CN108588593A - A kind of High-strength drill bit matrix formula - Google Patents

A kind of High-strength drill bit matrix formula Download PDF

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Publication number
CN108588593A
CN108588593A CN201810625345.4A CN201810625345A CN108588593A CN 108588593 A CN108588593 A CN 108588593A CN 201810625345 A CN201810625345 A CN 201810625345A CN 108588593 A CN108588593 A CN 108588593A
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CN
China
Prior art keywords
parts
drill bit
graphite powder
strength
lithium stearate
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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.)
Withdrawn
Application number
CN201810625345.4A
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Chinese (zh)
Inventor
吴宏
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.)
Rugao Thousand Dragon Tools Co Ltd
Original Assignee
Rugao Thousand Dragon Tools Co Ltd
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Filing date
Publication date
Application filed by Rugao Thousand Dragon Tools Co Ltd filed Critical Rugao Thousand Dragon Tools Co Ltd
Priority to CN201810625345.4A priority Critical patent/CN108588593A/en
Publication of CN108588593A publication Critical patent/CN108588593A/en
Withdrawn legal-status Critical Current

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    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C49/00Alloys containing metallic or non-metallic fibres or filaments
    • C22C49/02Alloys containing metallic or non-metallic fibres or filaments characterised by the matrix material
    • C22C49/10Refractory metals
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C49/00Alloys containing metallic or non-metallic fibres or filaments
    • C22C49/14Alloys containing metallic or non-metallic fibres or filaments characterised by the fibres or filaments

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  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Compositions Of Macromolecular Compounds (AREA)
  • Lubricants (AREA)

Abstract

The present invention provides a kind of High-strength drill bit matrix formulas, which is characterized in that is made from the following raw materials in parts by weight:30 40 parts of iron, 10 15 parts of tungsten carbide, 20 25 parts of chromium, 10 16 parts of nickel, 35 parts of manganese, 0.3 0.5 parts of phosphorus, 10 15 parts of copper, 13 parts of nano graphite powder, 0.5 1 parts of antimony oxide, 12 parts of calcium carbonate, 1.6 1.8 parts of lithium stearate, 0.1 0.2 parts of zinc borate, 58 parts of paulownia sawdust, 5 10 parts of carbon fiber, 2.5 2.7 parts of amino silane.Formula rate and varying strength the proportioning combination of the present invention, and comprising nano graphite powder, antimony oxide, lithium stearate, zinc borate, paulownia sawdust and then determine reasonable hybrid technique system in being formulated, high strength matrix formula can be made, improve the bending resistance of drill bit, toughness and hardness performance, the case where substantially reducing drill bit chip off-falling in use and the breaking wing, improves productivity.

