CN105438637A - Morgan line bundling machine - Google Patents
Morgan line bundling machine Download PDFInfo
- Publication number
- CN105438637A CN105438637A CN201510983473.2A CN201510983473A CN105438637A CN 105438637 A CN105438637 A CN 105438637A CN 201510983473 A CN201510983473 A CN 201510983473A CN 105438637 A CN105438637 A CN 105438637A
- Authority
- CN
- China
- Prior art keywords
- speed
- alloy material
- morgan
- hours
- room temperature
- 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.)
- Pending
Links
- 239000000956 alloy Substances 0.000 claims abstract description 32
- 239000002184 metal Substances 0.000 claims abstract description 25
- 239000012535 impurity Substances 0.000 claims abstract description 10
- 238000010792 warming Methods 0.000 claims description 18
- 239000000463 material Substances 0.000 claims description 14
- 239000000203 mixture Substances 0.000 claims description 9
- 238000001816 cooling Methods 0.000 abstract 2
- 238000010438 heat treatment Methods 0.000 abstract 2
- 238000007669 thermal treatment Methods 0.000 abstract 1
- 238000005299 abrasion Methods 0.000 description 2
- 230000003026 anti-oxygenic effect Effects 0.000 description 2
- 238000005260 corrosion Methods 0.000 description 2
- 230000007797 corrosion Effects 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B65—CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
- B65D—CONTAINERS FOR STORAGE OR TRANSPORT OF ARTICLES OR MATERIALS, e.g. BAGS, BARRELS, BOTTLES, BOXES, CANS, CARTONS, CRATES, DRUMS, JARS, TANKS, HOPPERS, FORWARDING CONTAINERS; ACCESSORIES, CLOSURES, OR FITTINGS THEREFOR; PACKAGING ELEMENTS; PACKAGES
- B65D63/00—Flexible elongated elements, e.g. straps, for bundling or supporting articles
- B65D63/10—Non-metallic straps, tapes, or bands; Filamentary elements, e.g. strings, threads or wires; Joints between ends thereof
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D6/00—Heat treatment of ferrous alloys
- C21D6/007—Heat treatment of ferrous alloys containing Co
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/002—Ferrous alloys, e.g. steel alloys containing In, Mg, or other elements not provided for in one single group C22C38/001 - C22C38/60
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/10—Ferrous alloys, e.g. steel alloys containing cobalt
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/60—Ferrous alloys, e.g. steel alloys containing lead, selenium, tellurium, or antimony, or more than 0.04% by weight of sulfur
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Materials Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Crystallography & Structural Chemistry (AREA)
- Materials For Medical Uses (AREA)
Abstract
The invention discloses a morgan line bundling machine. The machine comprises a metal body which is manufactured from a thermally-treated alloy material, wherein the alloy material comprises the following components: 1 to 2% of As, 0.9% of S, 0.5% of P, 0.3% of Be, 0.4% of Co, 0.8% of Pb, and the balance Fe and inevitable impurities. The alloy material is subjected to thermal treatment by the following steps: 1) heating at the speed of 15 DEG C per minute until the temperature reaches 605 DEG C, and then maintaining the temperature for 3. 5 hours; 2) cooling at the speed of 25 DEG C per minute until the temperature reaches the room temperature; 3) heating at the speed of 20 DEG C per minute until the temperature is 705 DEG C, and maintaining the temperature for 3 hours; 4) cooling at the speed of 25 DEG C per minute until the temperature reaches the room temperature. According to the morgan line bundling machine, the metal body is high in performance, and the service life is long.
Description
Technical field
The present invention relates to morgan's line material bander.
Background technology
The work under bad environment of morgan's line material bander, to its metal master performance requriements higher.
Summary of the invention
The object of the present invention is to provide a kind of morgan's line material bander, its metal master is made by through hot-cured alloy material, and metal master is lightweight, intensity is high, abrasion-resistant, withstanding corrosion, heat-resisting, cold-resistant, antioxygenic property is good, and period of service is long.
For achieving the above object, technical scheme of the present invention is a kind of morgan's line material bander of design, and comprise metal master, described metal master is made by through hot-cured alloy material, and by weight percentage, the composition of this alloy material is:
As:1~2%,
S:0.9%,
P:0.5%,
Be:0.3%,
Co:0.4%,
Pb:0.8%,
Surplus is Fe and inevitable impurity;
Described alloy material is heat-treated as follows:
1) be warming up to 605 DEG C with the speed of 15 DEG C/min, be incubated 3.5 hours;
2) room temperature is cooled to the speed of 25 DEG C/min again;
3) be warming up to 705 DEG C with the speed of 20 DEG C/min again, be incubated 3 hours;
4) room temperature is cooled to the speed of 25 DEG C/min again.
