US1571240A - Metal girder - Google Patents

Metal girder Download PDF

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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
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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
Application number
US50874A
Inventor
Dornier Claudius
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
FIRM DORNIER METALLBAUTEN GmbH
Original Assignee
FIRM DORNIER METALLBAUTEN GmbH
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Priority claimed from US619696A external-priority patent/US1571239A/en
Application filed by FIRM DORNIER METALLBAUTEN GmbH filed Critical FIRM DORNIER METALLBAUTEN GmbH
Priority to US50874A priority Critical patent/US1571240A/en
Application granted granted Critical
Publication of US1571240A publication Critical patent/US1571240A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C1/00Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/06Frames; Stringers; Longerons ; Fuselage sections
    • B64C1/065Spars
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C1/00Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C2001/0054Fuselage structures substantially made from particular materials
    • B64C2001/0081Fuselage 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.

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  • 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.
US50874A 1923-02-17 1925-08-17 Metal girder Expired - Lifetime US1571240A (en)

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

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Publication Number Publication Date
US1571240A true US1571240A (en) 1926-02-02

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US50874A Expired - Lifetime US1571240A (en) 1923-02-17 1925-08-17 Metal girder

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2446410A (en) * 1943-11-27 1948-08-03 Kibbey W Couse Combination pry-and-boom structure

Cited By (1)

* Cited by examiner, † Cited by third party
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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