CN107513655A - A kind of titanium alloy deep drill blade material - Google Patents
A kind of titanium alloy deep drill blade material Download PDFInfo
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- CN107513655A CN107513655A CN201710838794.2A CN201710838794A CN107513655A CN 107513655 A CN107513655 A CN 107513655A CN 201710838794 A CN201710838794 A CN 201710838794A CN 107513655 A CN107513655 A CN 107513655A
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- titanium alloy
- elements
- alloy deep
- blade material
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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C30/00—Alloys containing less than 50% by weight of each constituent
- C22C30/02—Alloys containing less than 50% by weight of each constituent containing copper
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C14/00—Alloys based on titanium
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C30/00—Alloys containing less than 50% by weight of each constituent
- C22C30/06—Alloys containing less than 50% by weight of each constituent containing zinc
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- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Earth Drilling (AREA)
Abstract
The invention discloses a kind of titanium alloy deep drill blade material, including:15 25 parts of titanium elements, 1.5 6 parts of boron element, 3.5 7 parts of ferro element, 1.5 6.5 parts of magnesium elements, 0.5 3.5 parts of v element, 5.5 8 parts of molybdenum element, 2.5 6.5 parts of chromium, 15 parts of Zn-ef ficiency, 6.6 8 parts of copper.By the above-mentioned means, a kind of titanium alloy deep drill blade material of the present invention, calorific intensity is high, corrosion stability is good and the good characteristics such as high temperature performance is good and irreplaceable position is achieved in industries such as aerospace, atomic energy, electric power, chemical industry and oil well loggings.
Description
Technical field
The present invention relates to drill bit material technical field, more particularly to a kind of titanium alloy deep drill blade material.
Background technology
Brick is raveled under the extruding of blade and centrifugal action at work, is formed native stream and is pressed to crater wall, while along page
Face elevator is to earth's surface, drill bit the problem of temperature height can produce fracture, deformation in use.
The content of the invention
The present invention solves the technical problem of a kind of titanium alloy deep drill blade material is provided, calorific intensity is high, anti-
Corrosion is good and high temperature performance well etc. good characteristic and achieved in industries such as aerospace, atomic energy, electric power, chemical industry and oil well loggings
Irreplaceable position.
In order to solve the above technical problems, a kind of titanium alloy deep drill blade material, including:Titanium elements, boron element, iron member
Element, magnesium elements, v element, molybdenum element, chromium, Zn-ef ficiency, copper, the mass fraction of each component are:Titanium elements 15-25
Part, boron element 1.5-6 parts, ferro element 3.5-7 parts, magnesium elements 1.5-6.5 parts, v element 0.5-3.5 parts, molybdenum element 5.5-8 parts,
Chromium 2.5-6.5 parts, Zn-ef ficiency 1-5 parts, copper 6.6-8 parts.
In a preferred embodiments of the invention, the mass fraction of each component in the titanium alloy deep drill blade material
For:15 parts of titanium elements, 1.5 parts of boron element, 3.5 parts of ferro element, 1.5 parts of magnesium elements, 0.5 part of v element, 5.5 parts of molybdenum element, chromium
2.5 parts of element, 1 part of Zn-ef ficiency, 6.6 parts of copper.
In a preferred embodiments of the invention, the mass fraction of each component in the titanium alloy deep drill blade material
For:16 parts of titanium elements, 2.5 parts of boron element, 4 parts of ferro element, 2.5 parts of magnesium elements, 1.5 parts of v element, 6 parts of molybdenum element, chromium
3.5 parts, 2 parts of Zn-ef ficiency, 7 parts of copper.
In a preferred embodiments of the invention, the mass fraction of each component in the titanium alloy deep drill blade material
For:18 parts of titanium elements, 2.5 parts of boron element, 5 parts of ferro element, 3 parts of magnesium elements, 2 parts of v element, 6.5 parts of molybdenum element, chromium 4
Part, 3 parts of Zn-ef ficiency, 7.5 parts of copper.
In a preferred embodiments of the invention, the mass fraction of each component in the titanium alloy deep drill blade material
For:22 parts of titanium elements, 5 parts of boron element, 6 parts of ferro element, 6 parts of magnesium elements, 3 parts of v element, 7 parts of molybdenum element, 6 parts of chromium, zinc
4 parts of element, 7 parts of copper.
