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CN105438637A - Morgan line bundling machine - Google Patents

Morgan line bundling machine Download PDF

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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
Application number
CN201510983473.2A
Other languages
Chinese (zh)
Inventor
单坤林
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.)
CHANGSHU XINYE MACHINERY MANUFACTURING Co Ltd
Original Assignee
CHANGSHU XINYE MACHINERY MANUFACTURING 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 CHANGSHU XINYE MACHINERY MANUFACTURING Co Ltd filed Critical CHANGSHU XINYE MACHINERY MANUFACTURING Co Ltd
Priority to CN201510983473.2A priority Critical patent/CN105438637A/en
Publication of CN105438637A publication Critical patent/CN105438637A/en
Pending legal-status Critical Current

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Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B65CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
    • B65DCONTAINERS 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
    • B65D63/00Flexible elongated elements, e.g. straps, for bundling or supporting articles
    • B65D63/10Non-metallic straps, tapes, or bands; Filamentary elements, e.g. strings, threads or wires; Joints between ends thereof
    • CCHEMISTRY; METALLURGY
    • C21METALLURGY OF IRON
    • C21DMODIFYING 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
    • C21D6/00Heat treatment of ferrous alloys
    • C21D6/007Heat treatment of ferrous alloys containing Co
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/002Ferrous alloys, e.g. steel alloys containing In, Mg, or other elements not provided for in one single group C22C38/001 - C22C38/60
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/10Ferrous alloys, e.g. steel alloys containing cobalt
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/60Ferrous alloys, e.g. steel alloys containing lead, selenium, tellurium, or antimony, or more than 0.04% by weight of sulfur

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  • 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

Morgan's line material bander
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.
CN201510983473.2A 2015-12-24 2015-12-24 Morgan line bundling machine Pending CN105438637A (en)

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)

Country Link
CN (1) CN105438637A (en)

Citations (9)

* Cited by examiner, † Cited by third party
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

Patent Citations (9)

* Cited by examiner, † Cited by third party
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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PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
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Application publication date: 20160330

RJ01 Rejection of invention patent application after publication