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US2443170A - Reinforced sheet metal - Google Patents

Reinforced sheet metal Download PDF

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Publication number
US2443170A
US2443170A US456669A US45666942A US2443170A US 2443170 A US2443170 A US 2443170A US 456669 A US456669 A US 456669A US 45666942 A US45666942 A US 45666942A US 2443170 A US2443170 A US 2443170A
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US
United States
Prior art keywords
sheet
ridges
crests
sheets
grooves
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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.)
Expired - Lifetime
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US456669A
Inventor
Richard S Smith
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Reconstruction Finance Corp
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Reconstruction Finance Corp
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Publication date
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Priority to US456669A priority Critical patent/US2443170A/en
Application granted granted Critical
Publication of US2443170A publication Critical patent/US2443170A/en
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Expired - Lifetime legal-status Critical Current

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Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B21MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21HMAKING PARTICULAR METAL OBJECTS BY ROLLING, e.g. SCREWS, WHEELS, RINGS, BARRELS, BALLS
    • B21H8/00Rolling metal of indefinite length in repetitive shapes specially designed for the manufacture of particular objects, e.g. checkered sheets
    • B21H8/005Embossing sheets or rolls
    • EFIXED CONSTRUCTIONS
    • E04BUILDING
    • E04CSTRUCTURAL ELEMENTS; BUILDING MATERIALS
    • E04C2/00Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels
    • E04C2/30Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by the shape or structure
    • E04C2/32Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by the shape or structure formed of corrugated or otherwise indented sheet-like material; composed of such layers with or without layers of flat sheet-like material
    • 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
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/49616Structural member making
    • Y10T29/49623Static structure, e.g., a building component
    • Y10T29/49632Metal reinforcement member for nonmetallic, e.g., concrete, structural element
    • 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
    • Y10T428/1241Nonplanar uniform thickness or nonlinear uniform diameter [e.g., L-shape]
    • 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.]
    • Y10T428/12771Transition metal-base component
    • Y10T428/12861Group VIII or IB metal-base component
    • Y10T428/12951Fe-base component
    • Y10T428/12972Containing 0.01-1.7% carbon [i.e., steel]

