CN105234757A - End face grinding device - Google Patents
End face grinding device Download PDFInfo
- Publication number
- CN105234757A CN105234757A CN201410323233.5A CN201410323233A CN105234757A CN 105234757 A CN105234757 A CN 105234757A CN 201410323233 A CN201410323233 A CN 201410323233A CN 105234757 A CN105234757 A CN 105234757A
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- China
- Prior art keywords
- dovetail guide
- guide base
- gas
- index dial
- face
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- Finish Polishing, Edge Sharpening, And Grinding By Specific Grinding Devices (AREA)
Abstract
The invention belongs to the field of machining of composite materials and provides an end face grinding device. The end face grinding device comprises a speed reducer (04) and a dovetail guide rail base (11). The interior of the speed reducer (04) is connected with a rotary connecting rod (09) through a gear. The rotary connecting rod (09) is driven to rotate by rotating a rocker of the speed reducer (04). The rotary connecting rod (09) is sleeved with a dividing plate (08), and the dividing plate (08) and the rotary connecting rod (09) rotate coaxially. A long groove is formed in the surface of the left side of the dividing plate (08) in the radial direction. A small support (10) is screwed in the long groove in the surface of the left side of the dividing plate (08) through a bolt, and the portion, connected with the dividing plate (08) in a screwed mode, of the small support (10) can move along the long groove. The dovetail guide rail base (11) is connected to the upper surface of the small support (10) in a screwed mode. A dovetail guide rail (02) is located on the dovetail guide rail base (11) and can move leftwards and rightwards on the dovetail guide rail base (11).
Description
Technical field
The invention belongs to multiple material manufacture field, relate to a kind of face grinding device.
Background technology
Existing aircraft product is in Butt Assembling process, need to carry out repair grinding to the production breakdown interface of aircraft components, in process, in workman's repair grinding process, because aircraft Product Process parting surface size is larger, the flatness that product support face is higher can not be ensured, and have influence on the assembly precision of aircraft components.Hand grinding is wasted time and energy, thus have impact on transporation by plane precision, have impact on the transporation by plane degree of accuracy, adds manufacturing cost.
Summary of the invention
The technical problem to be solved in the present invention: provide a kind of face grinding device, can improve grinding accuracy, ensures transporation by plane precision, reduces manufacturing cost.
Technical scheme of the present invention: a kind of face grinding device, comprising:
Decelerator [04] inside is connected with adapting rod [09] by gear, rotating decelerator [04] rocking bar drives adapting rod [09] to rotate, index dial [08] is enclosed within adapting rod [09] and adapting rod [09] coaxial rotation, index dial [08] left-hand face radially has elongated slot, little bearing [10] is by bolt spiral shell on the elongated slot of index dial [08] left-hand face, and the position that is spirally connected of little bearing [10] and index dial [08] can be moved along elongated slot, dovetail guide base [11] is screwed onto the upper surface of little bearing [10], dovetail guide [02] is positioned on dovetail guide base [11], and dovetail guide [02] can move left and right on dovetail guide base [11], air motor [03] is set on dovetail guide [02], air motor [03] left side is connected with adapter [01], adapter [01] assembling emery wheel carries out grinding to workpiece end face, little bearing [10] is passed by pipeline in air motor [03] right side, index dial [08], decelerator [04], be connected with pneumatic triple piece [06] left side outlet, pneumatic triple piece [06] right hand inlet port is connected with source of the gas by connecing mouth [05], gas from source of the gas is transferred to air motor [03] after pneumatic triple piece [06] decompression, air motor [03] drives adapter [01] to rotate under the promotion of source of the gas gas, decelerator [04] and pneumatic triple piece [06] are placed on large bearing [07], and large bearing [07] is Height Adjustable.
Further, dovetail guide [02] bottom has the through screwed hole in left and right, a stay bolt is through dovetail guide base [11], with the screw hole of dovetail guide [02] bottom, stay bolt rotates and drives dovetail guide [02] dovetail guide base [11] side-to-side movement relatively.
Concrete, dovetail guide base [11] side has screwed hole, a caging bolt is screwed onto in the screwed hole of dovetail guide base [11], and caging bolt front end withstands on dovetail guide [02] bottom sides restriction dovetail guide [02] dovetail guide base [11] motion relatively.
