USRE21921E - Welded structural member - Google Patents
Welded structural member Download PDFInfo
- 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
- Authority
- 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
Links
- 239000002184 metal Substances 0.000 description 15
- 238000003466 welding Methods 0.000 description 6
- 238000004519 manufacturing process Methods 0.000 description 5
- 238000010276 construction Methods 0.000 description 1
- 239000000463 material Substances 0.000 description 1
Images
Classifications
-
- E—FIXED CONSTRUCTIONS
- E04—BUILDING
- E04C—STRUCTURAL ELEMENTS; BUILDING MATERIALS
- E04C3/00—Structural elongated elements designed for load-supporting
- E04C3/02—Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces
- E04C3/04—Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces of metal
- E04C3/06—Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces of metal with substantially solid, i.e. unapertured, web
- E04C3/07—Joists; 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
-
- E—FIXED CONSTRUCTIONS
- E04—BUILDING
- E04C—STRUCTURAL ELEMENTS; BUILDING MATERIALS
- E04C3/00—Structural elongated elements designed for load-supporting
- E04C3/02—Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces
- E04C3/04—Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces of metal
- E04C2003/0404—Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces of metal beams, girders, or joists characterised by cross-sectional aspects
- E04C2003/0408—Joists; 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
- E04C2003/0413—Joists; 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
-
- E—FIXED CONSTRUCTIONS
- E04—BUILDING
- E04C—STRUCTURAL ELEMENTS; BUILDING MATERIALS
- E04C3/00—Structural elongated elements designed for load-supporting
- E04C3/02—Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces
- E04C3/04—Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces of metal
- E04C2003/0404—Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces of metal beams, girders, or joists characterised by cross-sectional aspects
- E04C2003/0426—Joists; 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
- E04C2003/0434—Joists; 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
-
- E—FIXED CONSTRUCTIONS
- E04—BUILDING
- E04C—STRUCTURAL ELEMENTS; BUILDING MATERIALS
- E04C3/00—Structural elongated elements designed for load-supporting
- E04C3/02—Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces
- E04C3/04—Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces of metal
- E04C2003/0404—Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces of metal beams, girders, or joists characterised by cross-sectional aspects
- E04C2003/0443—Joists; 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
- E04C2003/0452—H- or I-shaped
-
- Y—GENERAL 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49616—Structural member making
- Y10T29/49623—Static structure, e.g., a building component
- Y10T29/49634—Beam 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.
Landscapes
- 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.
Publications (1)
| Publication Number | Publication Date |
|---|---|
| USRE21921E true USRE21921E (en) | 1941-10-14 |
Family
ID=2088056
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US21921D Expired USRE21921E (en) | Welded structural member |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | USRE21921E (en) |
Cited By (23)
| 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 |
-
0
- US US21921D patent/USRE21921E/en not_active Expired
Cited By (42)
| 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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