work efficiency high；Arrange
Being provided with screw rod bottom workbench and drive motor, can be regulated the position of workbench by screw rod, holding position is easy to adjust；
The carbon fiber added in the raw material of the crossbeam arranged keeps structural strength high, lightweight；The antimony oxide of interpolation, hydrogen in crossbeam
Magnesium oxide and aluminium hydroxide keep good flame retardation effect；Stearic acid file, aluminium stearate and the phosphorous vinegar added in the crossbeam arranged
Titanium dioxide keeps structural elongation high.
Accompanying drawing explanation
Fig. 1 is the structure chart of the present invention a kind of drilling-tapping machine.
Fig. 2 is the top view of the present invention a kind of drilling-tapping machine.
Detailed description of the invention
Embodiment one:
Refering to shown in Fig. 1 and Fig. 2, a kind of drilling-tapping machine, including fuselage 1, crossbeam 2, driving motor 3 and turret head 4, institute
Stating crossbeam 2 and set on the fuselage 1, described crossbeam 2 is fixing with fuselage 1 to be connected, and described driving motor 3 is arranged on crossbeam 2, described turn
Tower head 4 is arranged on crossbeam 2 front end, and described turret head 4 is hinged with crossbeam 2, and described fuselage 1 side is provided with drilling equipment 5 and attacks
Tooth device 6, described drilling equipment 5 and merit tooth device 6 are fixing with fuselage 1 respectively to be connected, and is provided with workbench bottom described fuselage 1
7, described workbench 7 is slidably connected with fuselage 1, and described turret head 4 side is provided with spring 8, and described spring 8 end is provided with extension
Hook 9, described spring 8 is connected with crossbeam 2 by hook 9, is provided with screw rod 10 and drives motor 11 bottom described workbench 7.
Described crossbeam 2 is made up of the material of following parts by weight proportioning, including 50 parts of carbon fiber, 7 parts of asbestos, polypropylene fibre
Tie up 10 parts, polyvinyl chloride fibre 6 parts, polyimide fiber 3 parts, tetrafluoro-hexafluoroethylene copolymer fiber 1 part, three oxidation two
8 parts of antimony, 5 parts of magnesium hydroxide, aluminium hydroxide 3 parts, butyl rubber 3 parts, silicone 10 parts, white carbon black 7 parts, stearic acid file 8 parts, stearic acid
2 parts of aluminum, phosphorous vinegar titanium dioxide 1 part and Firebrake ZB 2 parts.
Described screw rod 10 is in transmission connection with driving motor 11.
Described screw rod 10 is in transmission connection with workbench 7.
Described spring 8 is compression spring.
Bottom described fuselage 1, leg 12 is installed.
Described leg 12 is provided with more than one.
Described carbon fiber is carbon nano-fiber.
Described butyl rubber is through being ground into 20 mesh powder.
The preparation method of a kind of crossbeam 2, comprises the following steps:
1) by 50 parts of carbon fiber, 7 parts of asbestos, polypropylene fibre 10 parts, polyvinyl chloride fibre 6 parts, polyimide fiber 3
In part, tetrafluoro-hexafluoroethylene copolymer fiber 1 part and 8 parts of input drying baker of antimony oxide, temperature is kept to be 45-50 DEG C
It is dried 3-5 hour, standby；
2) by step 1) raw material of gained puts in reactor, and temperature regulates to 2800-295 DEG C, and speed of agitator is
3500-3800r/min, reacts 20-25 minute, standby；
3) by 5 parts of magnesium hydroxide, aluminium hydroxide 3 parts, butyl rubber 3 parts, silicone 10 parts, white carbon black 7 parts, stearic acid file 8 parts,
Aluminium stearate 2 parts, phosphorous vinegar titanium dioxide 1 part and Firebrake ZB 2 parts are put in heating tank, carry out 55-65 DEG C and preheat 3 points
Clock, standby；
4) by step 3) gained raw material puts in blender, and holding rotating speed is 2000-2200r/min, and stirring 15-20 divides
Clock, mix homogeneously, standby；
5) by step 2) gained raw material and step 4) raw material puts in high-temperature heating case, is heated to 300-320 DEG C, standby
With；
6) by step 5) gained material injecting mould is shaped, die sinking after natural cooling, obtain blank, standby；
7) to step 6) gained blank carries out bore operation, carries out sanding and polishing operation the most again, obtains semi-finished product, standby
With；
8) in step 7) carry out nickel plating process on gained semi-finished product,.
