US3664890A - Method of producing a deep drawn composite article - Google Patents

Method of producing a deep drawn composite article Download PDF

Info

Publication number
US3664890A
US3664890A US13165A US3664890DA US3664890A US 3664890 A US3664890 A US 3664890A US 13165 A US13165 A US 13165A US 3664890D A US3664890D A US 3664890DA US 3664890 A US3664890 A US 3664890A
Authority
US
United States
Prior art keywords
earing
component
deep drawing
composite
alloy
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.)
Expired - Lifetime
Application number
US13165A
Inventor
Joseph Winter
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.)
Olin Corp
Original Assignee
Olin Corp
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 Olin Corp filed Critical Olin Corp
Application granted granted Critical
Publication of US3664890A publication Critical patent/US3664890A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23KSOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K20/00Non-electric welding by applying impact or other pressure, with or without the application of heat, e.g. cladding or plating
    • B23K20/001Non-electric welding by applying impact or other pressure, with or without the application of heat, e.g. cladding or plating by extrusion or drawing
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B21MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21DWORKING OR PROCESSING OF SHEET METAL OR METAL TUBES, RODS OR PROFILES WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21D22/00Shaping without cutting, by stamping, spinning, or deep-drawing
    • B21D22/20Deep-drawing
    • B21D22/203Deep-drawing of compound articles
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10STECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S428/00Stock material or miscellaneous articles
    • Y10S428/922Static electricity metal bleed-off metallic stock
    • Y10S428/923Physical dimension
    • Y10S428/924Composite
    • Y10S428/926Thickness of individual layer specified
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/12All metal or with adjacent metals
    • Y10T428/12493Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.]
    • Y10T428/12736Al-base component
    • Y10T428/1275Next to Group VIII or IB metal-base component
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/12All metal or with adjacent metals
    • Y10T428/12493Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.]
    • Y10T428/12986Adjacent functionally defined components

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Metal Rolling (AREA)

Abstract

A method of producing a deep drawn article wherein earing is eliminated or substantially lessened comprising integrally bonding a first metallic component having characteristic 45* earing propensity after deep drawing to a second metallic component having characteristic 90* earing propensity after deep drawing, and deep drawing, and the article produced thereby.

