CN106403610A - Separating preventing hard alloy maintenance tool - Google Patents

Separating preventing hard alloy maintenance tool Download PDF

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Publication number
CN106403610A
CN106403610A CN201611008650.6A CN201611008650A CN106403610A CN 106403610 A CN106403610 A CN 106403610A CN 201611008650 A CN201611008650 A CN 201611008650A CN 106403610 A CN106403610 A CN 106403610A
Authority
CN
China
Prior art keywords
base metal
main body
metal main
maintenance tool
hard alloy
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.)
Granted
Application number
CN201611008650.6A
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Chinese (zh)
Other versions
CN106403610B (en
Inventor
连新兰
杨京广
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.)
Nantong Mengding New Materials Co., Ltd.
Original Assignee
Henan Guangdu Superhard Material Co Ltd
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Henan Guangdu Superhard Material Co Ltd filed Critical Henan Guangdu Superhard Material Co Ltd
Priority to CN201611008650.6A priority Critical patent/CN106403610B/en
Priority to CN201810541186.XA priority patent/CN108680023B/en
Priority to CN201810542797.6A priority patent/CN108917407B/en
Priority to CN201810541189.3A priority patent/CN108895840B/en
Priority to CN201810571817.2A priority patent/CN109028959B/en
Publication of CN106403610A publication Critical patent/CN106403610A/en
Application granted granted Critical
Publication of CN106403610B publication Critical patent/CN106403610B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F27FURNACES; KILNS; OVENS; RETORTS
    • F27DDETAILS OR ACCESSORIES OF FURNACES, KILNS, OVENS, OR RETORTS, IN SO FAR AS THEY ARE OF KINDS OCCURRING IN MORE THAN ONE KIND OF FURNACE
    • F27D1/00Casings; Linings; Walls; Roofs
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F27FURNACES; KILNS; OVENS; RETORTS
    • F27DDETAILS OR ACCESSORIES OF FURNACES, KILNS, OVENS, OR RETORTS, IN SO FAR AS THEY ARE OF KINDS OCCURRING IN MORE THAN ONE KIND OF FURNACE
    • F27D7/00Forming, maintaining, or circulating atmospheres in heating chambers

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Insertion Pins And Rivets (AREA)
  • Manufacture And Refinement Of Metals (AREA)
  • Carbon Steel Or Casting Steel Manufacturing (AREA)

Abstract

The invention relates to the field of hardware tools, in particular to a separating preventing hard alloy maintenance tool. The separating preventing hard alloy maintenance tool comprises a communicating rod, a base metal main body, an inclined surface, penetration mounting holes and alloy components; the lower part of the communicating rod is connected with the base metal main body; the inclined surface is arranged at the edge of the upper part of the base metal main body; the penetration mounting holes are formed in the inclined surface; the alloy components are embedded into the penetration mounting holes; each alloy component comprises a hollow sleeve, a super-hard core body and a connecting shaft assembly; each super-hard core body is arranged in the corresponding hollow sleeve in a sleeving manner and is fixedly connected with the corresponding connecting shaft assembly. According to the separating preventing hard alloy maintenance tool, through the arrangement of the penetration mounting holes and the hollow sleeves, the super-hard core bodies can be subjected to dual protection, and the problem of separating of the super-hard core bodies caused by the difference of thermal expansion coefficients is prevented; through the arrangement of the inclined surface, direct impact pressure in a furnace is favourably transferred to one side so as to reduce a pressure coefficient.