Preferably, morgan's line material bander, comprises metal master, and described metal master is made by through hot-cured alloy material, and by weight percentage, the composition of this alloy material is:
As:1%,
S:0.9%,
P:0.5%,
Be:0.3%,
Co:0.4%,
Pb:0.8%,
Surplus is Fe and inevitable impurity;
Described alloy material is heat-treated as follows:
1) be warming up to 605 DEG C with the speed of 15 DEG C/min, be incubated 3.5 hours;
2) room temperature is cooled to the speed of 25 DEG C/min again;
3) be warming up to 705 DEG C with the speed of 20 DEG C/min again, be incubated 3 hours;
4) room temperature is cooled to the speed of 25 DEG C/min again.
Preferably, morgan's line material bander, comprises metal master, and described metal master is made by through hot-cured alloy material, and by weight percentage, the composition of this alloy material is:
As:2%,
S:0.9%,
P:0.5%,
Be:0.3%,
Co:0.4%,
Pb:0.8%,
Surplus is Fe and inevitable impurity;
Described alloy material is heat-treated as follows:
1) be warming up to 605 DEG C with the speed of 15 DEG C/min, be incubated 3.5 hours;
2) room temperature is cooled to the speed of 25 DEG C/min again;
3) be warming up to 705 DEG C with the speed of 20 DEG C/min again, be incubated 3 hours;
4) room temperature is cooled to the speed of 25 DEG C/min again.
Advantage of the present invention and beneficial effect are: provide a kind of morgan's line material bander, its metal master is made by through hot-cured alloy material, metal master is lightweight, intensity is high, abrasion-resistant, withstanding corrosion, heat-resisting, cold-resistant, antioxygenic property is good, and period of service is long.
Detailed description of the invention
Below in conjunction with embodiment, the specific embodiment of the present invention is further described.Following examples only for technical scheme of the present invention is clearly described, and can not limit the scope of the invention with this.
The technical scheme that the present invention specifically implements is:
Embodiment 1
A kind of morgan's line material bander, comprise metal master, described metal master is made by through hot-cured alloy material, and by weight percentage, the composition of this alloy material is:
As:1~2%,
S:0.9%,
P:0.5%,
Be:0.3%,
Co:0.4%,
Pb:0.8%,
Surplus is Fe and inevitable impurity;
Described alloy material is heat-treated as follows:
1) be warming up to 605 DEG C with the speed of 15 DEG C/min, be incubated 3.5 hours;
2) room temperature is cooled to the speed of 25 DEG C/min again;
3) be warming up to 705 DEG C with the speed of 20 DEG C/min again, be incubated 3 hours;
4) room temperature is cooled to the speed of 25 DEG C/min again.
Embodiment 2
Morgan's line material bander, comprises metal master, and described metal master is made by through hot-cured alloy material, and by weight percentage, the composition of this alloy material is:
As:1%,
S:0.9%,
P:0.5%,
Be:0.3%,
Co:0.4%,
Pb:0.8%,
Surplus is Fe and inevitable impurity;
Described alloy material is heat-treated as follows:
1) be warming up to 605 DEG C with the speed of 15 DEG C/min, be incubated 3.5 hours;
2) room temperature is cooled to the speed of 25 DEG C/min again;
3) be warming up to 705 DEG C with the speed of 20 DEG C/min again, be incubated 3 hours;
4) room temperature is cooled to the speed of 25 DEG C/min again.
Embodiment 3
Morgan's line material bander, comprises metal master, and described metal master is made by through hot-cured alloy material, and by weight percentage, the composition of this alloy material is:
As:2%,
S:0.9%,
P:0.5%,
Be:0.3%,
Co:0.4%,
Pb:0.8%,
Surplus is Fe and inevitable impurity;
Described alloy material is heat-treated as follows:
1) be warming up to 605 DEG C with the speed of 15 DEG C/min, be incubated 3.5 hours;
2) room temperature is cooled to the speed of 25 DEG C/min again;
3) be warming up to 705 DEG C with the speed of 20 DEG C/min again, be incubated 3 hours;
4) room temperature is cooled to the speed of 25 DEG C/min again.
The above is only the preferred embodiment of the present invention; it should be pointed out that for those skilled in the art, under the prerequisite not departing from the technology of the present invention principle; can also make some improvements and modifications, these improvements and modifications also should be considered as protection scope of the present invention.
Claims (3)
1. morgan's line material bander, is characterized in that, comprises metal master, and described metal master is made by through hot-cured alloy material, and by weight percentage, the composition of this alloy material is:
As:1~2%,
S:0.9%,
P:0.5%,
Be:0.3%,
Co:0.4%,
Pb:0.8%,
Surplus is Fe and inevitable impurity;
Described alloy material is heat-treated as follows:
1) be warming up to 605 DEG C with the speed of 15 DEG C/min, be incubated 3.5 hours;
2) room temperature is cooled to the speed of 25 DEG C/min again;
3) be warming up to 705 DEG C with the speed of 20 DEG C/min again, be incubated 3 hours;
4) room temperature is cooled to the speed of 25 DEG C/min again.
