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USRE21921E - Welded structural member - Google Patents

Welded structural member Download PDF

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Publication number
USRE21921E
USRE21921E US21921DE USRE21921E US RE21921 E USRE21921 E US RE21921E US 21921D E US21921D E US 21921DE US RE21921 E USRE21921 E US RE21921E
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US
United States
Prior art keywords
web
flange
portions
groove
metal
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
Application number
Publication date
Application granted granted Critical
Publication of USRE21921E publication Critical patent/USRE21921E/en
Expired legal-status Critical Current

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Classifications

    • EFIXED CONSTRUCTIONS
    • E04BUILDING
    • E04CSTRUCTURAL ELEMENTS; BUILDING MATERIALS
    • E04C3/00Structural elongated elements designed for load-supporting
    • E04C3/02Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces
    • E04C3/04Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces of metal
    • E04C3/06Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces of metal with substantially solid, i.e. unapertured, web
    • E04C3/07Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces of metal with substantially solid, i.e. unapertured, web at least partly of bent or otherwise deformed strip- or sheet-like material
    • EFIXED CONSTRUCTIONS
    • E04BUILDING
    • E04CSTRUCTURAL ELEMENTS; BUILDING MATERIALS
    • E04C3/00Structural elongated elements designed for load-supporting
    • E04C3/02Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces
    • E04C3/04Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces of metal
    • E04C2003/0404Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces of metal beams, girders, or joists characterised by cross-sectional aspects
    • E04C2003/0408Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces of metal beams, girders, or joists characterised by cross-sectional aspects characterised by assembly or the cross-section
    • E04C2003/0413Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces of metal beams, girders, or joists characterised by cross-sectional aspects characterised by assembly or the cross-section being built up from several parts
    • EFIXED CONSTRUCTIONS
    • E04BUILDING
    • E04CSTRUCTURAL ELEMENTS; BUILDING MATERIALS
    • E04C3/00Structural elongated elements designed for load-supporting
    • E04C3/02Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces
    • E04C3/04Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces of metal
    • E04C2003/0404Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces of metal beams, girders, or joists characterised by cross-sectional aspects
    • E04C2003/0426Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces of metal beams, girders, or joists characterised by cross-sectional aspects characterised by material distribution in cross section
    • E04C2003/0434Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces of metal beams, girders, or joists characterised by cross-sectional aspects characterised by material distribution in cross section the open cross-section free of enclosed cavities
    • EFIXED CONSTRUCTIONS
    • E04BUILDING
    • E04CSTRUCTURAL ELEMENTS; BUILDING MATERIALS
    • E04C3/00Structural elongated elements designed for load-supporting
    • E04C3/02Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces
    • E04C3/04Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces of metal
    • E04C2003/0404Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces of metal beams, girders, or joists characterised by cross-sectional aspects
    • E04C2003/0443Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces of metal beams, girders, or joists characterised by cross-sectional aspects characterised by substantial shape of the cross-section
    • E04C2003/0452H- or I-shaped
    • 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
    • Y10T29/49634Beam or girder