Description

Anti-detachment hard alloy maintenance tool
Technical field
The invention belongs to maintenance tool technical field, more particularly, to anti-detachment hard alloy maintenance tool.
Background technology
High temperature furnace in actual use because in-furnace temperature maintains high point for a long time so that stove internal gas pressure raise, Need interruption that body of heater is carried out with blood pressure lowering process, existing technical scheme typically adopts the good sintered-carbide tool pair of resistance to elevated temperatures It is safeguarded, hard alloy is less than the thermal coefficient of expansion of body of heater main body due to thermal coefficient of expansion, easily causes sintered-carbide tool and takes off The problem falling, it is poor that existing hard alloy maintenance tool has a stablizing effect, caducous problem.
Therefore, invent a kind of anti-detachment hard alloy maintenance tool and seem very necessary.
Content of the invention
In order to solve above-mentioned technical problem, the present invention provides anti-detachment hard alloy maintenance tool, existing hard to solve Matter alloy maintenance tool stablizing effect is poor, caducous problem.
In order to achieve the above object, the present invention employs the following technical solutions.
Anti-detachment hard alloy maintenance tool, including ditch through rod, base metal main body, inclined plane, infiltration installing hole and alloy Assembly, described ditch through rod connects base metal main body in bottom;Described inclined plane is arranged on the top edge of base metal main body; Described infiltration installing hole is arranged in inclined plane;Described alloy components embed inside infiltration installing hole;Described alloy group Part includes hollow sleeve, superhard core body and connect axle assembly, described superhard core body be socketed in hollow sleeve internal and be connected Axle assembly is fixedly connected.
Described inclined plane is specifically located at the upper plane outer rim of base metal main body;Described inclination mask body and base metal The upper plane of main body is in 45° angle, is easy to alloy components and the installation of superhard core body, avoids pressure directly to make straight up simultaneously For superhard core body, be conducive to the stability of superhard core body.
Described base metal main body adopts circular or oval one kind, is conducive to the surface smoothness of inclined plane.
Described alloy components are fixed in base metal main body especially by infiltration installing hole;Described alloy components adopt Multiple, it is to avoid pressure directly acts on superhard core body, reach the effect reducing pressure in advance.
After described superhard core body is inserted vertically into hollow sleeve, it is fixedly connected in cross with being connected axle assembly, further Be conducive to the positional stability of superhard core body.
The present invention has the advantages that:Because the anti-detachment hard alloy maintenance tool of the present invention is widely used in tieing up Shield technical field of tools.Meanwhile, beneficial effects of the present invention are:
1st, the setting of inclined plane of the present invention, has and shifts to side using by flinging pressure in stove, reduce pressure coefficient.
2nd, the present invention permeates the setting of installing hole and hollow sleeve, be conducive to dual superhard core body is protected, prevent The problem that comes off that superhard core body is led to due to thermal expansion coefficient difference.
3rd, the present invention connects being equipped with of axle assembly and patchhole, is conducive to vertical applying direction to superhard core body and taking off Power, prevents coming off of superhard core body.
Brief description
Fig. 1 is the structural representation of the present invention.
Fig. 2 is the cross-sectional structure schematic diagram of the present invention.
Fig. 3 is the alloy components structural representation of the present invention.
Fig. 4 is the patchhole structural representation of the present invention.
In figure:
1- ditch through rod, 2- base metal main body, 3- inclined plane, 4- permeates installing hole, 5- alloy components, 51- hollow sleeve, and 52- surpasses Hard core body, 53- connects axle assembly, 6- patchhole, the upper plane of 7-.
Specific embodiment
Below in conjunction with drawings and Examples, the present invention is described further:
The embodiment of the present invention:
As shown in accompanying drawing 1 is to accompanying drawing 3
The present invention provides anti-detachment hard alloy maintenance tool, and including ditch through rod 1, base metal main body 2, inclined plane 3, infiltration is installed Hole 4 and alloy components 5, described ditch through rod 1 connects base metal main body 2 in bottom;Described inclined plane 3 is arranged on base metal master The top edge of body 2;Described infiltration installing hole 4 is arranged in inclined plane 3;Described alloy components 5 embed infiltration installing hole 4 Internal;Described alloy components 5 include hollow sleeve 51, superhard core body 52 and connect axle assembly 53, described superhard core body 52 It is socketed in hollow sleeve 51 inside and be fixedly connected with being connected axle assembly 53.
Described inclined plane 3 is specifically located at upper plane 7 outer rim of base metal main body 2;Described inclined plane 3 is concrete and low-priced The upper plane 7 of metal master 2 is in 45° angle, is easy to alloy components 5 and the installation of superhard core body 52, avoids pressure vertical simultaneously Directly act on superhard core body 52 upwards, be conducive to the stability of superhard core body 52.
Described base metal main body 2 adopts circular or oval one kind, is conducive to the surface smoothness of inclined plane 3.
Described alloy components 5 are fixed in base metal main body 2 especially by infiltration installing hole 4;Described alloy components 5 Using multiple, it is to avoid pressure directly acts on superhard core body 52, reach the effect reducing pressure in advance.
After described superhard core body 52 is inserted vertically into hollow sleeve 51, it is fixedly connected in cross with being connected axle assembly 53, Be conducive to the positional stability of superhard core body 52 further.
Patchhole constructive embodiment:
As shown in Figure 4
The present invention can also arrange patchhole 6 in base metal main body 2;Described patchhole 6 and inclined plane 3 be arranged in parallel, and Fixing described connection axle assembly 53 internally, connects axle assembly 53 and is fixedly connected described superhard core body 52, desirably prevent The disengaging of superhard core body 52.
Described patchhole 6 can be provided separately within the side connecting axle assembly 53 or be simultaneously located at connection axle assembly 53 Both sides.
In use, high temperature furnace internal pressure acts on infiltration by inclined plane 3 and fixes by installing in the hole the present invention On the alloy components 5 installed, after the stress impairs of alloy components 5, reach at superhard core body 52, superhard core body 52 is in bottom On fixing assembly in this connection, drive connection axle assembly 53 to move out simultaneously, be now inserted in the connecting shaft within patchhole 6 Assembly 53 relies on patchhole 6 to be applied to the inside counteracting force of superhard core body 52, prevents superhard core body 52 from coming off.
Using technical solutions according to the invention, or those skilled in the art is under the inspiration of technical solution of the present invention, Design similar technical scheme, and reach above-mentioned technique effect, all fall into protection scope of the present invention.