Definitions

  • the improved characteristics of stiffness and strength of the metal sheets of the present invention are attributable to a beneficial redistribution of the material with respect to neutral axes lying in a plane medially of the sheet.
  • the particular application of the principles of the present invention which is set forth herein by way of example has reference to a metal sheet, and in general the formations are intended to be produced by the cold rolling of hat sheets.
  • the improvements of the present invention may be appliedA to both ferrous and non-ferrous metals.
  • the successful attainment of the Vobjects of the present invention has been demonstrated in the case of stainless,r alloy and carbon steels, and various aluminum alloys.
  • Fig. 1 is a transverse cross-sectional View of a portion of a sheet having formations in its opposite faces;
  • Fig. 2 is a similar view of a sheet having formations in one face only;
  • Fig. 3 is a view similar to Fig. 1 but with variant formations in its opposite faces;
  • Fig ⁇ 4 is. an elevational view of the upper surface of the sheet of Fig. 1; y
  • Fig. 5 is an elevational view of thelower surface of the sheet of Fig, 1, and;
  • Fig. 6 is an elevational view of the upper surface of the sheet of Fig. 3. l
  • the angles of the ⁇ faces of the metal sheet between the ridges II' and the groovesor valleys I2 are such that the height of eachridge II or its distance from the neutral axis of the crosssection of the sheet is a minimum when the adjacent sinuous grooves are closest I thereto and reaches a maximum when adjacent sinuous grooves are most remote therefrom.
  • Reference to Fig. 4 shows that the grooves orvalleys I2 are so arranged that each adjacent pair either diverges or converges simultaneously. l
  • Emcient production of a sheet having the surface formations of the .present invention is facilitated, and in fact the desired strength and stiffness characteristics are augmented, ⁇ by reversing the formations of rthe reverse side of the sheet, shown in Fig. 5, as compared with the obverse side shown in Fig. 4.
  • the underside of thel sheet of Fig. 1, as appears 3 from Fig. 5, has sinuous ridges designated il and linear parallel grooves or valleys I5.
  • Fig. 2 shows a sheet body 20'having in its upper surface formations identical with those of the Upper surface of Fig. 1 and accordingly like characters of reference have been applied thereto.
  • , is at.
  • the ratios of strength and stiffness to unit weight will not be as high in the sheet of Fig. 2 as in the sheet of Fig. 1 but they will be substantially higher than in the case of a plain sheet.
  • Sheets of the kind shown in Fig. 2 may be desirably employed in the formation of airfoils or other skin surfacing of aircraft. In such cases, obviously, the plain uninterrupted surface of the sheet will be exposed to the air stream to render the airfoil or other aircraft part aerodynamically emcient.
  • the production of a sheet with one plain surface may likewise be desired for purely aesthetic reasons, or to facilitate decoration.
  • Fig. 3 I have illustrated a form of surface treatment similar to that of Fig. 1 but characterized chiefly by the fact that the ridges are less sharply defined. I have found the crosssection of Fig. 3 to be more satisfactory, from various standpoints, when applying the principles of my invention to heavier gauge metals.
  • the crests are lineal and parallel and are designated 3l. Despite this parallelism and lineality, the crests 3i ndulate in a vertical direction along their lengths. This is evidenced by the two elevations of the crests 3i appearing at the left and right sides of the cross-section, Fig. 3.
  • the dot and dash construction lines indicate the crests 3i and the shaded sinuous portions therebetween designate grooves or valleys 32.
  • the sinuous grooves'or valleys shown in Fig. 6 are at a condition of maximum divergence with respectjto the central crests 3l and are at a position of minimum spacing with respect to the ridges 3
  • the under surface of sheet body 30 of Fig. 3 is to some extent complementary to the upper surface.
  • the sheet body'30 has lineal parallel grooves or valleys 34 and sinuous ridges 35. The effect of this arrangement in the production of the variation in height of the crests ,3l and the variation in the depths in the grooves or the valleys 3,4 is ⁇ the same in principle as in the case of Fig. 1.
  • a reinforced structural sheet having longitudinal corrugations presenting ridges at opposite sides thereof, the crests of the ridges at one side extending along straight parallel lines and tlie crests of the ridges at the opposite sides being generally parallel but pursuing a predetermined regularly recurring sinuous course as viewed perpendicularly to said side of the sheet.
  • a structurally reinforced metallic sheet having a plurality of adjacent longitudinal corrugations, the ridgeof each corrugation comprising an undulating line as viewed in longitudinal cross-section, the crests of the undulating corrugations being staggered with respect to the crests of adjacent longitudinal corrugations, said corrugations having portions of maximum width at said crests and portions of minimum width at their nodes with adjacent staggered corrugations interfitting laterally.
  • a reinforced structural sheet having a plurality of longitudinal, generally parallel ridges therein, said ridges having predetermined regularly recurring variations in amplitude along their lengths, the variations in amplitude being staggered with respect to the variations in amplitude of ridges next adjacent thereto with the ridges interiitting laterally and all longitudinal cross sections through said sheet produce undulating contours and the sheet is thus reinforced against iiexure both transversely and longitudinally.
  • a reinforced structural sheet having a plurality of longitudinal. generally parallel ridges therein, said ridges having predetermined regularlyrecurring variations in width along their lengths, the variations in width being staggered with respect tothe variations in width of ridges next adjacent thereto with the ridges interiltting laterally and all longitudinal cross sections through said sheet produce undulating contours and the sheet is thus reinforced against exure both transversely and longitudinally.

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  • Engineering & Computer Science (AREA)
  • Architecture (AREA)
  • Mechanical Engineering (AREA)
  • Civil Engineering (AREA)
  • Structural Engineering (AREA)
  • Laminated Bodies (AREA)