Description

United States Patent Winter METHOD OF PRODUCING A DEEP DRAWN COMPOSITE ARTICLE lnventor: Joseph Winter, New Haven, Conn.
Assignee: Olin Corporation Filed: Feb. 20, 1970 Appl. No.: 13,165
US. Cl. ..l48/ll.5 A, 29/194 Int. Cl. ..C22f l/04, B32b 15/20 Field of Search 148/1 1.5, 34, 127; 29/194 References Cited UNITED STATES PATENTS l/l970 Miller ..29/194 1 May 23, 1972 Primary Examiner-L. Dewayne Rutledge Assistant ExaminerW. W. Stallard Attorney-Gordon G. Menzies, Richard S. Strickler, Robert H. Bachman, Donald R. Motsko and Thomas P. ODay 57 ABSTRACT 7 Claims, No Drawings METHOD OF PRODUCING A DEEP DRAWN COMPOSITE ARTICLE This invention relates generally to sheet metal and sheet metal processing, and more particularly to deep drawing and deep drawn articles.
Deep drawing of flat sheet metal is a long established and well-known method of producing cup-shaped articles from flat sheets, the process sometimes known as cupping. Depending upon the type of article desired the cupping process may yield the finished article, at least as far as the basic shape is concerned, or only an intermediately shaped item from which other articles are fabricated through further processing of the basic cup, or through additional manufacturing in which the cup is merely a component of an assemblage. In any event, the formation of the cup is a critical step in any of the above processes; hence the nature and practice of the formation of the cup is of vital importance to the art of deep drawing of sheet metal.
This art has long been troubled by a characteristic of sheet metal known an earing which manifests itself as a scalloped appearance around the top edge of the formed cup. The seallops, or cars, are formed during the deep drawing step in the fabrication of the cup, and represent an almost universally undesirable feature of the article, whether it be finally shaped or intended for further processing of manufacturing. The result is that the ears must be eliminated in order to present a smooth or flat upper lip on the cup. This of course necessitates machining in the form of shearing or cutting, followed by additional finishing in some situations, with an attendant increase in production costs and higher costs resulting from increased material waste. It is evident, therefore, that the reduction or elimination of earing in the deep drawing of sheet metal represents a major contribution to this art.
To facilitate an understanding of the process of this invention, it becomes necessary to examine the causative aspects of the problem of earing. Generally speaking, earing is the manifestation of property anisotropy caused by crystallographic preferredness or by granular fibrous texturing within sheet or strip materials. More particularly, earing results as a result of the deep drawing of metal sheet or strip in which there exists a preferential directionality of ductility properties as distinguished from isotropy. The directionality of these ductility properties is a function either of atom slippage along slip lines within the normal texture of the metal grains, or of mechanical preferredness of the fibrous grain structure of the metal. The effect of the property anisotropy is that the physical properties of the metal are not the same in all directions, but rather vary in accordance with the directionality of the crystallographic structure or the fibrous grain texturing. The physical manifestation of this affect is that upon subsequent cold work by deep drawing, the metal cannot elongate or stretch as well in one direction relative to the original rolling direction as it can in another, with the result that troughs appear around the upper rim of the cup in those directions where the metal exhibits a greater resistance to stretching. Because of crystallographic symmetry this phenomenon results in ears oriented either paralled and perpendicular to the direction of rolling of the metal referred to as 90 earing, or with the ears oriented intermediate the quadrants defined by the rolling direction, referred to as 45 earing. It is, of course, these ears which make the product commercially uneconomic by necessitating additional processing with concomitant higher material and labor costs in order to provide an acceptable product.
From classical metallurgy it is known that in the face centered cubic metals, such as aluminum, copper, and gamma iron etc., and their alloys, that cold rolling increases the propensity for 45 caring; and that recrystallizing increases the propensity for 90 earing. Nevertheless in certain alloys the alloying elements can produce an overriding effect such that the alloys will display characteristic behavior.
The factors which effect earing within any particular alloy are the composition, the casting practice, preheating practice, hot rolling temperature and technique, slab and strip interannealing, cold rolling reduction and final annealing practices.
The above can be used to predict the ductility directionality of the composite of a multiple alloy system and thereby provide a complex system wherein earing is controlled.
It is therefore a principal object of the present invention to provide a method for producing a deep drawn article wherein earing is eliminated or substantially lessened during deep drawing.
It is a further object of the present invention to provide a new and improved article characterized by the elimination or reduction of earing after deep drawing.
Still further objects and advantages of the present invention will appear hereafter.
The process of the present invention comprises (A) providing a metal component having a characteristic 45 earing propensity, with respect to rolling direction after processing and deep drawing, and a metal component having a characteristic earing propensity, with respect to rolling direction, after processing and deep drawing, (B) integrally bonding together said components to form an integrally bonded composite, (C) cold rolling and annealing said composite in order to assure that the components attain their characteristic earing propensity and (D) deep drawing the composite.
Naturally, the present invention contemplates a multiple component composite wherein the contribution of each component is predictable.
It has been found that a deep drawn article in accordance with the present invention possesses excellent strength characteristics and with earing substantially lessened, or eliminated, thereby promoting increased economy due to reduced trimming operations and attendant generated scrap.
As aforementioned, the type and degree of earing propensity is dependent upon the entire thermal and mechanical treatment of the metal or alloy, and may even vary for the same alloy composition.