In a preferred embodiments of the invention, the mass fraction of each component in the titanium alloy deep drill blade material
For:25 parts of titanium elements, 6 parts of boron element, 7 parts of ferro element, 6.5 parts of magnesium elements, 3.5 parts of v element, 8 parts of molybdenum element, chromium 6.5
Part, 5 parts of Zn-ef ficiency, 8 parts of copper.
The beneficial effects of the invention are as follows:A kind of titanium alloy deep drill blade material of the present invention, calorific intensity is high, corrosion stability is good
Wait good characteristic well with high temperature performance and achieve and can not replace in industries such as aerospace, atomic energy, electric power, chemical industry and oil well loggings
The position in generation.
Embodiment
The technical scheme in the embodiment of the present invention will be clearly and completely described below, it is clear that described implementation
Example is only the part of the embodiment of the present invention, rather than whole embodiments.It is common based on the embodiment in the present invention, this area
All other embodiment that technical staff is obtained under the premise of creative work is not made, belong to the model that the present invention protects
Enclose.
A kind of titanium alloy deep drill blade material of the present invention, including:Titanium elements, boron element, ferro element, magnesium elements, vanadium
Element, molybdenum element, chromium, Zn-ef ficiency, copper, the mass fraction of each component are:Titanium elements 15-25 parts, boron element 1.5-6
Part, ferro element 3.5-7 parts, magnesium elements 1.5-6.5 parts, v element 0.5-3.5 parts, molybdenum element 5.5-8 parts, chromium 2.5-6.5
Part, Zn-ef ficiency 1-5 parts, copper 6.6-8 parts.
Further, the mass fraction of each component is in the titanium alloy deep drill blade material:15 parts of titanium elements, boron
1.5 parts of element, 3.5 parts of ferro element, 1.5 parts of magnesium elements, 0.5 part of v element, 5.5 parts of molybdenum element, 2.5 parts of chromium, Zn-ef ficiency 1
Part, 6.6 parts of copper.
Further, the mass fraction of each component is in the titanium alloy deep drill blade material:16 parts of titanium elements, boron
2.5 parts of element, 4 parts of ferro element, 2.5 parts of magnesium elements, 1.5 parts of v element, 6 parts of molybdenum element, 3.5 parts of chromium, 2 parts of Zn-ef ficiency,
7 parts of copper.
Further, the mass fraction of each component is in the titanium alloy deep drill blade material:18 parts of titanium elements, boron
2.5 parts of element, 5 parts of ferro element, 3 parts of magnesium elements, 2 parts of v element, 6.5 parts of molybdenum element, 4 parts of chromium, 3 parts of Zn-ef ficiency, copper coin
7.5 parts of element.
Further, the mass fraction of each component is in the titanium alloy deep drill blade material:22 parts of titanium elements, boron
5 parts of element, 6 parts of ferro element, 6 parts of magnesium elements, 3 parts of v element, 7 parts of molybdenum element, 6 parts of chromium, 4 parts of Zn-ef ficiency, copper 7
Part.
Further, the mass fraction of each component is in the titanium alloy deep drill blade material:25 parts of titanium elements, boron
6 parts of element, 7 parts of ferro element, 6.5 parts of magnesium elements, 3.5 parts of v element, 8 parts of molybdenum element, 6.5 parts of chromium, 5 parts of Zn-ef ficiency, copper
8 parts of element.
The beneficial effects of the invention are as follows:A kind of titanium alloy deep drill blade material of the present invention, calorific intensity is high, corrosion stability is good
Wait good characteristic well with high temperature performance and achieve and can not replace in industries such as aerospace, atomic energy, electric power, chemical industry and oil well loggings
The position in generation.
Embodiments of the invention are the foregoing is only, are not intended to limit the scope of the invention, it is every to utilize this hair
The equivalent structure or equivalent flow conversion that bright description is made, or directly or indirectly it is used in other related technology necks
Domain, similarly it is included in the scope of patent protection of the present invention.
Claims (6)
- A kind of 1. titanium alloy deep drill blade material, it is characterised in that including:Titanium elements, boron element, ferro element, magnesium elements, V element, molybdenum element, chromium, Zn-ef ficiency, copper, the mass fraction of each component are:Titanium elements 15-25 parts, boron element 1.5-6 parts, ferro element 3.5-7 parts, magnesium elements 1.5-6.5 parts, v element 0.5-3.5 parts, molybdenum element 5.5-8 parts, chromium 2.5-6.5 part, Zn-ef ficiency 1-5 parts, copper 6.6-8 parts.