Description

, Patented .lune 8, 1948 REINFORCED SHEET METAL Richard S. Smith, Buffalo, N. Y., assignor, by mesne assignments, to Reconstruction Finance Corporation, New York the United States N. Y., a corporation of Application August 29, 1942, Serial No. 456,669 f l This invention relates to sheets 'of metal of various constituencies having improved characteristics oi' strength and stiffness when compared with at sheets of the same material lof equal unit weight.
The improved characteristics of stiffness and strength of the metal sheets of the present invention are attributable to a beneficial redistribution of the material with respect to neutral axes lying in a plane medially of the sheet. The particular application of the principles of the present invention which is set forth herein by way of example has reference to a metal sheet, and in general the formations are intended to be produced by the cold rolling of hat sheets. In the general field of metallic sheets the improvements of the present invention may be appliedA to both ferrous and non-ferrous metals. The successful attainment of the Vobjects of the present invention has been demonstrated in the case of stainless,r alloy and carbon steels, and various aluminum alloys.
The use of plain corrugated sheets of metal, chiefly steel, has been thoroughly explored and fairly widely used. This attempt at strengthening steel is ineffective in all excepting very special cases, since its only effect is to stiffen the sheet when it is loaded as a beam with the corrugations running parallel to the direction of the beam. If loaded at right angles to this direction a corrugated sheet has very much less stiffness than a plain sheet since the corrugations merely open up or flatten out. Likewise, a corrugated sheet has far less resistance to buckling under compressive loads at right angles to the corrugations and tensile forces in this direction do not meet substantial resistance until the sheet has y been stretched to a substantially flat uncorrugated condition. Treating metal sheets by corrugation methods increases the weight Iper unit of area as compared with the flat sheet, while treatment of sheets according to the present invention, by actual displacement of metal, de-4 teristics are imparted to the sheet, when compared with a fiat sheet of the same unit weight and material, and this is true regardless of the direction of application of compressive buckling loads, tensile loads or iiexural loads.' Strengthenl ing of a metal sheet in accordance with the prin- 4 Claims. (Cl. 29,-180) ciples of the present invention may be eifected in a. varietyv of ways, as is` exemplified by the various alternative forms illustrated in the accompanying drawing, and described below. It is to be understood that surface formations other than those illustrated in detail will occur to those skilled inthe art and the principles of the present invention are not to be limited otherwise than as defined in the appended claims.
`In the drawingsz" Fig. 1 is a transverse cross-sectional View of a portion of a sheet having formations in its opposite faces;
Fig. 2 is a similar view of a sheet having formations in one face only;
Fig. 3 is a view similar to Fig. 1 but with variant formations in its opposite faces;
Fig` 4 is. an elevational view of the upper surface of the sheet of Fig. 1; y
Fig. 5 is an elevational view of thelower surface of the sheet of Fig, 1, and;
Fig. 6 is an elevational view of the upper surface of the sheet of Fig. 3. l
Throughout the several figures of the drawing, like characters of reference denote like parts and in Figs. 1, 4 and 5 the numeral I0 designates y 'and disposed midway between adjacent ridges III, excepting for their regularly recurring sinuosity.
The angles of the` faces of the metal sheet between the ridges II' and the groovesor valleys I2 are such that the height of eachridge II or its distance from the neutral axis of the crosssection of the sheet is a minimum when the adjacent sinuous grooves are closest I thereto and reaches a maximum when adjacent sinuous grooves are most remote therefrom.l Reference to Fig. 4 shows that the grooves orvalleys I2 are so arranged that each adjacent pair either diverges or converges simultaneously. l
Emcient production of a sheet having the surface formations of the .present invention is facilitated, and in fact the desired strength and stiffness characteristics are augmented, `by reversing the formations of rthe reverse side of the sheet, shown in Fig. 5, as compared with the obverse side shown in Fig. 4. Stated generally, the underside of thel sheet of Fig. 1, as appears 3 from Fig. 5, has sinuous ridges designated il and linear parallel grooves or valleys I5.
By reason of the relationship of the two faces of the sheet of Fig. 1, a maximum redistribution of the material of the sheet body I is accomplished with a minimum of colning or cold-forging. The production of the desired surface formations cannot be effected by a mere bending of the sheet body; first, by reason of the sinuosity of the grooves on one face of the body and the ridges on the other, and second, by reason of the desired sharp deiinitionof the crests of the ridges. This sharp definition contributes materially to the moment of inertia of the crosssection, which is a direct measure of the resistance of the cross-section to bending.
Fig. 2 shows a sheet body 20'having in its upper surface formations identical with those of the Upper surface of Fig. 1 and accordingly like characters of reference have been applied thereto. The underside of the sheet body 20, designated 2|, is at. The ratios of strength and stiffness to unit weight will not be as high in the sheet of Fig. 2 as in the sheet of Fig. 1 but they will be substantially higher than in the case of a plain sheet. Sheets of the kind shown in Fig. 2 may be desirably employed in the formation of airfoils or other skin surfacing of aircraft. In such cases, obviously, the plain uninterrupted surface of the sheet will be exposed to the air stream to render the airfoil or other aircraft part aerodynamically emcient. The production of a sheet with one plain surface may likewise be desired for purely aesthetic reasons, or to facilitate decoration.
In Fig. 3 I have illustrated a form of surface treatment similar to that of Fig. 1 but characterized chiefly by the fact that the ridges are less sharply defined. I have found the crosssection of Fig. 3 to be more satisfactory, from various standpoints, when applying the principles of my invention to heavier gauge metals.
In the upper or obverse face of the sheet of Fig. 3,
the body of which is designated 30, the crests are lineal and parallel and are designated 3l. Despite this parallelism and lineality, the crests 3i ndulate in a vertical direction along their lengths. This is evidenced by the two elevations of the crests 3i appearing at the left and right sides of the cross-section, Fig. 3.
In Fig. 6 the dot and dash construction lines indicate the crests 3i and the shaded sinuous portions therebetween designate grooves or valleys 32. Note that4 as shown in Fig. 3 the sinuous grooves'or valleys shown in Fig. 6 are at a condition of maximum divergence with respectjto the central crests 3l and are at a position of minimum spacing with respect to the ridges 3| lying on each side of the central ridge ofl Fig. 3. v
As in the case of Fig. 1, the under surface of sheet body 30 of Fig. 3 is to some extent complementary to the upper surface. At its under side the sheet body'30 has lineal parallel grooves or valleys 34 and sinuous ridges 35. The effect of this arrangement in the production of the variation in height of the crests ,3l and the variation in the depths in the grooves or the valleys 3,4 is` the same in principle as in the case of Fig. 1.
It is by -virtue of this variation in crest and groove amplitude that a cross-section of any of the sheets, Figs. 1, 2 or 3, taken at right angles 4 to those cross-sections, will similarly produce an undulating cross-section. It is this fact that gives the sheet increased flexural strength with respect to cross-sections taken along the direction of the general extent of the ridges and grooves.
Referring to preferred proportion of the formation, I have successfully demonstrated the benets of the invention in cases where the distance between respective crests along a single ridge bore ratios varying between 4 to 1 and 8 to 1 with respect to the lateral pitch of adjacent ridges.
What is claimed is:
1. A reinforced structural sheet having longitudinal corrugations presenting ridges at opposite sides thereof, the crests of the ridges at one side extending along straight parallel lines and tlie crests of the ridges at the opposite sides being generally parallel but pursuing a predetermined regularly recurring sinuous course as viewed perpendicularly to said side of the sheet.
2. A structurally reinforced metallic sheet having a plurality of adjacent longitudinal corrugations, the ridgeof each corrugation comprising an undulating line as viewed in longitudinal cross-section, the crests of the undulating corrugations being staggered with respect to the crests of adjacent longitudinal corrugations, said corrugations having portions of maximum width at said crests and portions of minimum width at their nodes with adjacent staggered corrugations interfitting laterally.
3. A reinforced structural sheet having a plurality of longitudinal, generally parallel ridges therein, said ridges having predetermined regularly recurring variations in amplitude along their lengths, the variations in amplitude being staggered with respect to the variations in amplitude of ridges next adjacent thereto with the ridges interiitting laterally and all longitudinal cross sections through said sheet produce undulating contours and the sheet is thus reinforced against iiexure both transversely and longitudinally.
r 4. A reinforced structural sheet having a plurality of longitudinal. generally parallel ridges therein, said ridges having predetermined regularlyrecurring variations in width along their lengths, the variations in width being staggered with respect tothe variations in width of ridges next adjacent thereto with the ridges interiltting laterally and all longitudinal cross sections through said sheet produce undulating contours and the sheet is thus reinforced against exure both transversely and longitudinally.
. RICHARD S. SMITH.
REFERENCES CITED The following references are of record in the file of this patent:
UNITED STATES PATETS Dunajeif 'Man 4, 1941
US456669A 1942-08-29 1942-08-29 Reinforced sheet metal Expired - Lifetime US2443170A (en)

