US1604151A - Light-weight girder - Google Patents
Light-weight girder Download PDFInfo
- Publication number
- US1604151A US1604151A US392563A US39256320A US1604151A US 1604151 A US1604151 A US 1604151A US 392563 A US392563 A US 392563A US 39256320 A US39256320 A US 39256320A US 1604151 A US1604151 A US 1604151A
- Authority
- US
- United States
- Prior art keywords
- girder
- light
- flange plates
- plates
- sheet 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 - Lifetime
Links
- 239000002184 metal Substances 0.000 description 8
- 230000004048 modification Effects 0.000 description 4
- 238000012986 modification Methods 0.000 description 4
- 238000010276 construction Methods 0.000 description 2
- 210000002105 tongue Anatomy 0.000 description 2
- 241001315609 Pittosporum crassifolium Species 0.000 description 1
- 244000268528 Platanus occidentalis Species 0.000 description 1
- 229910000831 Steel Inorganic materials 0.000 description 1
- 238000004026 adhesive bonding Methods 0.000 description 1
- 238000005452 bending Methods 0.000 description 1
- 229920002678 cellulose Polymers 0.000 description 1
- 239000001913 cellulose Substances 0.000 description 1
- 239000002131 composite material Substances 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
- 238000003466 welding Methods 0.000 description 1
- 239000002023 wood Substances 0.000 description 1
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
- B64C1/065—Spars
-
- 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
Definitions
- My invention refers to girders which combine small weight with reat strength and can be manufactured witfi ease, so that they are suitable for wholesale manufacture more especially for the purpose of air craft construction.
- a middle web of sheet metal bent in zigzaa fashion has its longitudinal edges rigidly fixed to flange plates extending vertically in regard to the surface of the middle web.
- the width of the flange plates does not materially exceed the depth of the corrugations formed in the middle web which is thus easily accessible from both sides and in this way distinguishes favorably from girders whose webs consist of a row of adjoining cells. Besides, it braces the flange plates in a most effective manner and the danger of buckling and'bending is thus effectually avoided.
- Fig. 1 is a perspective view of aplate girder with plane flange plates and Fig. 2 is a similar view of a girder with corrugated flange plates, the parts being shown unassembled.
- the middle web is formed by a thin corrugated sheet metal strip at having its lateral edges provided with tongues b deflected at right angles to said strip a.
- plane flange plates 0 being fixed to the tongues b by riveting or welding.
- gle strips e, e are riveted or otherwise secured to both sides of the middle web (1 so as to laterally project above and below it, respectively, an the flange plates f are secured .by riveting or otherwise to the outer surfaces of the angle strips e.
- the girder is reinforced by means of strong plates h extending between and fixedto the angle stri s on each side of the middle web.
- girders which at least artially consist of wood, cellulose or other artificial products. According to the constructional material employed, the various parts of the girder can also be united with each other by gluing or bolting or in similar manner.
- I claim 1 In a composite sheet metal girder in combination, two sheet metal plates disposed parallel, a separate sheet metal web bent zi zag fashion arranged intermediate said plates and angle strips fixed to said web and to said plates, respectively.
Landscapes
- Engineering & Computer Science (AREA)
- Architecture (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Civil Engineering (AREA)
- Structural Engineering (AREA)
- Rod-Shaped Construction Members (AREA)
- Joining Of Building Structures In Genera (AREA)
Description
Patented Oct. 26,1926.
UNITED STATES PATENT OFFICE.
CLAUDE DORNIER, OI FRIEDBIOESHAIEN, GERMANY, ASBIGNOR TO THE FIRE: LUI'TSCHIFFBAU ZEPPELIN GESELLBCHAFT MIT BESCKBANKTEB HAI'TUNG, OI
FRIEDBICHSHAFEN, GERMANY.
LIGHT-WEIGHT GIRDEB.
Application illed June 88, 1820, Serial No. 392,583, and in Germany In 4, 1917.
(GRANTED UNDER- m PROVISIONS 01' THE ACT OF KARO! 3, 1921, 41 STATE. L, 1818.)
My invention refers to girders which combine small weight with reat strength and can be manufactured witfi ease, so that they are suitable for wholesale manufacture more especially for the purpose of air craft construction.
