US1571240A - Metal girder - Google Patents
Metal girder Download PDFInfo
- Publication number
- US1571240A US1571240A US50874A US5087425A US1571240A US 1571240 A US1571240 A US 1571240A US 50874 A US50874 A US 50874A US 5087425 A US5087425 A US 5087425A US 1571240 A US1571240 A US 1571240A
- Authority
- US
- United States
- Prior art keywords
- girder
- metal
- side walls
- metal girder
- flanges
- 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 title description 14
- 238000010276 construction Methods 0.000 description 4
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 238000003466 welding Methods 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
-
- 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
- B64C2001/0054—Fuselage structures substantially made from particular materials
- B64C2001/0081—Fuselage structures substantially made from particular materials from metallic materials
Definitions
- My invention relates to metal girders and more especially toa metal girder intended for air craft construction, where structural elements of high strength and low weight. are required.
- a box-shaped girder with oppositely located apertures having in wardly directed flanges which are connected with each other by means of tubular connecting pieces fixed to the flanges by riveting, welding or the like either at their inner 'or outer surface or at one end with the inner and at the other end with the outer surface a of the flange.
- the planes of their longitudinal edges may be efl'ected in any desired manner, for in stance by means of-a panel.
- the girder consists of two side walls 1 and 2 provided with circular apertures 20 and 30, havin in wardly directed flanges 3 and 4 which are connected with each other by a short tubular piece 12 flanged at its ends, one flange 13 abutting against flange 4 of one aperture 1 from the inside, while the other flange 14 abuts against the flange 3 from the outside.
- the tubular piece 12 is fixed to the side walls by a circular row of rivets 1'5.
- the marginal portions-of the side walls 1 and 2 are bent outwards at right angles. as shown at 16, and the parts 17 near the free edges of these portions are bent at an obtuse angle.
- To theparts 16 are riveted metal strips 10 and 11, the lower metal strip having two longitudinal grooves formed therein while the top metal strip 11 has the form of an ordinary channel.
- the girder described combines low weight with extraordinary strength and rigidity and canfbe manufactured at comparatively very low costs.
- a low weight sheet-metal girder for g 1 air craft'constru'ction comprising two juxta- The connection ofthe two sidewalls .m'
- a low weightsheet-metal girder for air craft construction comprisingtwo juxtaposed apertured side walls, inwardly directed flanges adjoining the apertures of said walls and a flanged tubular connecting piece rigidly fixed between the flanges of oppositely disposed apertures.
- a low weight sheet-metal girder'for air craft construction comprising, two juxtaposed apertured side walls, inwardly direct ed flanges adjoining the apertures of. said walls, a flanged tubular connecting piece rigidly fixed between the flanges of oppositely disposed a ertures and grooved sheet metal strips fixe to and connecting adjoining longitudinal edges of said side walls.
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Rod-Shaped Construction Members (AREA)
Description
Feb. 2 1926. 1,571,240
C. DORNIER METAL GIRDER Original Filed Feb. 17, 1923 ezwenl ar:
Patented Feb. 2, 1926.
UNITED STA ES PATENT orncs.
GLAUDIUS OI FBIEDBI C JHSHAFEN-oN TflE-BoDENsiEE, GERMANY, I AS- SIGNOR OF ONE-HALF '10 FIRM DOBNIER METALLBAUTEN GESELLSCHAFT MI'I. BESGHRKNKTER HAFTUNG, OF FRIEDRICHSHAFEN-QN-THE-BODENSEE, GERMANY.
METAL GIRDER.
Original aliplication 'flled February 17, 1923, Serial No. 619,896. Divided and this application filed August To all wlwmz'tma z concern: I
Be it known that I, 'CLAUnIUs DoRNInn', a citizen of Germany, residing at Friedrichshafen-on-theBodensee, Germany, have invented certain new and useful Improvements in Metal Girders, of which the following is a specification.
My invention relates to metal girders and more especially toa metal girder intended for air craft construction, where structural elements of high strength and low weight. are required.
To this end I provide a box-shaped girder with oppositely located apertures having in wardly directed flangeswhich are connected with each other by means of tubular connecting pieces fixed to the flanges by riveting, welding or the like either at their inner 'or outer surface or at one end with the inner and at the other end with the outer surface a of the flange.
the planes of their longitudinal edges may be efl'ected in any desired manner, for in stance by means of-a panel. I prefer beInd-1 ing the marginal portionsof the side walls so as to form outwardly directed flanges and to connect these latter with each other by a sheet-metal strip which may be grooved or channelled.
In the drawings ailixed to this specificstion and forming part thereof, a girder embodying my invention illustrated in crosssection by way of exa ple.
Referring to the drawing, the girder consists of two side walls 1 and 2 provided with circular apertures 20 and 30, havin in wardly directed flanges 3 and 4 which are connected with each other by a short tubular piece 12 flanged at its ends, one flange 13 abutting against flange 4 of one aperture 1 from the inside, while the other flange 14 abuts against the flange 3 from the outside. The tubular piece 12 is fixed to the side walls by a circular row of rivets 1'5.
'17, 1825: Serial No. 50,874.
The marginal portions-of the side walls 1 and 2 are bent outwards at right angles. as shown at 16, and the parts 17 near the free edges of these portions are bent at an obtuse angle. To theparts 16 are riveted metal strips 10 and 11, the lower metal strip having two longitudinal grooves formed therein while the top metal strip 11 has the form of an ordinary channel.
The girder described combines low weight with extraordinary strength and rigidity and canfbe manufactured at comparatively very low costs. I
I wish it tobe understood that I do not desire to be limited to the exact details of construction shown and described, for obvious modifications will occur to a person skilled. in the art.
I claim 1.' A low weight sheet-metal girder for g 1 air craft'constru'ction comprising two juxta- The connection ofthe two sidewalls .m'
posed apertures.
2. A low weightsheet-metal girder for air craft construction comprisingtwo juxtaposed apertured side walls, inwardly directed flanges adjoining the apertures of said walls and a flanged tubular connecting piece rigidly fixed between the flanges of oppositely disposed apertures.
3. A low weight sheet-metal girder'for air craft construction comprising, two juxtaposed apertured side walls, inwardly direct ed flanges adjoining the apertures of. said walls, a flanged tubular connecting piece rigidly fixed between the flanges of oppositely disposed a ertures and grooved sheet metal strips fixe to and connecting adjoining longitudinal edges of said side walls.
' In testimony whereof I aflix my signature.
QLAUDIUS- DORNIER.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US50874A US1571240A (en) | 1923-02-17 | 1925-08-17 | Metal girder |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US619696A US1571239A (en) | 1923-02-17 | 1923-02-17 | Metal girder for light metal structures |
US50874A US1571240A (en) | 1923-02-17 | 1925-08-17 | Metal girder |
Publications (1)
Publication Number | Publication Date |
---|---|
US1571240A true US1571240A (en) | 1926-02-02 |
Family
ID=26728786
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US50874A Expired - Lifetime US1571240A (en) | 1923-02-17 | 1925-08-17 | Metal girder |
Country Status (1)
Country | Link |
---|---|
US (1) | US1571240A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2446410A (en) * | 1943-11-27 | 1948-08-03 | Kibbey W Couse | Combination pry-and-boom structure |
-
1925
- 1925-08-17 US US50874A patent/US1571240A/en not_active Expired - Lifetime
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2446410A (en) * | 1943-11-27 | 1948-08-03 | Kibbey W Couse | Combination pry-and-boom structure |
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