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Cited By (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2571573A (en) * 1944-07-27 1951-10-16 Melotte Ecremeuses Metallic surface for butter churns
US2735520A (en) * 1956-02-21 Collins
US2741834A (en) * 1952-06-26 1956-04-17 Macdonald S Reed Method of forming integrally stiffened panels
US2848846A (en) * 1956-04-30 1958-08-26 Pittsburgh Plate Glass Co Glass bending molds
US2991544A (en) * 1957-05-07 1961-07-11 American Can Co Bright surfaced metal sheets and method of producing same
US3059733A (en) * 1955-07-13 1962-10-23 Peter S Pedersen Reinforced panel sheets
US3165815A (en) * 1961-07-28 1965-01-19 Voest Ag Process for the manufacture of sections
US3190822A (en) * 1961-01-09 1965-06-22 Burnham John Process for electrolytically etching valve metal surfaces
US4857412A (en) * 1986-01-16 1989-08-15 Paul Fleury Method for forming a planar sheet or plate to a curved shape
US20100127125A1 (en) * 2008-08-05 2010-05-27 Ming Li Metal sheets and plates having friction-reducing textured surfaces and methods of manufacturing same
USD645258S1 (en) * 2011-02-01 2011-09-20 The Procter & Gamble Compay Paper product
USD652631S1 (en) 2010-08-09 2012-01-24 The Procter & Gamble Company Paper product
USD663126S1 (en) * 2010-08-27 2012-07-10 Lapinid Jr Narciso Portion of a vacuum cleaner
US20140311208A1 (en) * 2010-12-28 2014-10-23 Kyocera Document Solutions Inc. Method of manufacturing a sheet metal frame
USD718537S1 (en) * 2013-09-26 2014-12-02 First Quality Tissue, Llc Paper product with surface pattern
US20150357053A1 (en) * 2014-06-10 2015-12-10 Westinghouse Electric Company Llc Crush resistant nuclear fuel assembly support grid
US10132042B2 (en) 2015-03-10 2018-11-20 The Procter & Gamble Company Fibrous structures
US11408129B2 (en) 2018-12-10 2022-08-09 The Procter & Gamble Company Fibrous structures
USD985948S1 (en) * 2018-10-04 2023-05-16 The Procter & Gamble Company Sheet with pattern
US12203221B2 (en) 2014-08-05 2025-01-21 The Procter & Gamble Company Fibrous structures