Embodiment two:
Refering to shown in Fig. 1 and Fig. 2, a kind of drilling-tapping machine, including fuselage 1, crossbeam 2, driving motor 3 and turret head 4, institute
Stating crossbeam 2 and set on the fuselage 1, described crossbeam 2 is fixing with fuselage 1 to be connected, and described driving motor 3 is arranged on crossbeam 2, described turn
Tower head 4 is arranged on crossbeam 2 front end, and described turret head 4 is hinged with crossbeam 2, and described fuselage 1 side is provided with drilling equipment 5 and attacks
Tooth device 6, described drilling equipment 5 and merit tooth device 6 are fixing with fuselage 1 respectively to be connected, and is provided with workbench bottom described fuselage 1
7, described workbench 7 is slidably connected with fuselage 1, and described turret head 4 side is provided with spring 8, and described spring 8 end is provided with extension
Hook 9, described spring 8 is connected with crossbeam 2 by hook 9, is provided with screw rod 10 and drives motor 11 bottom described workbench 7.
Described crossbeam 2 is made up of the material of following parts by weight proportioning, including 47.5 parts of carbon fiber, 7.5 parts of asbestos, poly-third
Alkene fiber 12.5 parts, polyvinyl chloride fibre 8 parts, polyimide fiber 4 parts, tetrafluoro-hexafluoroethylene copolymer fiber 2 parts, three
Aoxidize 9 parts of two antimony, 7 parts of magnesium hydroxide, aluminium hydroxide 4 parts, butyl rubber 4.5 parts, silicone 12 parts, white carbon black 8 parts, stearic acid file 9
Part, aluminium stearate 3 parts, phosphorous vinegar titanium dioxide 1.5 parts and Firebrake ZB 3.5 parts.
Described screw rod 10 is in transmission connection with driving motor 11.
Described screw rod 10 is in transmission connection with workbench 7.
Described spring 8 is compression spring.
Bottom described fuselage 1, leg 12 is installed.
Described leg 12 is provided with more than one.
Described carbon fiber is carbon nano-fiber.
Described butyl rubber is through being ground into 20 mesh powder.
The preparation method of a kind of crossbeam 2, comprises the following steps:
1) by 47.5 parts of carbon fiber, 7.5 parts of asbestos, polypropylene fibre 12.5 parts, polyvinyl chloride fibre 8 parts, polyimides
In fiber 4 parts, tetrafluoro-hexafluoroethylene copolymer fiber 2 parts and 9 parts of input drying baker of antimony oxide, holding temperature is 45-
50 DEG C dry 3-5 hour, standby；
2) by step 1) raw material of gained puts in reactor, and temperature regulates to 2800-295 DEG C, and speed of agitator is
3500-3800r/min, reacts 20-25 minute, standby；
3) by 7 parts of magnesium hydroxide, aluminium hydroxide 4 parts, butyl rubber 4.5 parts, silicone 12 parts, white carbon black 8 parts, stearic acid file 9
Part, aluminium stearate 3 parts, phosphorous vinegar titanium dioxide 1.5 parts and Firebrake ZB 3.5 parts are put in heating tank, carry out 55-65 DEG C in advance
Heat 3 minutes, standby；
4) by step 3) gained raw material puts in blender, and holding rotating speed is 2000-2200r/min, and stirring 15-20 divides
Clock, mix homogeneously, standby；
5) by step 2) gained raw material and step 4) raw material puts in high-temperature heating case, is heated to 300-320 DEG C, standby
With；
6) by step 5) gained material injecting mould is shaped, die sinking after natural cooling, obtain blank, standby；
7) to step 6) gained blank carries out bore operation, carries out sanding and polishing operation the most again, obtains semi-finished product, standby
With；
8) in step 7) carry out nickel plating process on gained semi-finished product,.
Embodiment three:
Refering to shown in Fig. 1 and Fig. 2, a kind of drilling-tapping machine, including fuselage 1, crossbeam 2, driving motor 3 and turret head 4, institute
Stating crossbeam 2 and set on the fuselage 1, described crossbeam 2 is fixing with fuselage 1 to be connected, and described driving motor 3 is arranged on crossbeam 2, described turn
Tower head 4 is arranged on crossbeam 2 front end, and described turret head 4 is hinged with crossbeam 2, and described fuselage 1 side is provided with drilling equipment 5 and attacks
Tooth device 6, described drilling equipment 5 and merit tooth device 6 are fixing with fuselage 1 respectively to be connected, and is provided with workbench bottom described fuselage 1
7, described workbench 7 is slidably connected with fuselage 1, and described turret head 4 side is provided with spring 8, and described spring 8 end is provided with extension
Hook 9, described spring 8 is connected with crossbeam 2 by hook 9, is provided with screw rod 10 and drives motor 11 bottom described workbench 7.
