WO1995033080A1 - Iron-chromium-boron alloy for glass manufacturing tools - Google Patents
Iron-chromium-boron alloy for glass manufacturing tools Download PDFInfo
- Publication number
- WO1995033080A1 WO1995033080A1 PCT/AU1995/000312 AU9500312W WO9533080A1 WO 1995033080 A1 WO1995033080 A1 WO 1995033080A1 AU 9500312 W AU9500312 W AU 9500312W WO 9533080 A1 WO9533080 A1 WO 9533080A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- alloy
- tool
- chromium
- carbon
- boron
- Prior art date
Links
Classifications
-
- C—CHEMISTRY; METALLURGY
- C03—GLASS; MINERAL OR SLAG WOOL
- C03B—MANUFACTURE, SHAPING, OR SUPPLEMENTARY PROCESSES
- C03B9/00—Blowing glass; Production of hollow glass articles
- C03B9/30—Details of blowing glass; Use of materials for the moulds
- C03B9/48—Use of materials for the moulds
-
- 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
- C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
- C22C38/32—Ferrous alloys, e.g. steel alloys containing chromium with boron
Definitions
- This invention is concerned with improved tooling used in the manufacture of glass articles, such as glass containers, and with an alloy for such tooling.
- Glass containers are made by forming molten glass, at temperatures above the glass softening temperature.
- the glass may be made from either recycled glass or from a mixture of raw materials that includes lime, soda ash, silica sand and other additives.
- an amount of molten glass at a temperature over 1200°C is placed into a metal die and shaped by blowing air through a metal nozzle.
- the shaping process is repeated at high rates and significant wear is experienced by tools such as the metal "blow nozzle" or plunger which is in contact with what becomes the neck of the glass container and through which the air is blown.
- metal components or tools such as nozzles and other tools, that come into contact with the hot glass, must have high hardness and high wear resistance as well as high resistance to oxidation and scaling. Because of the rapid thermal cycling that occurs through repeated contact with molten glass and removal of the glass from the die, metal components or tools should have a high resistance to thermal cracking. In most types of glass container manufacture, the metal tooling experiences many thousands of thermal cycles before being re-machined or replaced.
- the "blow- blow plunger” forms the inside of the neck of the bottle, as well as enabling air to be blown to press the molten glass against the wall of the die.
- Such blow-blow plungers and other glass moulding components are conventionally made from nickel boron alloys containing 2 to 3 wt% boron, usually 98 wt% nickel and 2 wt% boron. These alloys produce a microstructure of nickel dendrites and a eutectic mixture of nickel and nickel boride. This material has a good thermal shock resistance and a reasonable hardness of about 40 to 45 Rockwell C.
- the nickel matrix is relatively soft and cannot be hardened by heat treatment. The soft matrix contributes to two problems:
- the present invention is directed to providing improved ferrous alloys suitable for manufacture of tools, which have high resistance to both wear and thermal shock, for the manufacture of glass articles such as containers.
- the invention also provides such tools cast from such alloys.
- a tool according to the invention may comprise a blow nozzle or plunger, such as a blow-blow plunger or a push-blow plunger.
- the tool may comprise any other component of machinery for use in the manufacture of glass articles, such as containers, which component is used in forming the article by contact with molten glass.
- the component thus may comprise a die or die section used for shaping a glass article.
- An alloy according to the invention is an iron-chromium-boron alloy.
- the alloy has from 1 to 20 wt% chromium, from 0.5 to 3 wt% boron, up to 1.0 wt% carbon or higher if substantial amounts of strong carbide forming elements such as molybdenum, vanadium, titanium, niobium and tungsten are present, optional alloying additions as detailed in the following, and a balance apart from incidental impurities of iron.
- a tool according to the invention is cast from a melt of the alloy of the invention, and can achieve a high hardness and resistance to wear, coupled with a high resistance to thermal shock. The tool also has a high resistance to oxidation.