Description

A kind of High-strength drill bit matrix formula
Technical field
The invention belongs to bit technique fields, and in particular to a kind of High-strength drill bit matrix formula.
Background technology
Early stage combined drill is platybasic type, and shallow-water tank, for some even without sink, bit breakage is small in use, but makes It is poor with effect, and NEW TYPE OF COMPOSITE piece drill bit, it is designed as the shape of wing formula.This drill bit sink is deep, and wing is long, when drill bit uses It is efficient, long lifespan.But due to sink depth, wing is long, often occurs the case where bit matrix chip off-falling, the breaking wing in use, gives Drilling well work brings many troubles, and increases many drilling cost costs.
Invention content
Present invention aims in view of the drawbacks of the prior art and insufficient, a kind of High-strength drill bit matrix formula is provided, To solve the problems, such as proposed in background technology.
In order to solve the above technical problems, the embodiment of the present invention provides a kind of High-strength drill bit matrix formula, feature It is, is made from the following raw materials in parts by weight:30-40 parts of iron, 10-15 parts of tungsten carbide, 20-25 parts of chromium, 10-16 parts of nickel, manganese 3-5 Part, 0.3-0.5 parts of phosphorus, 10-15 parts of copper, 1-3 parts of nano graphite powder, 0.5-1 parts of antimony oxide, 1-2 parts of calcium carbonate, stearic acid 1.6-1.8 parts of lithium, 0.1-0.2 parts of zinc borate, 5-8 parts of paulownia sawdust, 5-10 parts of carbon fiber, 2.5-2.7 parts of amino silane.
Further, it is made from the following raw materials in parts by weight:32-38 parts of iron, 12-14 parts of tungsten carbide, 22-24 parts of chromium, nickel 12-14 parts, 4-5 parts of manganese, 0.4-0.5 parts of phosphorus, 12-14 parts of copper, 2-3 parts of nano graphite powder, 0.6-0.9 parts of antimony oxide, carbon Sour calcium 1.2-1.8 parts, 1.7-1.8 parts of lithium stearate, 0.14-0.17 parts of zinc borate, 6-7 parts of paulownia sawdust, 7-9 parts of carbon fiber, ammonia 2.6-2.7 parts of base silane.
Further, it is made from the following raw materials in parts by weight:35 parts of iron, 13 parts of tungsten carbide, 23 parts of chromium, 13 parts of nickel, manganese 4 Part, 0.4 part of phosphorus, 13 parts of copper, 2 parts of nano graphite powder, 0.7 part of antimony oxide, 1.5 parts of calcium carbonate, 1.7 parts of lithium stearate, boron 0.15 part of sour zinc, 6 parts of paulownia sawdust, 8 parts of carbon fiber, 2.6 parts of amino silane.
The above-mentioned technical proposal of the present invention has the beneficial effect that:The formula rate and varying strength proportioning group of the present invention It closes, and includes nano graphite powder, antimony oxide, lithium stearate, zinc borate, paulownia sawdust and then determining rationally mixing in being formulated Process system, you can make high strength matrix formula, improve the bending resistance of drill bit, toughness and hardness performance, drop significantly The case where low drill bit chip off-falling in use and the breaking wing, improve productivity.
Specific implementation mode
To keep the technical problem to be solved in the present invention, technical solution and advantage clearer, below use specific embodiment into Row detailed description.
Embodiment one
A kind of High-strength drill bit matrix formula, which is characterized in that be made from the following raw materials in parts by weight:30-40 parts of iron, 10-15 parts of tungsten carbide, 20-25 parts of chromium, 10-16 parts of nickel, 3-5 parts of manganese, 0.3-0.5 parts of phosphorus, 10-15 parts of copper, nano graphite powder 1-3 Part, 0.5-1 parts of antimony oxide, 1-2 parts of calcium carbonate, 1.6-1.8 parts of lithium stearate, 0.1-0.2 parts of zinc borate, paulownia sawdust 5-8 Part, 5-10 parts of carbon fiber, 2.5-2.7 parts of amino silane.
Embodiment two
A kind of High-strength drill bit matrix formula, which is characterized in that be made from the following raw materials in parts by weight:30-40 parts of iron, 10-15 parts of tungsten carbide, 20-25 parts of chromium, 10-16 parts of nickel, 3-5 parts of manganese, 0.3-0.5 parts of phosphorus, 10-15 parts of copper, nano graphite powder 1-3 Part, 0.5-1 parts of antimony oxide, 1-2 parts of calcium carbonate, 1.6-1.8 parts of lithium stearate, 0.1-0.2 parts of zinc borate, paulownia sawdust 5-8 Part, 5-10 parts of carbon fiber, 2.5-2.7 parts of amino silane.
Embodiment three
It is made from the following raw materials in parts by weight:35 parts of iron, 13 parts of tungsten carbide, 23 parts of chromium, 13 parts of nickel, 4 parts of manganese, 0.4 part of phosphorus, 13 parts of copper, 2 parts of nano graphite powder, 0.7 part of antimony oxide, 1.5 parts of calcium carbonate, 1.7 parts of lithium stearate, 0.15 part of zinc borate, 6 parts of paulownia sawdust, 8 parts of carbon fiber, 2.6 parts of amino silane.
The present invention formula rate and varying strength proportioning combination, and be formulated in comprising nano graphite powder, antimony oxide, Lithium stearate, zinc borate, paulownia sawdust and then determining reasonable hybrid technique system, you can make high strength matrix formula, improve The bending resistance of drill bit, toughness and hardness performance, improve the case where substantially reducing drill bit chip off-falling in use and the breaking wing Productivity.
The above is the preferred embodiment of the present invention, it is noted that for those skilled in the art For, without departing from the principles of the present invention, it can also make several improvements and retouch, these improvements and modifications It should be regarded as protection scope of the present invention.