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US662567A (en) * 1900-04-25 1900-11-27 Isabella Von Lipowska Metal bearing-plate.
US1450357A (en) * 1920-07-01 1923-04-03 Earl W Curtis Crosscut sawing machine
US1766857A (en) * 1928-11-12 1930-06-24 William E Van Dorn Metal car end
US1944990A (en) * 1931-01-28 1934-01-30 Costruzioni Meccaniche Breda E Aircraft covering
US1996004A (en) * 1933-11-28 1935-03-26 Nat Steel Car Corp Ltd Corrugated structural unit
US2154597A (en) * 1937-01-23 1939-04-18 Harrington & King Perforating Floor tread
US2233592A (en) * 1938-07-21 1941-03-04 Commercial Ingredients Corp Resilient sheet

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US662567A (en) * 1900-04-25 1900-11-27 Isabella Von Lipowska Metal bearing-plate.
US1450357A (en) * 1920-07-01 1923-04-03 Earl W Curtis Crosscut sawing machine
US1766857A (en) * 1928-11-12 1930-06-24 William E Van Dorn Metal car end
US1944990A (en) * 1931-01-28 1934-01-30 Costruzioni Meccaniche Breda E Aircraft covering
US1996004A (en) * 1933-11-28 1935-03-26 Nat Steel Car Corp Ltd Corrugated structural unit
US2154597A (en) * 1937-01-23 1939-04-18 Harrington & King Perforating Floor tread
US2233592A (en) * 1938-07-21 1941-03-04 Commercial Ingredients Corp Resilient sheet