Described crossbeam 2 is made up of the material of following parts by weight proportioning, including 45 parts of carbon fiber, 8 parts of asbestos, polypropylene fibre
Tie up 15 parts, polyvinyl chloride fibre 10 parts, polyimide fiber 5 parts, tetrafluoro-hexafluoroethylene copolymer fiber 3 parts, three oxidation two
10 parts of antimony, 9 parts of magnesium hydroxide, aluminium hydroxide 5 parts, butyl rubber 6 parts, silicone 14 parts, white carbon black 9 parts, stearic acid file 10 parts, tristearin
4 parts of aluminum of acid, phosphorous vinegar titanium dioxide 2 parts and Firebrake ZB 5 parts.
Described screw rod 10 is in transmission connection with driving motor 11.
Described screw rod 10 is in transmission connection with workbench 7.
Described spring 8 is compression spring.
Bottom described fuselage 1, leg 12 is installed.
Described leg 12 is provided with more than one.
Described carbon fiber is carbon nano-fiber.
Described butyl rubber is through being ground into 20 mesh powder.
The preparation method of a kind of crossbeam 2, comprises the following steps:
1) by 45 parts of carbon fiber, 8 parts of asbestos, polypropylene fibre 15 parts, polyvinyl chloride fibre 10 parts, polyimide fiber 5
In part, tetrafluoro-hexafluoroethylene copolymer fiber 3 parts and 10 parts of input drying baker of antimony oxide, temperature is kept to be 45-50 DEG C
It is dried 3-5 hour, standby；
2) by step 1) raw material of gained puts in reactor, and temperature regulates to 2800-295 DEG C, and speed of agitator is
3500-3800r/min, reacts 20-25 minute, standby；
3) by 9 parts of magnesium hydroxide, aluminium hydroxide 5 parts, butyl rubber 6 parts, silicone 14 parts, white carbon black 9 parts, stearic acid file 10
Part, aluminium stearate 4 parts, phosphorous vinegar titanium dioxide 2 parts and Firebrake ZB 5 parts are put in heating tank, carry out 55-65 DEG C of preheating 3
Minute, standby；
4) by step 3) gained raw material puts in blender, and holding rotating speed is 2000-2200r/min, and stirring 15-20 divides
Clock, mix homogeneously, standby；
5) by step 2) gained raw material and step 4) raw material puts in high-temperature heating case, is heated to 300-320 DEG C, standby
With；
6) by step 5) gained material injecting mould is shaped, die sinking after natural cooling, obtain blank, standby；
7) to step 6) gained blank carries out bore operation, carries out sanding and polishing operation the most again, obtains semi-finished product, standby
With；
8) in step 7) carry out nickel plating process on gained semi-finished product,.
Experimental example:
Choose the crossbeam of common crossbeam and import compared with the crossbeam of the present invention, and according to comprcssive strength, elongation percentage
With flame retardant effect foundation as a comparison, analyze the situation of three groups of crossbeams, and draw best crossbeam.
With common crossbeam be matched group one, the crossbeam of import be matched group two and the present invention crossbeam as experimental group, tool
Volume data is as shown in the table:
Contrasting three groups of materials, the crossbeam effect obtaining the present invention is best, comprcssive strength compared with two groups of matched groups, elongation percentage
Better with flame retardant effect.
The invention has the beneficial effects as follows: the turret head of setting easily carries out tool changing operation, keep work efficiency high；Arrange
Being provided with screw rod bottom workbench and drive motor, can be regulated the position of workbench by screw rod, holding position is easy to adjust；
The carbon fiber added in the raw material of the crossbeam arranged keeps structural strength high, lightweight；The antimony oxide of interpolation, hydrogen in crossbeam
Magnesium oxide and aluminium hydroxide keep good flame retardation effect；Stearic acid file, aluminium stearate and the phosphorous vinegar added in the crossbeam arranged
Titanium dioxide keeps structural elongation high.
The above, the only detailed description of the invention of the present invention, but protection scope of the present invention is not limited thereto, and any
The change expected without creative work or replacement, all should contain and be as the criterion at scope.
Claims (9)
1. a drilling-tapping machine, it is characterised in that: including fuselage, crossbeam, driving motor and turret head, described crossbeam is located at machine
With, described crossbeam is fixing with fuselage to be connected, and described driving motor is arranged on crossbeam, before described turret head is arranged on crossbeam
End, described turret head is hinged with crossbeam, and described fuselage side is provided with drilling equipment and tapping device, described drilling equipment and merit
Tooth device is fixing with fuselage respectively to be connected, and described fuselage bottom is provided with workbench, and described workbench is connected with sliding machine body, institute
Stating turret head side and be provided with spring, described spring end is provided with hook, and described spring is connected with crossbeam by hook, described
Screw rod is installed bottom workbench and drives motor.