Beneficial effect of the present invention:
(1) pre-determined bit state: be connected by the fixture of adapting rod [09] with location aircraft components, is used for ensureing that adapting rod [09] and aircraft product axis have higher concentricity.Adjust the relative position of little bearing [10] and index dial [08], and then the radius of gyration of the relative adapting rod [09] of adjustment adapter [01], adjust the position of required grinding.(2) grinding state, source of the gas common for workshop is connected to mouth [05], source of the gas is sent to gas motor [03] by pneumatic triple piece [06] by there being the gas of pressure, motor [03] of taking offence is with to rotate, [01] is provided with emery wheel to adapter, and this is also the main tool of aircraft end face being carried out to grinding.By constantly regulating dovetail guide [02] to adjust the amount of feeding of wheel grinding with the relative position of dovetail guide base [11], after adjusting the amount of feeding, by locked for dovetail guide [02], thus certain amount of feeding can be ensure that.By shake decelerator [04], drive index dial [08] to rotate, thus make emery wheel carry out uniform rotation along aircraft product axis, grinding is carried out to product support face.
After innovation, patent of the present invention have employed a kind of end face mill apparatus, can solve because aircraft Product Process parting surface size is larger, the flatness problems with respect that product support face is higher can not be ensured, ensure that the flatness of product end surface, improve transporation by plane precision, improve the transporation by plane degree of accuracy, decrease manufacturing cost, improve production efficiency.And can Reusability, simultaneously laborsaving, and efficiently.
Accompanying drawing explanation
Fig. 1 is a kind of face grinding device schematic diagram of patent of the present invention.
Fig. 2 is the dovetail guide [02] of patent of the present invention and dovetail guide base [11] syndeton sectional view.
Fig. 3 is B-B face sectional view in Fig. 2.
Detailed description of the invention
The invention provides a kind of face grinding device, as shown in Figure 1, comprising:
Decelerator [04] inside is connected with adapting rod [09] by gear, rotating decelerator [04] rocking bar drives adapting rod [09] to rotate, index dial [08] is enclosed within adapting rod [09] and adapting rod [09] coaxial rotation, index dial [08] left-hand face radially has elongated slot, little bearing [10] is by bolt spiral shell on the elongated slot of index dial [08] left-hand face, and the position that is spirally connected of little bearing [10] and index dial [08] can be moved along elongated slot, dovetail guide base [11] is screwed onto the upper surface of little bearing [10], dovetail guide [02] is positioned on dovetail guide base [11], and dovetail guide [02] can move left and right on dovetail guide base [11], air motor [03] is set on dovetail guide [02], air motor [03] left side is connected with adapter [01], adapter [01] assembling emery wheel carries out grinding to workpiece end face, little bearing [10] is passed by pipeline in air motor [03] right side, index dial [08], decelerator [04], be connected with pneumatic triple piece [06] left side outlet, pneumatic triple piece [06] right hand inlet port is connected with source of the gas by connecing mouth [05], gas from source of the gas is transferred to air motor [03] after pneumatic triple piece [06] decompression, air motor [03] drives adapter [01] to rotate under the promotion of source of the gas gas, decelerator [04] and pneumatic triple piece [06] are placed on large bearing [07], and large bearing [07] is Height Adjustable.
Further, as shown in Figure 2, dovetail guide [02] bottom has the through screwed hole in left and right, a stay bolt is through dovetail guide base [11], with the screw hole of dovetail guide [02] bottom, stay bolt rotates and drives dovetail guide [02] dovetail guide base [11] side-to-side movement relatively.
Concrete, as shown in Figure 3, dovetail guide base [11] side has screwed hole, a caging bolt is screwed onto in the screwed hole of dovetail guide base [11], and caging bolt front end withstands on dovetail guide [02] bottom sides restriction dovetail guide [02] dovetail guide base [11] motion relatively.
Detailed description of the invention is (1) pre-determined bit state: be connected by the fixture of adapting rod [09] with location aircraft components, is used for ensureing that adapting rod [09] and aircraft product axis have higher concentricity.Adjust the relative position of little bearing [10] and index dial [08], and then the radius of gyration of the relative adapting rod [09] of adjustment adapter [01], adjust the position of required grinding.(2) grinding state, source of the gas common for workshop is connected to mouth [05], source of the gas is sent to gas motor [03] by pneumatic triple piece [06] by there being the gas of pressure, motor [03] of taking offence is with to rotate, [01] is provided with emery wheel to adapter, and this is also the main tool of aircraft end face being carried out to grinding.By constantly regulating dovetail guide [02] to adjust the amount of feeding of wheel grinding with the relative position of dovetail guide base [11], after adjusting the amount of feeding, by locked for dovetail guide [02], thus certain amount of feeding can be ensure that.By shake decelerator [04], drive index dial [08] to rotate, thus make emery wheel carry out uniform rotation along aircraft product axis, grinding is carried out to product support face.