Copper, aluminum, iron and alloys thereof, are suitable in the present invention and are the preferred metals. The particular metal or alloy employed is not critical so long as each component will possess different earing propensities after deep drawing. in general, however, the material is selected from the group consisting of copper, aluminum, iron, and alloys thereof.
The earing propensity for any particular metal or alloy may be readily determined by acturally deep drawing various metals and alloys in the cold rolled or annealed condition. Thus, which earing propensities will occur is predetermined for a metal or alloy, having a given history of prior mechanical and thermal treatment, prior to practicing the present invention.
Generally, but not necessarily, bonding is accomplished by hot rolling the components together. The degree of reduction during hot rolling is not especially critical to this invention but must be sufficient to form an integrally bonded composite. Likewise, the thicknesses of the individual components prior to hot rolling are not especially critical to this invention but generally range from 5 mils to 1 inch in thickness, with the proportion of one component to the total thickness of both components ranging from about 5.0 percent to about 50.0 percent.
The degree of reduction of the composite during cold rolling, however, may be critical as having an influence upon the caring propensity dun'ng deep drawing, and must be determined experimentally for a given metal or alloy as aforementioned. Generally, however the degree of cold reduction ranges from 10.0 to 80.0 percent.
It is preferred that only one of said components recrystallizes during the annealing step just before deep drawing since this will assure the characteristic 90 earing propensity of this component. Naturally, the annealing temperature is dependent upon the particular metals or alloys employed, and the degree to which they have been cold reduced. In general, however, depending upon which metals or alloys comprise the composite, the composite is annealed at from 300 to l,400 F for about 1 minute to 5 hours wherein said composite has been cold reduced from about 10.0 to 80.0 percent.
The relative thicknesses of each component of the composite prior to deep drawing should be such as to provide the requisite reduction in earing for a given operation. Naturally a thinner component may be employed wherein a given propensity is low when bonded to a component of greater thickness in which the caring propensity is comparatively higher.
As aforementioned, the degree and type of earing propensity is determined by a variety of factors and therefore the exact alloy to be employed is determined by the prior mechanical working and thermal treatments given to a specified alloy. Naturally therefore a number of permissible alloy combinations of copper, iron or aluminum may be readily applicable to forming the composite.
A secondary purpose may also be served wherein in applications to different environments is easily provided for by the provision of the composite composed of different metals or alloys.
The present invention is more readily apparent from a consideration of the following illustrative examples.
EXAMPLE 1 of the same prior mechanical and thermal heating were likewise rolled together and annealed, chemically separated, then deep drawn to show the earing propensities of each alloy after deep drawing into articles having the same dimensions. The results of the varying earing propensities of the two composites and of the alloy components after deep drawing are shown in the following table.
TAB LE Anneal- Eating ing Thiekdiree- *Ear temp., ness, tion, height, Sample Material F./1 hr. in. degree percent A Composite of copper 320 0.061 90 3.8
alloy 110 bonded to aluminum alloy 1100 (50% copper plus 50% aluminum). A Copper alloy 110. 320 0. 02!) 90 7. 8 A Aluminum alloy 320 07 031 45 3. 7
1100. B Composite of copper 320 0.06l 45 4.7
alloy 110 bonded to aluminum alloy 1100 (50% copper plus 50% aluminum). B-. Copper alloy 110.... 320 0.029 45 6.3 B Aluminum alloy 320 0. 031 45 3.4
After deep drawing. *Percentage of average height of the cup.
earing propensities after heat treating and deep drawing significantly reduces the ear height of the finished article, thereby promoting a reduction in the amount of scrap generated by trimming of the article with a resultant increase ineconomy.
EXAMPLE 2 A sample of aluminum alloy 1 100 was clad to half its width to copper alloy 1 l0 and processed in a manner after samples A in example 1, except that the copper is about 25 percent of the thickness of the composite and the aluminum alloy is about 75 percent of the thickness of the composite wherein these components are bonded. A blanked disc was prepared wherein half of the blank was clad and wherein the thickness of the entire disc was uniform, i.e., the copper was inlaid. The disc was cupped as described above and the results show that the monolithic aluminum portion has high ears; whereas the clad metal has no cars due to the method of the present invention.
This invention may be embodied in other forms or carried out in other ways without departing from the spirt or essential characteristics thereof. The present embodiment is therefore to be considered as in all respects illustrative and not restrictive, the scope of the invention being indicated by the appended claims, and all changes which come within the meaning and range of equivalency are intended to be embraced therein.
What is claimed is:
l. A method of producing a deep drawn article wherein earing is eliminated or substantially lessened, comprising:
A. providing a metal component having a characteristic 45 earing propensity, with respect to rolling direction after processing and deep drawing, and a metal component having a characteristic earing propensity, with respect to rollin direction after processing and deep drawing, B. hot ro ing together said components to form an integrally bonded composite,
C. cold rolling and annealing said composite in order to assure that the components attain their characteristic earing propensity, and
D. deep drawing the composite.
2. The method of claim 1 wherein said annealing temperature is from 300 to l,400 F.
3. The method of claim 1 wherein at least one additional metallic component is integrally bonded in step (B) to form a multi-component article.
4. The method of claim 2 wherein said first component and said second component ranges from 5 mils to 1 inch in thickness before step C.
5. The method of claim 4 wherein one of said components is from 5.0 to 50.0 percent of the total thickness of both of said components.
6. The method of claim 5 wherein said first metallic component and said second metallic component are selected from the group consisting of copper, aluminum, iron, and alloys thereof.
7. The method of claim 6 wherein said first metallic com ponent is copper and said second metallic component is aluminum.

