CN106498229A - Titanium alloy for robot for space - Google Patents
Titanium alloy for robot for space Download PDFInfo
- Publication number
- CN106498229A CN106498229A CN201610904848.6A CN201610904848A CN106498229A CN 106498229 A CN106498229 A CN 106498229A CN 201610904848 A CN201610904848 A CN 201610904848A CN 106498229 A CN106498229 A CN 106498229A
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- CN
- China
- Prior art keywords
- space
- robot
- titanium alloy
- present
- balance
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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.)
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Classifications
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- 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
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- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Manipulator (AREA)
Abstract
For the titanium alloy of robot for space, contain according to weight percent content:Al:2.1 4.2%, Mn:2.5 3.2%, Cu:0.8 1.8%, Th:0.3 0.45%, Zr:6.2 8.5%, balance of Ti;The present invention improves the lower temperature resistance of titanium alloy using the alloy property of Zr and Ti, meanwhile, greatly reduce its own weight so as to which when working for robot for space, can be helped to play good accuracy.
Description
Technical field
The present invention relates to robot for space field, is particularly used for the titanium alloy of robot for space.
Background technology
Robot for space be in space environment activity, space environment and ground environment difference very big, robot for space
It is operated in microgravity, high vacuum, ultralow temperature, intense radiation, in the environment of illumination difference, therefore, robot for space and ground robot
Requirement also necessarily differ, the characteristics of have its own.First, the volume of robot for space is smaller, and weight is lighter, resists dry
Disturb ability stronger.Secondly, the degree of intelligence of robot for space is higher, and function is more complete.The energy that robot for space is consumed
As little as possible, working life is as long as possible, and due to being operated under space this special environment, to it can
Require by property also higher.
But, current robot for space under high vacuum environment and ultra-low temperature surroundings needs accurately to be operated, deposits
There iing own wt larger, affecting work precision, it is possible to the problems such as accident occurs.
Content of the invention
For solving the above problems, the present invention is adopted the following technical scheme that:
For the titanium alloy of robot for space, contain according to weight percent content:Al:2.1-4.2%, Mn:2.5-3.2%, Cu:
0.8-1.8%, Th:0.3-0.45%, Zr:6.2-8.5%, balance of Ti.
Further, the above-mentioned titanium alloy for robot for space, contains according to weight percent content:Al:2.1%,
Mn:2.5%, Cu:0.8%, Th:0.3%, Zr:6.2%, balance of Ti.
The present invention improves the lower temperature resistance of titanium alloy using the alloy property of Zr and Ti, meanwhile, greatly reduce which certainly
Body weight so as to which can be helped when working for robot for space to play good accuracy.
Specific embodiment
Below the technical scheme in the embodiment of the present invention is clearly and completely described, it is clear that described enforcement
Example is only a part of embodiment of the present invention, rather than whole embodiment.Embodiment in based on the present invention, this area are common
All other embodiment that technical staff is obtained under the premise of creative work is not made, belongs to the model of present invention protection
Enclose.
For the titanium alloy of robot for space, contain according to weight percent content:Al:2.1-4.2%, Mn:2.5-
3.2%, Cu:0.8-1.8%, Th:0.3-0.45%, Zr:6.2-8.5%, balance of Ti.
The present invention improves the lower temperature resistance of titanium alloy using the alloy property of Zr and Ti, meanwhile, greatly reduce which certainly
Body weight so as to which can be helped when working for robot for space to play good accuracy.
Embodiments of the invention are the foregoing is only, the scope of the claims of the present invention is not thereby limited, every using this
Equivalent structure or equivalent flow conversion that bright description is made, or directly or indirectly it is used in other related technology necks
Domain, is included within the scope of the present invention.
Claims (2)
1. the titanium alloy of robot for space is used for, it is characterised in that contained according to weight percent content:Al:2.1-4.2%,
Mn:2.5-3.2%, Cu:0.8-1.8%, Th:0.3-0.45%, Zr:6.2-8.5%, balance of Ti.
2. the titanium alloy of robot for space is used for as claimed in claim 1, it is characterised in that:Contain according to weight percent content
Have:Al:2.1%, Mn:2.5%, Cu:0.8%, Th:0.3%, Zr:6.2%, balance of Ti.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201610904848.6A CN106498229A (en) | 2016-10-18 | 2016-10-18 | Titanium alloy for robot for space |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201610904848.6A CN106498229A (en) | 2016-10-18 | 2016-10-18 | Titanium alloy for robot for space |
Publications (1)
Publication Number | Publication Date |
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CN106498229A true CN106498229A (en) | 2017-03-15 |
Family
ID=58293716
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201610904848.6A Pending CN106498229A (en) | 2016-10-18 | 2016-10-18 | Titanium alloy for robot for space |
Country Status (1)
Country | Link |
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CN (1) | CN106498229A (en) |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH08120373A (en) * | 1994-08-22 | 1996-05-14 | Sumitomo Metal Ind Ltd | High creep strength titanium alloy and its production |
CN1974859A (en) * | 2006-11-14 | 2007-06-06 | 永康市民泰钛业科技有限公司 | Titanium alloy anode for electrolyzing manganese dioxide and manufacturing method thereof |
CN101328551A (en) * | 2007-06-19 | 2008-12-24 | 中国科学院金属研究所 | Titanium alloy material producing no spark by friction |
-
2016
- 2016-10-18 CN CN201610904848.6A patent/CN106498229A/en active Pending
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH08120373A (en) * | 1994-08-22 | 1996-05-14 | Sumitomo Metal Ind Ltd | High creep strength titanium alloy and its production |
CN1974859A (en) * | 2006-11-14 | 2007-06-06 | 永康市民泰钛业科技有限公司 | Titanium alloy anode for electrolyzing manganese dioxide and manufacturing method thereof |
CN101328551A (en) * | 2007-06-19 | 2008-12-24 | 中国科学院金属研究所 | Titanium alloy material producing no spark by friction |
Non-Patent Citations (1)
Title |
---|
朱知寿等: "《新型航空高性能钛合金材料技术研究与发展》", 30 December 2013 * |
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Legal Events
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C06 | Publication | ||
PB01 | Publication | ||
SE01 | Entry into force of request for substantive examination | ||
SE01 | Entry into force of request for substantive examination | ||
RJ01 | Rejection of invention patent application after publication | ||
RJ01 | Rejection of invention patent application after publication |
Application publication date: 20170315 |