Definitions

  • This invention relates to the production of welded structures by means of a suitable web and a flange welded thereto.
  • Figure 1' is a perspective view of the assembled structure
  • Figure 2 is a detailed transverse sectional view showing the flange and web before welding
  • Figure 3 is a detailed sectional view showing the flange and web after welding:
  • the thickness of the folded flange may be equal to or greater than the thickness of the web.
  • the ratio of thickness between the single thickness of metal in the flange and the web is an example of the ratio of thickness between the single thickness of metal in the flange and the web.
  • Figure 4 is a detailed section of the web edge.
  • the numeral 2 designates the web, which is of single thickness of metal.
  • web may be a plain straight sheet of metal or,
  • the inner body portion 6 is preferably spaced from the outer .body portion 5, as shown in Figures 2 and 3, and
  • the extreme outer ends of the piece are bent outwardly to'a position substantially perpendicular to the outer body portions 5 and centrally thereof so as to provide outwardly extending portions or wings 1.
  • the outwardly extending portions or wings I are substantially parallel to each other and spaced apart preferably a distance slightly more than the thickness of the edge portions of the web 2 so as to provide a longitudinally extending slot or groove therebetween extending throughout the length of the flange.
  • the web 2 is then positioned in the longitudinally extending slot or groove between the outwardly extending portions I of the flange in cone tact with the inner faces of the same with the edge of the web preferably abutting firmly against the inner face 8 of the intermediate or outer body portion 5.
  • the web and both the outwardly extending portions I are suitably secured together preferably by being spot welded at the projections 3 and I, or if the edge portions of the web are flat and straight,
  • edge portions of the web and the outwardly extending portions 1 are spot welded at various points along the entire length thereof.
  • the thickness of the metal in the flange be less than the thickness of the metal in the web 2
  • the total thickness range between '70 and 95 per cent. of the thickness of the web metal or the combined total thickness of the doubled-up flange should range from 140 to 190. per cent. of the total web thickness.
  • the web 2 contact the inner face of the outer portion of the flange and, in so doing, reduce the amount of'welding required and at the same time produce a beam structure having suitable advantages over the beams of the present construction.
  • a structural member comprising at least one I flange formed from a single piece of metal bent backupon itself toprovide a double thickness of metal in spaced relationship and including laterally extended portions from the inner portion of said flange and a web provided with a plurality of projections extending alternately from each side thereof positioned between said laterally extended portions and welded thereto at the points said projections contact saidlaterallyv extended flange portions, said web adapted to project beyond the inner portion of said flangeto contact the inner face of the outer portion 2;
  • The-method of making a metal beam which includes making amet beam web in the form of an elongatedstrip of metal having opposite edgeportions, making a unitary metal beam flange comprising laterally opposite integrally connected longitudinally extending flange portions, with a longitudinally extending wing on prising laterally opposite integrally connected flange portions and an inwardly open groove extending longitudinally therealong, seatingl an edge portion of the web in the groove and welding the edge portion of the web to the side walls of
  • the method of making a beam which includes forming an elongated sheet metal web having a longitudinally extending substantially flat edge portion, forming a unitary elongated sheet metal flange having longitudinally extending wings thereon, with the wings spaced apart to proyide a longitudinally extending groove between the wings having substantially parallel side walls, inserting the edge portion of the web into the groove with opposite faces of the edge portion of the web substantially engaging the side walls of the groove and welding the faces of the web edge portion to the side walls of the groove.
  • the method of making a beam which includes forming an elongated sheet metal web having a longitudinally extending edge portion, forming an elongated unitary sheet metal flange comprising integrally connected, laterally opposite, longitudinally extending flange portions and longitudinally extending wings integrally connected with the flange, and with the wings spaced apart .to provide a longitudinally extending groove between the wings and the grooves having confronting side walls, inserting the edge portion of the web into the groove with opposite faces of the edge portion of the web substantially engaging the side walls of the groove, and welding. the faces of the web edge portion to the side walls of the groove.

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  • Engineering & Computer Science (AREA)
  • Architecture (AREA)
  • Civil Engineering (AREA)
  • Structural Engineering (AREA)
  • Rod-Shaped Construction Members (AREA)