Claims (6)

  1. 2. The method of claim 1 wherein said annealing temperature is from 300* to 1,400* F.
  2. 3. The method of claim 1 wherein at least one additional metallic component is integrally bonded in step (B) to form a multi-component article.
  3. 4. The method of claim 2 wherein said first component and said second component ranges from 5 mils to 1 inch in thickness before step C.
  4. 5. The method of claim 4 wherein one of said components is from 5.0 to 50.0 percent of the total thickness of both of said components.
  5. 6. The method of claim 5 wherein said first metallic component and said second metallic component are selected from the group consisting of copper, aluminum, iron, and alloys thereof.
  6. 7. The method of claim 6 wherein said first metallic component is copper and said second metallic component is aluminum.
US13165A 1970-02-20 1970-02-20 Method of producing a deep drawn composite article Expired - Lifetime US3664890A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US1316570A 1970-02-20 1970-02-20

Publications (1)

Publication Number Publication Date
US3664890A true US3664890A (en) 1972-05-23

Family

ID=21758638

Family Applications (1)

Application Number Title Priority Date Filing Date
US13165A Expired - Lifetime US3664890A (en) 1970-02-20 1970-02-20 Method of producing a deep drawn composite article

Country Status (1)

Country Link
US (1) US3664890A (en)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4005665A (en) * 1974-05-08 1977-02-01 Nippon Steel Corporation Method for making press-working blanks with reduced ear occurrence
EP0592211A1 (en) * 1992-10-09 1994-04-13 The Boc Group, Inc. Seamless cylinder shell construction
US6214135B1 (en) * 1996-02-08 2001-04-10 Showa Aluminum Corporation Entry board for drilling small holes, a method of making the same and a method for drilling small holes through a printed circuit board by using said entry board
US20050112344A1 (en) * 2003-08-20 2005-05-26 Redfern Sean M. Apparatus and method for use in printed circuit board drilling applications
US8323798B2 (en) 2007-09-28 2012-12-04 Tri-Star Laminates, Inc. Systems and methods for drilling holes in printed circuit boards
US20140335992A1 (en) * 2013-05-08 2014-11-13 Schaeffler Technologies Gmbh & Co. Kg Rotary power transfer disconnect device

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3490124A (en) * 1967-02-07 1970-01-20 Texas Instruments Inc Composite metal layers for fabricating deep drawn articles

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3490124A (en) * 1967-02-07 1970-01-20 Texas Instruments Inc Composite metal layers for fabricating deep drawn articles

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4005665A (en) * 1974-05-08 1977-02-01 Nippon Steel Corporation Method for making press-working blanks with reduced ear occurrence
EP0592211A1 (en) * 1992-10-09 1994-04-13 The Boc Group, Inc. Seamless cylinder shell construction
US5330091A (en) * 1992-10-09 1994-07-19 The Boc Group, Inc. Seamless cylinder shell construction
US5485736A (en) * 1992-10-09 1996-01-23 The Boc Group, Inc. Seamless cylinder shell construction
US6214135B1 (en) * 1996-02-08 2001-04-10 Showa Aluminum Corporation Entry board for drilling small holes, a method of making the same and a method for drilling small holes through a printed circuit board by using said entry board
US20050112344A1 (en) * 2003-08-20 2005-05-26 Redfern Sean M. Apparatus and method for use in printed circuit board drilling applications
US8323798B2 (en) 2007-09-28 2012-12-04 Tri-Star Laminates, Inc. Systems and methods for drilling holes in printed circuit boards
US8802237B2 (en) 2007-09-28 2014-08-12 Tri-Star Laminates, Inc. Entry sheet for drilling holes in printed circuit boards
US20140335992A1 (en) * 2013-05-08 2014-11-13 Schaeffler Technologies Gmbh & Co. Kg Rotary power transfer disconnect device

Similar Documents

Publication Publication Date Title
US2294648A (en) Method of rolling magnesium-base alloys
US2857269A (en) Titanium base alloy and method of processing same
US3392062A (en) Process of producing heat-treatable strips and sheets from heat-treatable aluminum alloys with a copper content of less than 1%
US3169085A (en) Method of producing titanium base strip
US3219491A (en) Thermal treatment of aluminum base alloy product
US3219492A (en) Thermal treatment of aluminum base alloy product
JPS5964735A (en) Light metal base alloy and manufacture
US3354531A (en) Process for making hollow articles by differential heat treatment
US3664890A (en) Method of producing a deep drawn composite article
US3994695A (en) Composite aluminum brazing sheet
US2676123A (en) Treatment of brass
US3607456A (en) Deep drawing steel and method of manufacture
US2940881A (en) Method for making cbe-on-face magnetic steel
US2637672A (en) Process of producing bolts
US3966506A (en) Aluminum alloy sheet and process therefor
US2067076A (en) Method of controlling grain structure in alloys and articles produced thereby
US3318738A (en) Method of fabricating non-earing aluminum
US3929516A (en) Process for producing Cu-base alloys
US3006758A (en) Zinc alloy
US2095580A (en) Steel strip and its production
US3788902A (en) Process for improving the elongation of grain refined copper base alloys
US3814590A (en) Aluminous metal articles and aluminum base alloys
US3661657A (en) Method for making aluminum sheet
US2210671A (en) Copper base alloy
US3717513A (en) Process for the production of composite sheets