CN204277138U - A kind of engine duct special screw tap - Google Patents
A kind of engine duct special screw tap Download PDFInfo
- Publication number
- CN204277138U CN204277138U CN201420820680.7U CN201420820680U CN204277138U CN 204277138 U CN204277138 U CN 204277138U CN 201420820680 U CN201420820680 U CN 201420820680U CN 204277138 U CN204277138 U CN 204277138U
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- CN
- China
- Prior art keywords
- screw tap
- tap
- operate portions
- blade
- holder
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- 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
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Abstract
The utility model discloses a kind of engine duct special screw tap, comprise integrated screw tap operate portions, tap holder and fixing square toes, described fixing square toes are arranged on one end of described tap holder, described screw tap operate portions is arranged on the other end of described tap holder, described screw tap operate portions, the axis of described tap holder and described fixing square toes on the same line, make a circle outside described screw tap operate portions and be provided with three groups of screw tap blades uniformly, a chip area is provided with between every two adjacent groups screw tap blade, often organize described screw tap blade and be double end right-handed thread, and the degree of depth of double thread is not etc., not only resistance to overturning is good, and solve the processing problems of double end right-handed thread groove on company's engine duct endoporus hole wall, described screw tap blade front pilot length is set to 5 ± 0.5mm.The not only good and long service life of guide effect.
Description
Technical field
The utility model relates to a kind of hardware & tools, and a kind of engine duct special screw tap, belongs to Machining Technology field specifically.
Background technology
Screw tap is the common hardware & tools of a kind of field of machining, is mainly used in machining internal thread on workpiece, also claims tap.Regular tap, by fixing square toes, tap holder and screw tap operate portions, makes a circle outside described screw tap operate portions and is provided with screw tap blade uniformly, during use, just carries out tapping with screw tap blade to workpiece.And due to current screw tap blade be all the form such as spirality or single thread, and the engine duct inner hole thread that my company now will process is double end right-handed thread, and double thread is deep mixed, so the regular tap on existing market cannot meet processing needs, and existing screw tap blade front pilot Design of length is improper, some is too short easily holds moment of torsion that can't stand increasing and fractures, and service life is short, and some long not only waste of material and guide effect is bad.
Utility model content
For the problems referred to above, the problem that the utility model quasi-solution is determined be to provide a kind of rational in infrastructure, lead, long service life and the engine duct special screw tap of good stability.
For achieving the above object, the utility model is by the following technical solutions: a kind of engine duct special screw tap, comprise integrated screw tap operate portions, tap holder and fixing square toes, described fixing square toes are arranged on one end of described tap holder, described screw tap operate portions is arranged on the other end of described tap holder, described screw tap operate portions, the axis of described tap holder and described fixing square toes on the same line, make a circle outside described screw tap operate portions and be provided with three groups of screw tap blades uniformly, a chip area is provided with between every two adjacent groups screw tap blade, often organize described screw tap blade and be double end right-handed thread, and the degree of depth of double thread is not etc., described screw tap blade front pilot length is set to 5 ± 0.5mm.
As preferably, described screw tap blade front pilot length is set to 5mm.
Effective achievement of the present utility model: the utility model is rational in infrastructure, make a circle outside screw tap operate portions and be provided with three groups of screw tap blades uniformly, and screw tap blade is set to double end right-handed thread, not only resistance to overturning is good, and solves the processing problems of double end right-handed thread groove on company's engine duct endoporus hole wall; Again screw tap blade front pilot length is set to 5 ± 0.5mm, not only good the and long service life of guide effect.In sum, the utility model have rational in infrastructure, lead, long service life and the feature of good stability.
Accompanying drawing explanation
Fig. 1 is front view of the present utility model.
Fig. 2 is right view of the present utility model.
Fig. 3 is the part sectioned view of one group of screw tap blade in Fig. 1.
In figure: 1-screw tap operate portions, 2-tap holder, 3-fixes square toes, 4-screw tap blade, 5-chip area.
Detailed description of the invention
In order to make those skilled in the art person better understand the utility model scheme, below in conjunction with the accompanying drawing in the present embodiment, clear, complete description is carried out to the technical scheme in the utility model embodiment.