- A kind of 2. titanium alloy deep drill blade material according to claim 1, it is characterised in that the titanium alloy deep hole The mass fraction of each component is in drill tip material:15 parts of titanium elements, 1.5 parts of boron element, 3.5 parts of ferro element, magnesium elements 1.5 Part, 0.5 part of v element, 5.5 parts of molybdenum element, 2.5 parts of chromium, 1 part of Zn-ef ficiency, 6.6 parts of copper.
- A kind of 3. titanium alloy deep drill blade material according to claim 1, it is characterised in that the titanium alloy deep hole The mass fraction of each component is in drill tip material:16 parts of titanium elements, 2.5 parts of boron element, 4 parts of ferro element, magnesium elements 2.5 Part, 1.5 parts of v element, 6 parts of molybdenum element, 3.5 parts of chromium, 2 parts of Zn-ef ficiency, 7 parts of copper.
- A kind of 4. titanium alloy deep drill blade material according to claim 1, it is characterised in that the titanium alloy deep hole The mass fraction of each component is in drill tip material:18 parts of titanium elements, 2.5 parts of boron element, 5 parts of ferro element, 3 parts of magnesium elements, 2 parts of v element, 6.5 parts of molybdenum element, 4 parts of chromium, 3 parts of Zn-ef ficiency, 7.5 parts of copper.
- A kind of 5. titanium alloy deep drill blade material according to claim 1, it is characterised in that the titanium alloy deep hole The mass fraction of each component is in drill tip material:22 parts of titanium elements, 5 parts of boron element, 6 parts of ferro element, 6 parts of magnesium elements, vanadium 3 parts of element, 7 parts of molybdenum element, 6 parts of chromium, 4 parts of Zn-ef ficiency, 7 parts of copper.
- A kind of 6. titanium alloy deep drill blade material according to claim 1, it is characterised in that the titanium alloy deep hole The mass fraction of each component is in drill tip material:25 parts of titanium elements, 6 parts of boron element, 7 parts of ferro element, 6.5 parts of magnesium elements, 3.5 parts of v element, 8 parts of molybdenum element, 6.5 parts of chromium, 5 parts of Zn-ef ficiency, 8 parts of copper.
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CN201710838794.2A CN107513655A (en) | 2017-09-18 | 2017-09-18 | A kind of titanium alloy deep drill blade material |
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CN201710838794.2A CN107513655A (en) | 2017-09-18 | 2017-09-18 | A kind of titanium alloy deep drill blade material |
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Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP1698714A2 (en) * | 2000-12-28 | 2006-09-06 | Kabushiki Kaisha Kobe Seiko Sho | Target used to form a hard film |
CN1962912A (en) * | 2006-11-14 | 2007-05-16 | 永康市民泰钛业科技有限公司 | High-hardness titanium alloy and method for producing same |
CN101563521A (en) * | 2006-11-06 | 2009-10-21 | 贝克休斯公司 | Earth-boring rotary drill bits including bit bodies comprising reinforced titanium or titanium-based alloy matrix materials, and methods for forming such bits |
CN102605212A (en) * | 2012-03-29 | 2012-07-25 | 北京科技大学 | Free-cutting titanium alloy and preparation method thereof |
CN105018788A (en) * | 2014-08-21 | 2015-11-04 | 太仓钧浩自行车科技有限公司 | Titanium alloy for frame of electric bicycle and preparation method thereof |
-
2017
- 2017-09-18 CN CN201710838794.2A patent/CN107513655A/en active Pending
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP1698714A2 (en) * | 2000-12-28 | 2006-09-06 | Kabushiki Kaisha Kobe Seiko Sho | Target used to form a hard film |
CN101563521A (en) * | 2006-11-06 | 2009-10-21 | 贝克休斯公司 | Earth-boring rotary drill bits including bit bodies comprising reinforced titanium or titanium-based alloy matrix materials, and methods for forming such bits |
CN1962912A (en) * | 2006-11-14 | 2007-05-16 | 永康市民泰钛业科技有限公司 | High-hardness titanium alloy and method for producing same |
CN102605212A (en) * | 2012-03-29 | 2012-07-25 | 北京科技大学 | Free-cutting titanium alloy and preparation method thereof |
CN105018788A (en) * | 2014-08-21 | 2015-11-04 | 太仓钧浩自行车科技有限公司 | Titanium alloy for frame of electric bicycle and preparation method thereof |
Non-Patent Citations (1)
Title |
---|
于泓主编: "《机械工程材料》", 30 September 2014, 北京:北京航空航天大学出版社 * |
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Application publication date: 20171226 |