2. morgan's line material bander according to claim 1, it is characterized in that, comprise metal master, described metal master is made by through hot-cured alloy material, and by weight percentage, the composition of this alloy material is:
As:1%,
S:0.9%,
P:0.5%,
Be:0.3%,
Co:0.4%,
Pb:0.8%,
Surplus is Fe and inevitable impurity;
Described alloy material is heat-treated as follows:
1) be warming up to 605 DEG C with the speed of 15 DEG C/min, be incubated 3.5 hours;
2) room temperature is cooled to the speed of 25 DEG C/min again;
3) be warming up to 705 DEG C with the speed of 20 DEG C/min again, be incubated 3 hours;
4) room temperature is cooled to the speed of 25 DEG C/min again.
3. morgan's line material bander according to claim 1, it is characterized in that, comprise metal master, described metal master is made by through hot-cured alloy material, and by weight percentage, the composition of this alloy material is:
As:2%,
S:0.9%,
P:0.5%,
Be:0.3%,
Co:0.4%,
Pb:0.8%,
Surplus is Fe and inevitable impurity;
Described alloy material is heat-treated as follows:
1) be warming up to 605 DEG C with the speed of 15 DEG C/min, be incubated 3.5 hours;
2) room temperature is cooled to the speed of 25 DEG C/min again;
3) be warming up to 705 DEG C with the speed of 20 DEG C/min again, be incubated 3 hours;
4) room temperature is cooled to the speed of 25 DEG C/min again.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201510983473.2A CN105438637A (en) | 2015-12-24 | 2015-12-24 | Morgan line bundling machine |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201510983473.2A CN105438637A (en) | 2015-12-24 | 2015-12-24 | Morgan line bundling machine |
Publications (1)
Publication Number | Publication Date |
---|---|
CN105438637A true CN105438637A (en) | 2016-03-30 |
Family
ID=55549375
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201510983473.2A Pending CN105438637A (en) | 2015-12-24 | 2015-12-24 | Morgan line bundling machine |
Country Status (1)
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CN (1) | CN105438637A (en) |
Citations (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE2613318A1 (en) * | 1976-03-29 | 1977-10-13 | Peter Dr Weinhold | Alloys with optimum properties - contg. one or more of ninety three different elements |
CN1127795A (en) * | 1995-01-26 | 1996-07-31 | 中国科学院金属研究所 | Directional solidification of best cast nickel based high-temp. alloy |
JP2002275563A (en) * | 2001-03-21 | 2002-09-25 | Kobe Steel Ltd | Hot-rollable phosphor bronze |
JP2010275640A (en) * | 2002-09-13 | 2010-12-09 | Olin Corp | Age-hardening copper-base alloy and processing |
CN102369304A (en) * | 2009-04-01 | 2012-03-07 | 罗瓦玛股份公司 | Hot working tool steel with excellent toughness and thermal conductivity |
CN102428197A (en) * | 2009-05-22 | 2012-04-25 | 西门子公司 | Ferritic martensitic iron-based alloy, component and method |
CN103128506A (en) * | 2013-02-04 | 2013-06-05 | 繁昌县琪鑫铸造有限公司 | Manufacturing method of anti-yield foundation bolt |
CN104011234A (en) * | 2011-12-27 | 2014-08-27 | 杰富意钢铁株式会社 | Hot-rolled steel sheet and process for manufacturing same |
CN104159681A (en) * | 2012-03-06 | 2014-11-19 | 杰富意钢铁株式会社 | Warm press forming method and automobile frame component |
-
2015
- 2015-12-24 CN CN201510983473.2A patent/CN105438637A/en active Pending
Patent Citations (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE2613318A1 (en) * | 1976-03-29 | 1977-10-13 | Peter Dr Weinhold | Alloys with optimum properties - contg. one or more of ninety three different elements |
CN1127795A (en) * | 1995-01-26 | 1996-07-31 | 中国科学院金属研究所 | Directional solidification of best cast nickel based high-temp. alloy |
JP2002275563A (en) * | 2001-03-21 | 2002-09-25 | Kobe Steel Ltd | Hot-rollable phosphor bronze |
JP2010275640A (en) * | 2002-09-13 | 2010-12-09 | Olin Corp | Age-hardening copper-base alloy and processing |
CN102369304A (en) * | 2009-04-01 | 2012-03-07 | 罗瓦玛股份公司 | Hot working tool steel with excellent toughness and thermal conductivity |
CN102428197A (en) * | 2009-05-22 | 2012-04-25 | 西门子公司 | Ferritic martensitic iron-based alloy, component and method |
CN104011234A (en) * | 2011-12-27 | 2014-08-27 | 杰富意钢铁株式会社 | Hot-rolled steel sheet and process for manufacturing same |
CN104159681A (en) * | 2012-03-06 | 2014-11-19 | 杰富意钢铁株式会社 | Warm press forming method and automobile frame component |
CN103128506A (en) * | 2013-02-04 | 2013-06-05 | 繁昌县琪鑫铸造有限公司 | Manufacturing method of anti-yield foundation bolt |
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C06 | Publication | ||
PB01 | Publication | ||
C10 | Entry into substantive examination | ||
SE01 | Entry into force of request for substantive examination | ||
RJ01 | Rejection of invention patent application after publication |
Application publication date: 20160330 |
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RJ01 | Rejection of invention patent application after publication |