Description

Oct. 14, 1941. G GREUI ICH Re. 21,921 WELDED STRUCTURAL MEMBER Original Fil'ed Deb.
6 N N I 7 EU DOA ma B r//// U ///////////A////////////////// W m V A a w. mw E 6 Reissued Oct. 14, 1941 UNITED STATE WELDED STRUCTURAL MEMBER.
Gerald G. Greulich, Mount Lebanon, Pa.
Original No. 2,108,373. dated February 15, 1938,
Serial No. 118,663, December 31, 1936. Application for reissue Dece Claims. (Cl. 189-37) This invention relates to the production of welded structures by means of a suitable web and a flange welded thereto.
Other objects and advantages will become apparent as the description proceeds, in which:
Figure 1' is a perspective view of the assembled structure;
Figure 2 is a detailed transverse sectional view showing the flange and web before welding;
Figure 3 is a detailed sectional view showing the flange and web after welding: and
mber 20, 1939, Serial No.
of the folded flange may be equal to or greater than the thickness of the web. As an example of the ratio of thickness between the single thickness of metal in the flange and the web,
I propose that this single thickness of the material from which the flange is formed should Figure 4 is a detailed section of the web edge.
In the drawing, the numeral 2 designates the web, which is of single thickness of metal. The
web may be a plain straight sheet of metal or,
back over the intermediate portion oi the piece;
so as to provide an intermediate or outer body portion 5 and an inner body portion 8. The inner body portion 6 is preferably spaced from the outer .body portion 5, as shown in Figures 2 and 3, and
the extreme outer ends of the piece are bent outwardly to'a position substantially perpendicular to the outer body portions 5 and centrally thereof so as to provide outwardly extending portions or wings 1. The outwardly extending portions or wings I are substantially parallel to each other and spaced apart preferably a distance slightly more than the thickness of the edge portions of the web 2 so as to provide a longitudinally extending slot or groove therebetween extending throughout the length of the flange.
The web 2 is then positioned in the longitudinally extending slot or groove between the outwardly extending portions I of the flange in cone tact with the inner faces of the same with the edge of the web preferably abutting firmly against the inner face 8 of the intermediate or outer body portion 5. When in such position, the web and both the outwardly extending portions I are suitably secured together preferably by being spot welded at the projections 3 and I, or if the edge portions of the web are flat and straight,
the edge portions of the web and the outwardly extending portions 1 are spot welded at various points along the entire length thereof.
While I prefer that the thickness of the metal in the flange be less than the thickness of the metal in the web 2, if desired, the total thickness range between '70 and 95 per cent. of the thickness of the web metal or the combined total thickness of the doubled-up flange should range from 140 to 190. per cent. of the total web thickness. By such a differential in the web and flange thicknesses, it is possible to obtain unlimited combination of web and flange sizes which permits production of any depth, width and height of beam desired.
Also, it is desired that the web 2 contact the inner face of the outer portion of the flange and, in so doing, reduce the amount of'welding required and at the same time produce a beam structure having suitable advantages over the beams of the present construction.
The principle involved herein may be applied with web members and flange members of other I thereof.
without departing from the scope of the invention, as defined in the following claims.
I claim:
1. A structural member comprising at least one I flange formed from a single piece of metal bent backupon itself toprovide a double thickness of metal in spaced relationship and including laterally extended portions from the inner portion of said flange and a web provided with a plurality of projections extending alternately from each side thereof positioned between said laterally extended portions and welded thereto at the points said projections contact saidlaterallyv extended flange portions, said web adapted to project beyond the inner portion of said flangeto contact the inner face of the outer portion 2; The-method of making a metal beam which includes making amet beam web in the form of an elongatedstrip of metal having opposite edgeportions, making a unitary metal beam flange comprising laterally opposite integrally connected longitudinally extending flange portions, with a longitudinally extending wing on prising laterally opposite integrally connected flange portions and an inwardly open groove extending longitudinally therealong, seatingl an edge portion of the web in the groove and welding the edge portion of the web to the side walls of the groove.
4. The method of making a beam which includes forming an elongated sheet metal web having a longitudinally extending substantially flat edge portion, forming a unitary elongated sheet metal flange having longitudinally extending wings thereon, with the wings spaced apart to proyide a longitudinally extending groove between the wings having substantially parallel side walls, inserting the edge portion of the web into the groove with opposite faces of the edge portion of the web substantially engaging the side walls of the groove and welding the faces of the web edge portion to the side walls of the groove.
5. The method of making a beam which includes forming an elongated sheet metal web having a longitudinally extending edge portion, forming an elongated unitary sheet metal flange comprising integrally connected, laterally opposite, longitudinally extending flange portions and longitudinally extending wings integrally connected with the flange, and with the wings spaced apart .to provide a longitudinally extending groove between the wings and the grooves having confronting side walls, inserting the edge portion of the web into the groove with opposite faces of the edge portion of the web substantially engaging the side walls of the groove, and welding. the faces of the web edge portion to the side walls of the groove.
GERALD G. GREULICH.
US21921D Welded structural member Expired USRE21921E (en)