Cited By (32)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2735520A (en) * 1956-02-21 Collins
US2571573A (en) * 1944-07-27 1951-10-16 Melotte Ecremeuses Metallic surface for butter churns
US2741834A (en) * 1952-06-26 1956-04-17 Macdonald S Reed Method of forming integrally stiffened panels
US3059733A (en) * 1955-07-13 1962-10-23 Peter S Pedersen Reinforced panel sheets
US2848846A (en) * 1956-04-30 1958-08-26 Pittsburgh Plate Glass Co Glass bending molds
US2991544A (en) * 1957-05-07 1961-07-11 American Can Co Bright surfaced metal sheets and method of producing same
US3190822A (en) * 1961-01-09 1965-06-22 Burnham John Process for electrolytically etching valve metal surfaces
US3165815A (en) * 1961-07-28 1965-01-19 Voest Ag Process for the manufacture of sections
US4857412A (en) * 1986-01-16 1989-08-15 Paul Fleury Method for forming a planar sheet or plate to a curved shape
US20140248453A1 (en) * 2008-08-05 2014-09-04 Alcoa Inc. Metal sheets and plates having friction-reducing textured surfaces and methods of manufacturing same
US9297394B2 (en) * 2008-08-05 2016-03-29 Alcoa Inc. Metal sheets and plates having friction-reducing textured surfaces and methods of manufacturing same
US20100127125A1 (en) * 2008-08-05 2010-05-27 Ming Li Metal sheets and plates having friction-reducing textured surfaces and methods of manufacturing same
US8578747B2 (en) 2008-08-05 2013-11-12 Alcoa Inc. Metal sheets and plates having friction-reducing textured surfaces and methods of manufacturing same
US8444092B2 (en) * 2008-08-05 2013-05-21 Alcoa Inc. Metal sheets and plates having friction-reducing textured surfaces and methods of manufacturing same
USD652632S1 (en) 2010-08-09 2012-01-24 The Procter & Gamble Company Paper product
USD652631S1 (en) 2010-08-09 2012-01-24 The Procter & Gamble Company Paper product
USD663126S1 (en) * 2010-08-27 2012-07-10 Lapinid Jr Narciso Portion of a vacuum cleaner
US20140311208A1 (en) * 2010-12-28 2014-10-23 Kyocera Document Solutions Inc. Method of manufacturing a sheet metal frame
US10245864B2 (en) * 2010-12-28 2019-04-02 Kyocera Document Solutions Inc. Method of manufacturing a sheet metal frame
USD645258S1 (en) * 2011-02-01 2011-09-20 The Procter & Gamble Compay Paper product
USD718537S1 (en) * 2013-09-26 2014-12-02 First Quality Tissue, Llc Paper product with surface pattern
US20150357053A1 (en) * 2014-06-10 2015-12-10 Westinghouse Electric Company Llc Crush resistant nuclear fuel assembly support grid
US10458069B2 (en) 2014-08-05 2019-10-29 The Procter & Gamble Compay Fibrous structures
US10472771B2 (en) 2014-08-05 2019-11-12 The Procter & Gamble Company Fibrous structures
US10822745B2 (en) 2014-08-05 2020-11-03 The Procter & Gamble Company Fibrous structures
US11725346B2 (en) 2014-08-05 2023-08-15 The Procter & Gamble Company Fibrous structures
US12203221B2 (en) 2014-08-05 2025-01-21 The Procter & Gamble Company Fibrous structures
US10132042B2 (en) 2015-03-10 2018-11-20 The Procter & Gamble Company Fibrous structures
USD985948S1 (en) * 2018-10-04 2023-05-16 The Procter & Gamble Company Sheet with pattern
US11408129B2 (en) 2018-12-10 2022-08-09 The Procter & Gamble Company Fibrous structures
US11732420B2 (en) 2018-12-10 2023-08-22 The Procter & Gamble Company Fibrous structures
US12071729B2 (en) 2018-12-10 2024-08-27 The Procter & Gamble Company Fibrous structures

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