- the alloy and the tool of the invention have the further benefit of being able to be softened by annealing and re-hardened to high hardness levels. Also, particularly with alloys with a high chromium content, such as at least 8 wt%, they have a high chromium content matrix which can be hardened to martensite with heat treatment and is hard and corrosion resistant. This matrix, coupled with the presence of hard iron-chromium eutectic borides, provides a material with much better wear resistance under conditions of elevated temperatures and rapid thermal cycling or heat shock.
- the iron-chromium-boron alloy and tools cast therefrom withstand wear for much longer periods than the nickel-boron alloy discussed above, and with their excellent oxidation resistance, the tools produce bottles which do not suffer from alloy metal contamination and thus give a more reliable product.
- the iron-chromium-boron alloy and tools cast therefrom can be softened to 35 Rockwell C by annealing, enabling machining, then re-hardening by heating to above 900°C and air cooling. Tempering can then further adjust hardness if needed.
- the alloy and the tool also can be provided with a high level of surface finish, achievable by polishing.
- the iron-chromium-boron alloy and tool according to the invention can be substantially free of carbon, with carbon present effectively only as an incidental impurity.
- carbon can be present at up to 1.0 wt%.
- carbon does not exceed 0.6 wt%, and may for example be present at from 0.1 to 0.6 wt%, such as from 0.1 to 0.3 wt%.
- the boron content is not less than 0.5 wt%, and most preferably is from 0.5 to 2.5 wt%, such as from 1 to 2.5 wt%.
- the preferred chromium content is from 3 to 18 wt%, such as from 8 to 18 wt%.
- the carbon level may be in excess of 1.0 wt% provided that the level of strong carbide forming elements is such that the excess carbon is bound by these elements in carbide or carbo-boride phases. The carbon content of the matrix would then remain low.
- strong carbide forming elements such as molybdenum, vanadium, titanium, tungsten and niobium
- the fracture toughness, thermal shock resistance and wear resistance of the cast ferrous alloys is largely determined by the volume fraction of hard phases, which in turn is a function of the content of both boron and carbon and carbide and boride forming elements, and also the interstitial boron and carbon content of the matrix.
- the boron content of the matrix is always low because the solubility of boron in ferrite and austenite is low.
- the solubility of carbon in austenite and therefore the carbon content of the martensitic matrix can be as high as approximately 2 wt% unless the carbon is bound in some other phase.
- the carbon content of the matrix is kept to a low enough level for sufficient fracture toughness or thermal shock resistance to be achieved for the application in question.
- the preferable level of carbon in the matrix is less than 0.3 wt% and can be significantly lower in some applications.
- the iron-base alloy can contain sufficient alloying additions for enhancement of oxidation properties and hardenability. Suitable alloying elements for these purposes include silicon, aluminium, manganese, nickel, copper and molybdenum, either separately or in combination.
- Preferred additions for these purposes are of silicon at up to 3 wt% such as from 0.5 to 3 wt%, aluminium at up to 0.2 wt%, manganese at up to 2 wt% such as from 0.2 to 1.5 wt%, nickel at from 0.2 to 3 wt% such as from 0.2 to 2 wt%, copper at up to 3 wt%, and/or molybdenum at up to 5 wt% such as from 0.5 to 5 wt%.
- the presence of silicon and/or aluminium in a melt of the iron-base alloy also is beneficial in keeping the melt in a de-oxidised condition.
- molybdenum also increases hardness and improves resistance to softening at high temperatures, due to its action as a strong carbide and/or boride forming element.
- sufficient amounts of other strong carbide and/or boride elements such as vanadium, titanium, tungsten and/or niobium, can be added to the iron-base alloy.
- Preferred additions for enhancing resistance to softening are molybdenum as indicated above, vanadium at up to 8 wt%, titanium at up to 5 wt%, niobium at up to 6 wt% and/or tungsten at up to 7 wt%.