Patent of the present invention have employed a kind of end face mill apparatus, can solve because aircraft Product Process parting surface size is larger, the flatness problems with respect that product support face is higher can not be ensured, ensure that the flatness of product end surface, improve transporation by plane precision, improve the transporation by plane degree of accuracy, decrease manufacturing cost, improve production efficiency.And can Reusability, simultaneously laborsaving, and efficiently.
Claims (3)
1. a face grinding device, is characterized in that, comprising:
Decelerator [04] inside is connected with adapting rod [09] by gear, rotating decelerator [04] rocking bar drives adapting rod [09] to rotate, index dial [08] is enclosed within adapting rod [09] and adapting rod [09] coaxial rotation, index dial [08] left-hand face radially has elongated slot, little bearing [10] is by bolt spiral shell on the elongated slot of index dial [08] left-hand face, and the position that is spirally connected of little bearing [10] and index dial [08] can be moved along elongated slot, dovetail guide base [11] is screwed onto the upper surface of little bearing [10], dovetail guide [02] is positioned on dovetail guide base [11], and dovetail guide [02] can move left and right on dovetail guide base [11], air motor [03] is set on dovetail guide [02], air motor [03] left side is connected with adapter [01], adapter [01] assembling emery wheel carries out grinding to workpiece end face, little bearing [10] is passed by pipeline in air motor [03] right side, index dial [08], decelerator [04], be connected with pneumatic triple piece [06] left side outlet, pneumatic triple piece [06] right hand inlet port is connected with source of the gas by connecing mouth [05], gas from source of the gas is transferred to air motor [03] after pneumatic triple piece [06] decompression, air motor [03] drives adapter [01] to rotate under the promotion of source of the gas gas, decelerator [04] and pneumatic triple piece [06] are placed on large bearing [07], and large bearing [07] is Height Adjustable.
2. a kind of face grinding device as claimed in claim 1, it is characterized in that, dovetail guide [02] bottom has the through screwed hole in left and right, a stay bolt is through dovetail guide base [11], with the screw hole of dovetail guide [02] bottom, stay bolt rotates and drives dovetail guide [02] dovetail guide base [11] side-to-side movement relatively.
3. a kind of face grinding device as claimed in claim 2, it is characterized in that, dovetail guide base [11] side has screwed hole, a caging bolt is screwed onto in the screwed hole of dovetail guide base [11], and caging bolt front end withstands on dovetail guide [02] bottom sides restriction dovetail guide [02] dovetail guide base [11] motion relatively.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410323233.5A CN105234757B (en) | 2014-07-08 | 2014-07-08 | A kind of face grinding device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410323233.5A CN105234757B (en) | 2014-07-08 | 2014-07-08 | A kind of face grinding device |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN105234757A true CN105234757A (en) | 2016-01-13 |
| CN105234757B CN105234757B (en) | 2017-10-31 |
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ID=55032706
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201410323233.5A Active CN105234757B (en) | 2014-07-08 | 2014-07-08 | A kind of face grinding device |
Country Status (1)
| Country | Link |
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| CN (1) | CN105234757B (en) |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2085773B (en) * | 1980-10-23 | 1984-01-18 | Yeatman Reed Richard | Brake disc machining apparatus |
| CN201055963Y (en) * | 2007-01-23 | 2008-05-07 | 广州华工百川科技股份有限公司 | Tire sander |
| CN201537753U (en) * | 2009-08-21 | 2010-08-04 | 刘伟哲 | Multi-station diamond saw blade automatic edging machine |
| CN102172989A (en) * | 2010-12-31 | 2011-09-07 | 武汉奥新科技有限公司 | Turning device for processing standard ceramic ferrule |
-
2014
- 2014-07-08 CN CN201410323233.5A patent/CN105234757B/en active Active
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2085773B (en) * | 1980-10-23 | 1984-01-18 | Yeatman Reed Richard | Brake disc machining apparatus |
| CN201055963Y (en) * | 2007-01-23 | 2008-05-07 | 广州华工百川科技股份有限公司 | Tire sander |
| CN201537753U (en) * | 2009-08-21 | 2010-08-04 | 刘伟哲 | Multi-station diamond saw blade automatic edging machine |
| CN102172989A (en) * | 2010-12-31 | 2011-09-07 | 武汉奥新科技有限公司 | Turning device for processing standard ceramic ferrule |
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| Publication number | Publication date |
|---|---|
| CN105234757B (en) | 2017-10-31 |
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