Claims (3)

1. a kind of High-strength drill bit matrix formula, which is characterized in that be made from the following raw materials in parts by weight:30-40 parts of iron, carbon Change 10-15 parts of tungsten, 20-25 parts of chromium, 10-16 parts of nickel, 3-5 parts of manganese, 0.3-0.5 parts of phosphorus, 10-15 parts of copper, nano graphite powder 1-3 Part, 0.5-1 parts of antimony oxide, 1-2 parts of calcium carbonate, 1.6-1.8 parts of lithium stearate, 0.1-0.2 parts of zinc borate, paulownia sawdust 5-8 Part, 5-10 parts of carbon fiber, 2.5-2.7 parts of amino silane.
2. a kind of High-strength drill bit matrix formula according to claim 1, which is characterized in that by the original of following parts by weight Material is made:32-38 parts of iron, 12-14 parts of tungsten carbide, 22-24 parts of chromium, 12-14 parts of nickel, 4-5 parts of manganese, 0.4-0.5 parts of phosphorus, copper 12- 14 parts, 2-3 parts of nano graphite powder, 0.6-0.9 parts of antimony oxide, 1.2-1.8 parts of calcium carbonate, 1.7-1.8 parts of lithium stearate, boron Sour zinc 0.14-0.17 parts, 6-7 parts of paulownia sawdust, 7-9 parts of carbon fiber, 2.6-2.7 parts of amino silane.
3. a kind of High-strength drill bit matrix formula according to claim 2, which is characterized in that by the original of following parts by weight Material is made:35 parts of iron, 13 parts of tungsten carbide, 23 parts of chromium, 13 parts of nickel, 4 parts of manganese, 0.4 part of phosphorus, 13 parts of copper, 2 parts of nano graphite powder, three Aoxidize 0.7 part of two antimony, 1.5 parts of calcium carbonate, 1.7 parts of lithium stearate, 0.15 part of zinc borate, 6 parts of paulownia sawdust, 8 parts of carbon fiber, amino 2.6 parts of silane.
CN201810625345.4A 2018-06-18 2018-06-18 A kind of High-strength drill bit matrix formula Withdrawn CN108588593A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201810625345.4A CN108588593A (en) 2018-06-18 2018-06-18 A kind of High-strength drill bit matrix formula

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201810625345.4A CN108588593A (en) 2018-06-18 2018-06-18 A kind of High-strength drill bit matrix formula

Publications (1)

Publication Number Publication Date
CN108588593A true CN108588593A (en) 2018-09-28

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Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN114192847A (en) * 2021-12-31 2022-03-18 江苏博瑞工具有限公司 Die-casting zinc alloy hexagonal-handle twist drill and manufacturing method thereof
CN114318058A (en) * 2021-12-30 2022-04-12 江苏海昌工具有限公司 High-performance alloy saw blade and preparation method thereof

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN114318058A (en) * 2021-12-30 2022-04-12 江苏海昌工具有限公司 High-performance alloy saw blade and preparation method thereof
CN114192847A (en) * 2021-12-31 2022-03-18 江苏博瑞工具有限公司 Die-casting zinc alloy hexagonal-handle twist drill and manufacturing method thereof

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Application publication date: 20180928