- the iron-base alloy required for the present invention can be prepared as a melt for casting by melting suitable constituent materials in an electric induction furnace. This most preferably entails melting mild steel scrap, low carbon ferro- chromium and low carbon ferro-boron. Other commercial foundry alloys can be added to provide alloy additions required in the iron-base alloy. For re-melt charges, return scrap with about 2 wt% boron can be readily melted with mild steel scrap and ferro-alloys. The melt may be kept in a de-oxidised condition by the use of ferro-silicon or aluminium.
- the iron-base alloys of the invention have a melting point close to 1300°C. In general, a melt pouring temperature of from 1400°C to 1450°C is desirable, depending on the nature of the casting.
- the iron-base alloys may be hardened by heat treating at temperatures in the range 950 to 1150°C to form austenite and air cooling to room temperature in order to form a martensitic microstructure in the matrix of the alloy.
- a typical hardness after such a hardening treatment is 50 on the Rockwell C scale.
- the iron-base alloys or a tool cast therefrom can be softened for machining by sub-critical annealing at temperatures in the range 700 to 750°C in order to decompose the matrix to a mixture of ferrite and carbide.
- Such a heat treatment results in a decrease of hardness to 30 to 35 Rockwell C.
- the alloys can be rehardened for service by heat treating at 950 to 1150°C and air cooling to provide a typical hardness of about 50 Rockwell C.
- the iron-base alloy tool may be cast to near net shape by a range of casting methods depending upon the dimensional accuracy that is required and the extent to which the amount of machining to final dimensions is to be minimised.
- Blow-blow plungers come into direct contact with the molten glass as it falls into the mould, and then forces the glass into an initial shape by air pressure.
- a small ledge on the tip of the plunger forms an inside rim on the neck of the bottle. This ledge on the plunger must remain sharp so that a thin blade of glass does not form on the inside neck of the bottle.
- a blow-blow plunger tool for the manufacture of glass containers was manufactured by investment casting an iron-base alloy, within the compositional range specified above, and final machining to the exact shape required for the tool.
- the composition of the alloy used in this example was: carbon 0.2 wt% chromium 17 wt% boron 2 wt% silicon 0.9 wt% manganese 0.8 wt% molybdenum 0.5 wt% iron remainder.
- the plunger was sub-critically annealed at 700°C for three hours to reduce the hardness to 35 Rockwell C.
- the plunger was heated to 950°C for one hour, then cooled in air to room temperature, followed by tempering at 300°C for three hours. The final hardness was 50 Rockwell C. Final machining and grinding was then done.
- blow-blow plunger manufactured in this way showed considerably improved performance over the conventional tooling made from nickel-boron alloy.
- Conventional blow-blow plungers in this particular application have to be removed from service after 1 to 2 weeks continuous operation because of wear and loss of dimensional accuracy. They are then remachined before returning to service.
- the blow-blow plunger manufactured according to the invention remained in continuous service for 10 weeks without having to be removed for remachining. This represents an improvement in the service life of the component by a factor of 5 to 10.
- plungers were made from an iron-chromium-boron alloy according to the invention, by investment casting. These were used in the production of glass containers. The plungers stayed in production for 10 to 12 weeks without having to be re-sharpened, giving a 5 to 7 times improvement in production life compared with plungers of a conventional nickel-boron alloy.
- the particular composition for these plungers was as follows: Carbon 0.23%
- Guide plate castings are solid flat discs with a central hole through which a plunger will pass and retract.
- the clearance between the plunger and the central hole is critical and should not be allowed to become large enough to allow molten glass to penetrate between the plunger and the guide plate.
- Wear between the plunger and the guide plate at temperatures up to 500°C is the main cause of replacement of the guide plate.
- Twenty guide plates made from the iron-chromium-boron alloy by investment casting have been trialed in production of a 500 ml bottle for 13 days continuously with no measurable change in dimension.
- Guide plates made from nickel-boron alloy or tool steel require measurement after seven days and generally approximately half are rejected because tolerances are exceeded because of wear.