In the novel girder, which is preferably made of light metal, a middle web of sheet metal bent in zigzaa fashion has its longitudinal edges rigidly fixed to flange plates extending vertically in regard to the surface of the middle web. The width of the flange plates does not materially exceed the depth of the corrugations formed in the middle web which is thus easily accessible from both sides and in this way distinguishes favorably from girders whose webs consist of a row of adjoining cells. Besides, it braces the flange plates in a most effective manner and the danger of buckling and'bending is thus effectually avoided. I
The drawings attached to this specification and forming part thereof illustrate two modifications of a girder embodying my invention by way of example.
Fig. 1 is a perspective view of aplate girder with plane flange plates and Fig. 2 is a similar view of a girder with corrugated flange plates, the parts being shown unassembled. In the modification'shown in Fig. 1 the middle web is formed by a thin corrugated sheet metal strip at having its lateral edges provided with tongues b deflected at right angles to said strip a. plane flange plates 0 being fixed to the tongues b by riveting or welding. 1
In the modification illustrated in Flg. 2
(I is the zigzag-shaped sheet metal strip forming the middle web. f, 'f are the top and bottom flange plates each of which is braced by two longitudinal grooves g. An-
gle strips e, e are riveted or otherwise secured to both sides of the middle web (1 so as to laterally project above and below it, respectively, an the flange plates f are secured .by riveting or otherwise to the outer surfaces of the angle strips e. At the ends the girder is reinforced by means of strong plates h extending between and fixedto the angle stri s on each side of the middle web.
Prefera 1y, thin steel plate or light metal sheetis employed. but it is also possible to produce girders which at least artially consist of wood, cellulose or other artificial products. According to the constructional material employed, the various parts of the girder can also be united with each other by gluing or bolting or in similar manner.
I wish it to be understood that I do not desire to be limited to the exactdetails of construction shown and described, for obvious. modifications will occur to a person skilled in the art.
I claim 1. In a composite sheet metal girder in combination, two sheet metal plates disposed parallel, a separate sheet metal web bent zi zag fashion arranged intermediate said plates and angle strips fixed to said web and to said plates, respectively.
In testimony whereof I. afiix signature.
CLAUDE DORNIER.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE1604151X | 1917-05-04 |
Publications (1)
Publication Number | Publication Date |
---|---|
US1604151A true US1604151A (en) | 1926-10-26 |
Family
ID=7736962
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US392563A Expired - Lifetime US1604151A (en) | 1917-05-04 | 1920-06-23 | Light-weight girder |
Country Status (1)
Country | Link |
---|---|
US (1) | US1604151A (en) |
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2997262A (en) * | 1960-01-21 | 1961-08-22 | Gen Dynamics Corp | Aircraft wing structure |
US3495816A (en) * | 1967-06-22 | 1970-02-17 | John Stuart Lyle | Variable rate spring reinforced structural member |
EP0009975A1 (en) * | 1978-10-04 | 1980-04-16 | Ford Motor Company Limited | Load support structural members and motor vehicle frames including such members |
US4769968A (en) * | 1987-03-05 | 1988-09-13 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Truss-core corrugation for compressive loads |
US6851246B2 (en) * | 2000-01-17 | 2005-02-08 | Faurecia Industries | Structural member comprising a body and reinforcing ribs and corresponding motor vehicle |
US20080006000A1 (en) * | 2006-07-05 | 2008-01-10 | Sukup Manufacturing Company | Support for a grain bin floor and method of making the same |
-
1920
- 1920-06-23 US US392563A patent/US1604151A/en not_active Expired - Lifetime
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2997262A (en) * | 1960-01-21 | 1961-08-22 | Gen Dynamics Corp | Aircraft wing structure |
US3495816A (en) * | 1967-06-22 | 1970-02-17 | John Stuart Lyle | Variable rate spring reinforced structural member |
EP0009975A1 (en) * | 1978-10-04 | 1980-04-16 | Ford Motor Company Limited | Load support structural members and motor vehicle frames including such members |
US4386792A (en) * | 1978-10-04 | 1983-06-07 | Ford Motor Company | Fabricated load support structural member |
US4769968A (en) * | 1987-03-05 | 1988-09-13 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Truss-core corrugation for compressive loads |
US6851246B2 (en) * | 2000-01-17 | 2005-02-08 | Faurecia Industries | Structural member comprising a body and reinforcing ribs and corresponding motor vehicle |
US20080006000A1 (en) * | 2006-07-05 | 2008-01-10 | Sukup Manufacturing Company | Support for a grain bin floor and method of making the same |
US7845129B2 (en) * | 2006-07-05 | 2010-12-07 | Sukup Manufacturing Company | Support for a grain bin floor |
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