As Fig. 1, shown in Fig. 2 and Fig. 3, the utility model discloses a kind of engine duct special screw tap, comprise integrated screw tap operate portions 1, tap holder 2 and fixing square toes 3, fixing square toes 3 are arranged on one end of tap holder 2, screw tap operate portions 1 is arranged on the other end of tap holder 2, screw tap operate portions 1, the axis of tap holder 2 and fixing square toes 3 on the same line, make a circle outside screw tap operate portions 1 and be provided with three groups of screw tap blades 4 uniformly, a chip area 5 is provided with between every two adjacent groups screw tap blade 4, often organize screw tap blade 4 and be double end right-handed thread, and the degree of depth of double thread is not etc., screw tap blade 4 front pilot length is set to 5 ± 0.5mm.
The utility model is rational in infrastructure, make a circle outside screw tap operate portions 1 and be provided with three groups of screw tap blades 4 uniformly, and screw tap blade 4 is set to double end right-handed thread, not only resistance to overturning is good, and solves the processing problems of double end right-handed thread groove on company's engine duct endoporus hole wall; Again screw tap blade 4 front pilot length is set to 5 ± 0.5mm, not only good the and long service life of guide effect.In sum, the utility model have rational in infrastructure, lead, long service life and the feature of good stability.
Obviously, described embodiment is only a part of embodiment of the present utility model, instead of whole embodiments.Based on the embodiment in the utility model, those of ordinary skill in the art are not making the every other embodiment obtained under creative work prerequisite, all should belong to the scope of the utility model protection.
Claims (2)
1. an engine duct special screw tap, comprise integrated screw tap operate portions (1), tap holder (2) and fixing square toes (3), described fixing square toes (3) are arranged on one end of described tap holder (2), described screw tap operate portions (1) is arranged on the other end of described tap holder (2), described screw tap operate portions (1), the axis of described tap holder (2) and described fixing square toes (3) on the same line, make a circle outside described screw tap operate portions (1) and be provided with three groups of screw tap blades (4) uniformly, a chip area (5) is provided with between every two adjacent groups screw tap blade (4), it is characterized in that: often organize described screw tap blade (4) and be double end right-handed thread, and the degree of depth of double thread is not etc., described screw tap blade (4) front pilot length is set to 5 ± 0.5mm.
2. engine duct special screw tap according to claim 1, is characterized in that: described screw tap blade (4) front pilot length is set to 5mm.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201420820680.7U CN204277138U (en) | 2014-12-09 | 2014-12-09 | A kind of engine duct special screw tap |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201420820680.7U CN204277138U (en) | 2014-12-09 | 2014-12-09 | A kind of engine duct special screw tap |
Publications (1)
Publication Number | Publication Date |
---|---|
CN204277138U true CN204277138U (en) | 2015-04-22 |
Family
ID=52860334
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201420820680.7U Expired - Fee Related CN204277138U (en) | 2014-12-09 | 2014-12-09 | A kind of engine duct special screw tap |
Country Status (1)
Country | Link |
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CN (1) | CN204277138U (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN106475642A (en) * | 2016-12-21 | 2017-03-08 | 平湖市山特螺纹工具有限公司 | The screw tap of hard alloy |
-
2014
- 2014-12-09 CN CN201420820680.7U patent/CN204277138U/en not_active Expired - Fee Related
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN106475642A (en) * | 2016-12-21 | 2017-03-08 | 平湖市山特螺纹工具有限公司 | The screw tap of hard alloy |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
GR01 | Patent grant | ||
C56 | Change in the name or address of the patentee | ||
CP01 | Change in the name or title of a patent holder |
Address after: 312352 Shangyu Economic Development Zone, Zhejiang Patentee after: Shaoxing City, Shangyu Chunhui internal combustion engine fittings Company Limited Address before: 312352 Shangyu Economic Development Zone, Zhejiang Patentee before: Shangyu Internal-combustion Accessories Co., Ltd. |
|
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: 20150422 Termination date: 20181209 |