Claims (5)

1. anti-detachment hard alloy maintenance tool is it is characterised in that it includes ditch through rod(1), base metal main body(2), inclined plane (3), permeate installing hole(4)And alloy components(5), described ditch through rod(1)Connect base metal main body in bottom(2);Described Inclined plane(3)It is arranged on base metal main body(2)Top edge;Described infiltration installing hole(4)It is arranged on inclined plane(3)On; Described alloy components(5)Embedded infiltration installing hole(4)Internal;Described alloy components(5)Including hollow sleeve(51), superhard Core body(52)With connection axle assembly(53), described superhard core body(52)It is socketed in hollow sleeve(51)Internal and total with connecting shaft Become(53)It is fixedly connected.
2. as claimed in claim 1 anti-detachment hard alloy maintenance tool it is characterised in that described inclined plane(3)Specifically It is arranged on base metal main body(2)Upper plane(7)Outer rim;Described inclined plane(3)Concrete and base metal main body(2)Upper plane (7)In 45° angle.
3. as claimed in claim 1 anti-detachment hard alloy maintenance tool it is characterised in that described base metal main body(2) Using circular or oval one kind.
4. as claimed in claim 1 anti-detachment hard alloy maintenance tool it is characterised in that described alloy components(5)Tool Body passes through to permeate installing hole(4)It is fixed on base metal main body(2)On;Described alloy components(5)Using multiple.
5. as claimed in claim 1 anti-detachment hard alloy maintenance tool it is characterised in that described superhard core body(52)Perpendicular Straight cutting enters hollow sleeve(51)Afterwards, be connected axle assembly(53)It is fixedly connected in cross.
CN201611008650.6A 2016-11-16 2016-11-16 Anti-detachment hard alloy maintenance tool Active CN106403610B (en)

Priority Applications (5)

Application Number Priority Date Filing Date Title
CN201611008650.6A CN106403610B (en) 2016-11-16 2016-11-16 Anti-detachment hard alloy maintenance tool
CN201810541186.XA CN108680023B (en) 2016-11-16 2016-11-16 High temperature furnace used anti-detachment hard alloy maintenance tool
CN201810542797.6A CN108917407B (en) 2016-11-16 2016-11-16 Anti-detachment hard alloy maintenance tool
CN201810541189.3A CN108895840B (en) 2016-11-16 2016-11-16 Anti-separation hard alloy maintenance tool for high-temperature furnace
CN201810571817.2A CN109028959B (en) 2016-11-16 2016-11-16 A kind of anti-detachment hard alloy maintenance tool

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201611008650.6A CN106403610B (en) 2016-11-16 2016-11-16 Anti-detachment hard alloy maintenance tool

Related Child Applications (4)

Application Number Title Priority Date Filing Date
CN201810542797.6A Division CN108917407B (en) 2016-11-16 2016-11-16 Anti-detachment hard alloy maintenance tool
CN201810541189.3A Division CN108895840B (en) 2016-11-16 2016-11-16 Anti-separation hard alloy maintenance tool for high-temperature furnace
CN201810571817.2A Division CN109028959B (en) 2016-11-16 2016-11-16 A kind of anti-detachment hard alloy maintenance tool
CN201810541186.XA Division CN108680023B (en) 2016-11-16 2016-11-16 High temperature furnace used anti-detachment hard alloy maintenance tool

Publications (2)

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CN106403610A true CN106403610A (en) 2017-02-15
CN106403610B CN106403610B (en) 2018-06-19