2. drilling-tapping machine as claimed in claim 2, it is characterised in that: described crossbeam is by the material of following parts by weight proportioning
Make, including carbon fiber 45-50 part, asbestos 7-8 part, polypropylene fibre 10-15 part, polyvinyl chloride fibre 6-10 part, polyamides Asia
Amine fiber 3-5 part, tetrafluoro-hexafluoroethylene copolymer fiber 1-3 part, antimony oxide 8-10 part, magnesium hydroxide 5-9 part, hydrogen
Aluminium oxide 3-5 part, butyl rubber 3-6 part, silicone 10-14 part, white carbon black 7-9 part, stearic acid file 8-10 part, aluminium stearate 2-4 part,
Phosphorous vinegar titanium dioxide 1-2 part and Firebrake ZB 2-5 part.
3. drilling-tapping machine as claimed in claim 3, it is characterised in that: described screw rod is connected with driving motor-driven.
4. drilling-tapping machine as claimed in claim 4, it is characterised in that: described screw rod is connected with table drive.
5. drilling-tapping machine as claimed in claim 5, it is characterised in that: described spring is compression spring.
6. drilling-tapping machine as claimed in claim 6, it is characterised in that: described fuselage bottom is provided with leg.
7. drilling-tapping machine as claimed in claim 7, it is characterised in that: described leg is provided with more than one.
8. drilling-tapping machine as claimed in claim 8, it is characterised in that: described carbon fiber is carbon nano-fiber.
9. drilling-tapping machine as claimed in claim 9, it is characterised in that: described butyl rubber is through being ground into 20 mesh powder.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610788960.8A CN106217046A (en) | 2016-08-31 | 2016-08-31 | A kind of drilling-tapping machine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610788960.8A CN106217046A (en) | 2016-08-31 | 2016-08-31 | A kind of drilling-tapping machine |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106217046A true CN106217046A (en) | 2016-12-14 |
Family
ID=58073711
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610788960.8A Pending CN106217046A (en) | 2016-08-31 | 2016-08-31 | A kind of drilling-tapping machine |
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| CN (1) | CN106217046A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106425481A (en) * | 2016-11-24 | 2017-02-22 | 东台市苏中电工机械有限公司 | Rail drilling and tapping machine |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB1111497A (en) * | 1966-04-29 | 1968-04-24 | Motch Merryweather Machinery | Automatic tool change arrangement |
| CN203236270U (en) * | 2013-03-06 | 2013-10-16 | 陈妍华 | Machine tool tool-changer with buffering effect |
| CN203266288U (en) * | 2013-05-20 | 2013-11-06 | 东莞市乔锋机械有限公司 | Vertical type metal machining central machine capable of replacing cutters synchronously |
| CN203765290U (en) * | 2013-11-25 | 2014-08-13 | 许昌汉诺威自动化有限公司 | Automatic rotary table multi-station drilling tapping machine |
| CN203918597U (en) * | 2014-04-25 | 2014-11-05 | 李良平 | High-speed high-precision drilling-tapping machine |
| CN104511779A (en) * | 2013-09-26 | 2015-04-15 | 发那科株式会社 | Tool changer equipped with covers |
| CN105623196A (en) * | 2016-03-22 | 2016-06-01 | 苏州捷德瑞精密机械有限公司 | Composite material of metal cutting machine tool and preparation method for composite material |
-
2016
- 2016-08-31 CN CN201610788960.8A patent/CN106217046A/en active Pending
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB1111497A (en) * | 1966-04-29 | 1968-04-24 | Motch Merryweather Machinery | Automatic tool change arrangement |
| CN203236270U (en) * | 2013-03-06 | 2013-10-16 | 陈妍华 | Machine tool tool-changer with buffering effect |
| CN203266288U (en) * | 2013-05-20 | 2013-11-06 | 东莞市乔锋机械有限公司 | Vertical type metal machining central machine capable of replacing cutters synchronously |
| CN104511779A (en) * | 2013-09-26 | 2015-04-15 | 发那科株式会社 | Tool changer equipped with covers |
| CN203765290U (en) * | 2013-11-25 | 2014-08-13 | 许昌汉诺威自动化有限公司 | Automatic rotary table multi-station drilling tapping machine |
| CN203918597U (en) * | 2014-04-25 | 2014-11-05 | 李良平 | High-speed high-precision drilling-tapping machine |
| CN105623196A (en) * | 2016-03-22 | 2016-06-01 | 苏州捷德瑞精密机械有限公司 | Composite material of metal cutting machine tool and preparation method for composite material |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106425481A (en) * | 2016-11-24 | 2017-02-22 | 东台市苏中电工机械有限公司 | Rail drilling and tapping machine |
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Application publication date: 20161214 |