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Cited By (23)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2877878A (en) * 1953-06-25 1959-03-17 Nat Gypsum Co Suspension ceiling
US3033783A (en) * 1958-04-07 1962-05-08 Permanent Filter Corp Filter and method of producing same
US4060706A (en) 1975-01-10 1977-11-29 Moeller Manufacturing Company, Inc. Method of forming a handle by welding
US5501053A (en) * 1990-09-28 1996-03-26 Tube Technology Pty., Ltd. Interengageable structural members
US6360510B1 (en) * 1998-12-22 2002-03-26 Porta-Fab Corporation Hat-channel stud for modular building system
US6374570B1 (en) * 2000-08-25 2002-04-23 Lockheed Martin Corporation Apparatus and method for joining dissimilar materials to form a structural support member
US20050133666A1 (en) * 2003-12-19 2005-06-23 Ingo Zerner Seat mounting rail, particularly for a commercial aircraft
US20050156095A1 (en) * 2003-12-19 2005-07-21 Alexei Vichniakov Seat mounting rail, particularly for a commercial aircraft
US20060113450A1 (en) * 2004-11-30 2006-06-01 The Boeing Company Self-locating feature for a pi-joint assembly
US20060113451A1 (en) * 2004-11-30 2006-06-01 The Boeing Company Minimum bond thickness assembly feature assurance
US20060115320A1 (en) * 2004-11-30 2006-06-01 The Boeing Company Determinant assembly features for vehicle structures
US20060150571A1 (en) * 2005-01-11 2006-07-13 Zahner L W Iii I-beam with curved flanges
US20060277859A1 (en) * 2003-09-01 2006-12-14 Forster Rohr Und Profiltechnik Ag Profile and method for producing a profile
US20080105661A1 (en) * 2006-11-02 2008-05-08 The Boeing Company Method and apparatus to construct metal securement member for an aircraft
US20080128550A1 (en) * 2006-10-31 2008-06-05 Airbus Deutschland Gmbh Stiffening element for an aircraft or spacecraft, and method for its production
US20080250747A1 (en) * 2007-04-12 2008-10-16 Johnson Fred E T-chord open web joist with adjustable ends
US20100162567A1 (en) * 2006-11-02 2010-07-01 The Boeing Company Mounting device for an aircraft
US20120079782A1 (en) * 2010-09-30 2012-04-05 Choong-Ki Kim Support beam structure capable of extending span and reducing height of ceiling structure and installing method thereof
US20120216475A1 (en) * 2011-02-27 2012-08-30 Kamal Safari Kermanshahi Cold Formed Roof and Columns Building Structure System
US20120328898A1 (en) * 2009-07-22 2012-12-27 Best Joist Inc. Roll formed steel beam
US8382070B1 (en) 2011-07-07 2013-02-26 Edward L. Gibbs Barrier system
US10443239B2 (en) * 2016-12-02 2019-10-15 Columbia Insurance Company Long span masonry lintel support system
US10480197B2 (en) 2017-04-04 2019-11-19 Columbia Insurance Company Masonry support