- the composition of the iron-chromium-boron guide plates was as follows:
- Thimbles are castings shaped like a top hat which are part of the support mechanism of the bottle mould.
- the main reason for replacement of the thimble is wear on the top horizontal face and wear in the bore.
- the thimbles are usually made from nickel-boron alloy or tool steel and after two to three weeks of continuous operation are removed and checked for wear.
- molybdenum was increased to over one per cent in order to improve hot hardness.
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Organic Chemistry (AREA)
- Manufacturing & Machinery (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Heat Treatment Of Articles (AREA)
- Powder Metallurgy (AREA)
Priority Applications (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP95919929A EP0763142A4 (en) | 1994-05-30 | 1995-05-29 | IRON-CHROME-BORE ALLOY FOR GLASS MANUFACTURING TOOLS |
KR1019960706767A KR970703441A (ko) | 1994-05-30 | 1995-05-29 | 유리제품 제공 공구용 철-크롬-붕소 합금(iron-chromium-boron alloy for glass manufacturing tools) |
AU25571/95A AU693204B2 (en) | 1994-05-30 | 1995-05-29 | Iron-chromium-boron alloy for glass manufacturing tools |
JP8500075A JPH10500735A (ja) | 1994-05-30 | 1995-05-29 | ガラス製造用工具のための鉄−クロム−ホウ素合金 |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
AUPM5930 | 1994-05-30 | ||
AUPM5930A AUPM593094A0 (en) | 1994-05-30 | 1994-05-30 | Tools for the manufacture of glass articles |
Publications (1)
Publication Number | Publication Date |
---|---|
WO1995033080A1 true WO1995033080A1 (en) | 1995-12-07 |
Family
ID=3780505
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/AU1995/000312 WO1995033080A1 (en) | 1994-05-30 | 1995-05-29 | Iron-chromium-boron alloy for glass manufacturing tools |
Country Status (7)
Country | Link |
---|---|
EP (1) | EP0763142A4 (ja) |
JP (1) | JPH10500735A (ja) |
CN (1) | CN1149322A (ja) |
AU (1) | AUPM593094A0 (ja) |
CA (1) | CA2190953A1 (ja) |
WO (1) | WO1995033080A1 (ja) |
ZA (1) | ZA954364B (ja) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0870849A2 (en) * | 1997-04-07 | 1998-10-14 | A. FINKL & SONS CO. | Tool for glass molding operations and method of manufacture thereof |
WO2020050727A1 (en) * | 2018-09-07 | 2020-03-12 | Milson Foundry Nz Limited | Steel alloy |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP4778735B2 (ja) | 2005-06-24 | 2011-09-21 | 東芝機械株式会社 | ガラス成形用金型の製造方法 |
DE112008000947B4 (de) | 2007-04-10 | 2012-01-19 | Toshiba Kikai K.K. | Glasformgebungsform |
CN106167876A (zh) * | 2016-07-01 | 2016-11-30 | 宜兴市凯诚模具有限公司 | 一种合金玻璃模具及其制造方法 |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3986867A (en) * | 1974-01-12 | 1976-10-19 | The Research Institute For Iron, Steel And Other Metals Of The Tohoku University | Iron-chromium series amorphous alloys |
US4140525A (en) * | 1978-01-03 | 1979-02-20 | Allied Chemical Corporation | Ultra-high strength glassy alloys |
US4318733A (en) * | 1979-11-19 | 1982-03-09 | Marko Materials, Inc. | Tool steels which contain boron and have been processed using a rapid solidification process and method |
US4362553A (en) * | 1979-11-19 | 1982-12-07 | Marko Materials, Inc. | Tool steels which contain boron and have been processed using a rapid solidification process and method |