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CN201810541186.XA Active CN108680023B (en) 2016-11-16 2016-11-16 High temperature furnace used anti-detachment hard alloy maintenance tool
CN201810541189.3A Active CN108895840B (en) 2016-11-16 2016-11-16 Anti-separation hard alloy maintenance tool for high-temperature furnace
CN201611008650.6A Active CN106403610B (en) 2016-11-16 2016-11-16 Anti-detachment hard alloy maintenance tool
CN201810571817.2A Active CN109028959B (en) 2016-11-16 2016-11-16 A kind of anti-detachment hard alloy maintenance tool
CN201810542797.6A Active CN108917407B (en) 2016-11-16 2016-11-16 Anti-detachment hard alloy maintenance tool

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CN201810541186.XA Active CN108680023B (en) 2016-11-16 2016-11-16 High temperature furnace used anti-detachment hard alloy maintenance tool
CN201810541189.3A Active CN108895840B (en) 2016-11-16 2016-11-16 Anti-separation hard alloy maintenance tool for high-temperature furnace

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CN201810571817.2A Active CN109028959B (en) 2016-11-16 2016-11-16 A kind of anti-detachment hard alloy maintenance tool
CN201810542797.6A Active CN108917407B (en) 2016-11-16 2016-11-16 Anti-detachment hard alloy maintenance tool

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Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6143055A (en) * 1997-06-26 2000-11-07 Eckert; C. Edward Carbon based composite material for molten metal
US20040025340A1 (en) * 2002-07-16 2004-02-12 Tsuyoshi Kubota Fracture split method for connecting rod
US20110100979A1 (en) * 2009-11-04 2011-05-05 Chi-Wah Keong Manufacturing method for rod member of three-dimensional statically indeterminate truss structure
CN203130734U (en) * 2013-02-24 2013-08-14 于浩 Exhausting bolt for boiler
CN103437442A (en) * 2013-08-07 2013-12-11 江苏爵格工业设备有限公司 Pressure relief device
JP2015164723A (en) * 2015-04-03 2015-09-17 住友金属鉱山株式会社 lining structure
CN206177017U (en) * 2016-11-16 2017-05-17 河南广度超硬材料有限公司 Anticreep is from carbide maintenance tool

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP5729421B2 (en) * 2013-06-18 2015-06-03 住友金属鉱山株式会社 Lining structure

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6143055A (en) * 1997-06-26 2000-11-07 Eckert; C. Edward Carbon based composite material for molten metal
US20040025340A1 (en) * 2002-07-16 2004-02-12 Tsuyoshi Kubota Fracture split method for connecting rod
US20110100979A1 (en) * 2009-11-04 2011-05-05 Chi-Wah Keong Manufacturing method for rod member of three-dimensional statically indeterminate truss structure
CN203130734U (en) * 2013-02-24 2013-08-14 于浩 Exhausting bolt for boiler
CN103437442A (en) * 2013-08-07 2013-12-11 江苏爵格工业设备有限公司 Pressure relief device
JP2015164723A (en) * 2015-04-03 2015-09-17 住友金属鉱山株式会社 lining structure
CN206177017U (en) * 2016-11-16 2017-05-17 河南广度超硬材料有限公司 Anticreep is from carbide maintenance tool

Also Published As

Publication number Publication date
CN109028959A (en) 2018-12-18
CN109028959B (en) 2019-08-20
CN108917407A (en) 2018-11-30
CN108680023A (en) 2018-10-19
CN108895840B (en) 2019-08-20
CN108895840A (en) 2018-11-27
CN106403610B (en) 2018-06-19
CN108917407B (en) 2019-08-20
CN108680023B (en) 2019-08-20

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Effective date of registration: 20180517

Address after: 325600 Dong Jia village, Baishi Town, Yueqing City, Wenzhou, Zhejiang

Applicant after: Guan Wei

Address before: 450007 37 Building 14, 156 Funiu Road, Zhengzhou, Henan

Applicant before: HENAN GUANGDU SUPERHARD MATERIAL CO., LTD.

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GR01 Patent grant
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TR01 Transfer of patent right

Effective date of registration: 20190619

Address after: 226000 Xingyuan Road North, Nantong High-tech Industrial Development Zone, Jiangsu Province

Patentee after: Nantong Mengding New Materials Co., Ltd.

Address before: 325600 Dong Jia village, Baishi Town, Yueqing City, Wenzhou, Zhejiang

Patentee before: Guan Wei

TR01 Transfer of patent right