Cited By (42)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2877878A (en) * 1953-06-25 1959-03-17 Nat Gypsum Co Suspension ceiling
US3033783A (en) * 1958-04-07 1962-05-08 Permanent Filter Corp Filter and method of producing same
US4060706A (en) 1975-01-10 1977-11-29 Moeller Manufacturing Company, Inc. Method of forming a handle by welding
US5501053A (en) * 1990-09-28 1996-03-26 Tube Technology Pty., Ltd. Interengageable structural members
US6360510B1 (en) * 1998-12-22 2002-03-26 Porta-Fab Corporation Hat-channel stud for modular building system
US6374570B1 (en) * 2000-08-25 2002-04-23 Lockheed Martin Corporation Apparatus and method for joining dissimilar materials to form a structural support member
US6718713B2 (en) * 2000-08-25 2004-04-13 Lockheed Martin Corporation Apparatus and method for joining dissimilar materials to form a structural support member
US20060277859A1 (en) * 2003-09-01 2006-12-14 Forster Rohr Und Profiltechnik Ag Profile and method for producing a profile
US7100885B2 (en) * 2003-12-19 2006-09-05 Airbus Deutschland Gmbh Seat mounting rail, particularly for a commercial aircraft
US20050133666A1 (en) * 2003-12-19 2005-06-23 Ingo Zerner Seat mounting rail, particularly for a commercial aircraft
US20050156095A1 (en) * 2003-12-19 2005-07-21 Alexei Vichniakov Seat mounting rail, particularly for a commercial aircraft
US7207756B2 (en) * 2003-12-19 2007-04-24 Airbus Deutschland Gmbh Seat mounting rail, particularly for a commercial aircraft
US8272618B2 (en) 2004-11-30 2012-09-25 The Boeing Company Minimum bond thickness assembly feature assurance
US8403586B2 (en) 2004-11-30 2013-03-26 The Boeing Company Determinant assembly features for vehicle structures
US20060115320A1 (en) * 2004-11-30 2006-06-01 The Boeing Company Determinant assembly features for vehicle structures
US20060113451A1 (en) * 2004-11-30 2006-06-01 The Boeing Company Minimum bond thickness assembly feature assurance
US20060113450A1 (en) * 2004-11-30 2006-06-01 The Boeing Company Self-locating feature for a pi-joint assembly
US20110123254A1 (en) * 2004-11-30 2011-05-26 The Boeing Company Determinant Assembly Features for Vehicle Structures
US7914223B2 (en) 2004-11-30 2011-03-29 The Boeing Company Determinant assembly features for vehicle structures
US7555873B2 (en) * 2004-11-30 2009-07-07 The Boeing Company Self-locating feature for a pi-joint assembly
US20090123225A1 (en) * 2004-11-30 2009-05-14 Wood Jeffrey H Determinant assembly features for vehicle structures
US20080196356A1 (en) * 2005-01-11 2008-08-21 A. Zahner Company I-beam with curved flanges
US7434366B2 (en) * 2005-01-11 2008-10-14 A. Zahner Company I-beam with curved flanges
US20060150571A1 (en) * 2005-01-11 2006-07-13 Zahner L W Iii I-beam with curved flanges
US7784243B2 (en) * 2005-01-11 2010-08-31 A. Zahner Company I-beam with curved flanges
US8910908B2 (en) * 2006-10-31 2014-12-16 Airbus Operations Gmbh Two-piece stiffening element
US20080128550A1 (en) * 2006-10-31 2008-06-05 Airbus Deutschland Gmbh Stiffening element for an aircraft or spacecraft, and method for its production
US20100162567A1 (en) * 2006-11-02 2010-07-01 The Boeing Company Mounting device for an aircraft
US7810757B2 (en) * 2006-11-02 2010-10-12 The Boeing Company Mounting device for an aircraft
US9394062B2 (en) 2006-11-02 2016-07-19 The Boeing Company Method and apparatus to construct metal securement member for an aircraft
US20080105661A1 (en) * 2006-11-02 2008-05-08 The Boeing Company Method and apparatus to construct metal securement member for an aircraft
US9016551B2 (en) * 2006-11-02 2015-04-28 The Boeing Company Method and apparatus to construct metal securement member for an aircraft
US20080250747A1 (en) * 2007-04-12 2008-10-16 Johnson Fred E T-chord open web joist with adjustable ends
US20120328898A1 (en) * 2009-07-22 2012-12-27 Best Joist Inc. Roll formed steel beam
US9975577B2 (en) * 2009-07-22 2018-05-22 Ispan Systems Lp Roll formed steel beam
US20120079782A1 (en) * 2010-09-30 2012-04-05 Choong-Ki Kim Support beam structure capable of extending span and reducing height of ceiling structure and installing method thereof
US8813445B2 (en) * 2010-09-30 2014-08-26 Choong-Ki Kim Support beam structure capable of extending span and reducing height of ceiling structure and installing method thereof
US8316621B2 (en) * 2011-02-27 2012-11-27 Kamal Safari Kermanshahi Cold formed roof and columns building structure system
US20120216475A1 (en) * 2011-02-27 2012-08-30 Kamal Safari Kermanshahi Cold Formed Roof and Columns Building Structure System
US8382070B1 (en) 2011-07-07 2013-02-26 Edward L. Gibbs Barrier system
US10443239B2 (en) * 2016-12-02 2019-10-15 Columbia Insurance Company Long span masonry lintel support system
US10480197B2 (en) 2017-04-04 2019-11-19 Columbia Insurance Company Masonry support

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