US4556533A (en) * | 1982-12-02 | 1985-12-03 | Nissan Motor Co., Ltd. | Wear-resistant sintered ferrous alloy and method of producing same |
Family Cites Families (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1493191A (en) * | 1922-11-16 | 1924-05-06 | Golyer Anthony G De | Alloy |
ZA934072B (en) * | 1992-06-19 | 1994-01-19 | Commw Scient Ind Res Org | Rolls for metal shaping |
-
1994
- 1994-05-30 AU AUPM5930A patent/AUPM593094A0/en not_active Abandoned
-
1995
- 1995-05-29 CA CA002190953A patent/CA2190953A1/en not_active Abandoned
- 1995-05-29 JP JP8500075A patent/JPH10500735A/ja active Pending
- 1995-05-29 WO PCT/AU1995/000312 patent/WO1995033080A1/en not_active Application Discontinuation
- 1995-05-29 ZA ZA954364A patent/ZA954364B/xx unknown
- 1995-05-29 CN CN95193342A patent/CN1149322A/zh active Pending
- 1995-05-29 EP EP95919929A patent/EP0763142A4/en not_active Withdrawn
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3986867A (en) * | 1974-01-12 | 1976-10-19 | The Research Institute For Iron, Steel And Other Metals Of The Tohoku University | Iron-chromium series amorphous alloys |
US4140525A (en) * | 1978-01-03 | 1979-02-20 | Allied Chemical Corporation | Ultra-high strength glassy alloys |
US4318733A (en) * | 1979-11-19 | 1982-03-09 | Marko Materials, Inc. | Tool steels which contain boron and have been processed using a rapid solidification process and method |
US4362553A (en) * | 1979-11-19 | 1982-12-07 | Marko Materials, Inc. | Tool steels which contain boron and have been processed using a rapid solidification process and method |
US4556533A (en) * | 1982-12-02 | 1985-12-03 | Nissan Motor Co., Ltd. | Wear-resistant sintered ferrous alloy and method of producing same |
Non-Patent Citations (7)
Title |
---|
DERWENT ABSTRACT, Accession No. 80963A/45, Classes M22, P53, (M27); & JP,A,53 113 207 (DAIDO TOKUSHOKO KK.), 03 October 1978. * |
DERWENT ABSTRACT, Accession No. 87-119554/17, Class M27; & JP,A,62 063 652 (TOYOTA JIDOSHA KK), 20 March 1987. * |
DERWENT ABSTRACT, Accession No. 92-346988/42, Class X12; & SU,A,1 671 729 (KRAMA IND INST), 23 August 1991. * |
DERWENT SOVIET INVENTIONS ILLUSTRATED, SECTION I, CHEMICAL, issued March 1971, Metallurgy, p.10; & SU,A,273 640 (GOROBUNOV et al.), 10 September 1970. * |
PATENT ABSTRACTS OF JAPAN, C-68, page 62; & JP,A,56 065 967 (HITACHI SEISAKUSHO K.K.), 04 June 1981. * |
PATENT ABSTRACTS OF JAPAN, M-60, page 12; & JP,A,54 036 440 (DAIDO SEIKO K.K.), 17 March 1979. * |
See also references of EP0763142A4 * |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0870849A2 (en) * | 1997-04-07 | 1998-10-14 | A. FINKL & SONS CO. | Tool for glass molding operations and method of manufacture thereof |
EP0870849A3 (en) * | 1997-04-07 | 1999-10-13 | A. FINKL & SONS CO. | Tool for glass molding operations and method of manufacture thereof |
WO2020050727A1 (en) * | 2018-09-07 | 2020-03-12 | Milson Foundry Nz Limited | Steel alloy |
Also Published As
Publication number | Publication date |
---|---|
EP0763142A4 (en) | 1997-09-17 |
CN1149322A (zh) | 1997-05-07 |
EP0763142A1 (en) | 1997-03-19 |
JPH10500735A (ja) | 1998-01-20 |
CA2190953A1 (en) | 1995-12-07 |
ZA954364B (en) | 1996-02-19 |
AUPM593094A0 (en) | 1994-06-23 |
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