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US1571239A - Metal girder for light metal structures - Google Patents

Metal girder for light metal structures Download PDF

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Publication number
US1571239A
US1571239A US619696A US61969623A US1571239A US 1571239 A US1571239 A US 1571239A US 619696 A US619696 A US 619696A US 61969623 A US61969623 A US 61969623A US 1571239 A US1571239 A US 1571239A
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US
United States
Prior art keywords
metal
flanges
girder
walls
structures
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
US619696A
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
Application filed by FIRM DORNIER METALLBAUTEN GmbH filed Critical FIRM DORNIER METALLBAUTEN GmbH
Priority to US619696A priority Critical patent/US1571239A/en
Priority to US50874A priority patent/US1571240A/en
Application granted granted Critical
Publication of US1571239A publication Critical patent/US1571239A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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Classifications

    • 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

  • connection of the two side walls in the planes of the girths may be effected in any desired manner, for instance, by means of a panel, but it is preferred to provide the side walls in the girth plane with outwardly directed flan es and to connect'these latter with each ot er by a sheet-metal strip.
  • the side walls in the girth plane with outwardly directed flan es and to connect'these latter with each ot er by a sheet-metal strip.
  • the longitudinal edge portions of the side-walls are preferably bent outwards a-t an obtuse angle.
  • the sheet-metal strips are preferably grooved or channelled.
  • the girder consists of -twoside walls 1 and 2 provided with circular apertures A'having inwardly directed. flanges 3 and 4 which are fastened to each other by rivets 5.V If weldable metal is used', the flanges may be connected with each other by spot ⁇ welding. The longitudinal edge portions ofthe walls 1 and 2 are bent outwards forming flanges 6 and the rims 7 of these flanges are again bent in such a manner, that the flange rims 7 disposed on the same side converge as vshown in Figure 1.' A
  • the lower boom consists of a plain strip boom 9 is y"I wish it to be understood that I do not idesire to lbe limited to the exact details of constructionfshown and described, for obvious modifications,"will occur to a person skilled in the/art'.
  • a lightsheet metal girder comprising two juxtaposed apertured side walls and inwardly 1 said flanges ing rigidy connected.
  • lightsheet metal irder com rising two uxtaposed aperture Ward y directed flanges surrounding the apertures of said wallsl, said flanges being rigidl connected Jand plate strips riveted to an connecting adjoining free edges of said side walls.
  • A'light sheet metal girder comprising two f'uxtaposed apertured side. walls, inward y directed flanges surrounding the apertures of said walls, said flan es being rigidly connected, ilanges extending substantially at right angles from the longitudinal edges of said side walls and ⁇ plate strips riveted to and connecting the latter flanges on adjoining edges.
  • a light sheet metal girder comprising two juxtaposed apertured side Walls and inwardly directed flanges surrounding the apertures of said walls, the flanges ol one side Wall extending in overlapping relation to the-flanges of the other side wall and be-v 10 ing rigidly connected therewith.

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Connection Of Plates (AREA)

Description

Feb; 2v, 1926. l
c. DoRNlER METAL GIRDER FOR ALJGH'I'y AMETAL STRUCTURES Filed Feb. '17. 192s Patented Feb. 2, 1926.
UNITED ,STATI-:s
eATENT- OFFICE.
cfLnUDIUs nomma. or .FRIEDRICHSHAFEN-oN-rHn-BonnNsnn, GERMANY, .as-f
SIGNOR :ro THE FIRM: noemen .METALLBAUTEN ensnnnscnu'r ma' BnscHRNx'rnn HAFTUNG, or .rnInnmcnsnunN-oN-THnLnoDnNsnn, GERMANY;
METAL GIBDEB FOB LIGHT METAL STRUCTURES.
l Application mea February 17, 192s. serial Na. classe.
To all whom t may concern:
Be it known that I, CLAUDrUs DoRmER,`
according to my'invention are provided with oppositely `located apertures 'having inwardly directed flanges which may extend so far insidethat they can be connected with each otherby riveting orvvelding.u The apv erture's may have any desired shape.
is', however, preferable to provide apertures of substantially equal shape and diameter.-
The inter-connected flanges of the apertures 'form hollow connecting members, the axis of which extends about at rightangles to the longitudinal axis of the girder.
The connection of the two side walls in the planes of the girths may be effected in any desired manner, for instance, by means of a panel, but it is preferred to provide the side walls in the girth plane with outwardly directed flan es and to connect'these latter with each ot er by a sheet-metal strip. In view of the comparative thinness of the sheet-metal em loyed in the construction of,
aircraft this a ords favorable conditions of assembling and `Warrants a good accessibility of the-rivet seams. The longitudinal edge portions of the side-walls are preferably bent outwards a-t an obtuse angle. The sheet-metal strips are preferably grooved or channelled.,
In the drawings /alxed to this specification and forming part thereof a girder embodying my invention is illustrated by way of example. In the drawing `Figure 1 is a cross section and V8 of sheet-metal, while the top formed' of a sheet-metal channel.
,apertures of said wal Figure 2 a side elevation` Referring to the drawing, the girderconsists of -twoside walls 1 and 2 provided with circular apertures A'having inwardly directed. flanges 3 and 4 which are fastened to each other by rivets 5.V If weldable metal is used', the flanges may be connected with each other by spot` welding. The longitudinal edge portions ofthe walls 1 and 2 are bent outwards forming flanges 6 and the rims 7 of these flanges are again bent in such a manner, that the flange rims 7 disposed on the same side converge as vshown in Figure 1.' A
The lower boom consists of a plain strip boom 9 is y"I wish it to be understood that I do not idesire to lbe limited to the exact details of constructionfshown and described, for obvious modifications,"will occur to a person skilled in the/art'.
I claimpg- 1. A lightsheet metal girder comprising two juxtaposed apertured side walls and inwardly 1 said flanges ing rigidy connected. 2. lightsheet metal irder com rising two uxtaposed aperture Ward y directed flanges surrounding the apertures of said wallsl, said flanges being rigidl connected Jand plate strips riveted to an connecting adjoining free edges of said side walls.
3. A'light sheet metal girder comprising two f'uxtaposed apertured side. walls, inward y directed flanges surrounding the apertures of said walls, said flan es being rigidly connected, ilanges extending substantially at right angles from the longitudinal edges of said side walls and `plate strips riveted to and connecting the latter flanges on adjoining edges. i
4. A light sheet metal irder com rising two juxtaposed aperture side wa ls, inwardly directed flanges surrounding the apertures of said Walls, said flanges being rigidly connected, -obtusely angular flanges exrected llan'gses surrounding) the.
side wa 1s, in-4 tending Substantially at righty angles from the longitudinal edges of said side walls and plate strips riveted to and connecting the latter flanges on adjoining edges.
5. A light sheet metal girder comprising two juxtaposed apertured side Walls and inwardly directed flanges surrounding the apertures of said walls, the flanges ol one side Wall extending in overlapping relation to the-flanges of the other side wall and be-v 10 ing rigidly connected therewith. In testimony whereof I alix my signature.
CLAUDIUS DORN IER.
US619696A 1923-02-17 1923-02-17 Metal girder for light metal structures Expired - Lifetime US1571239A (en)

Priority Applications (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

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US619696A US1571239A (en) 1923-02-17 1923-02-17 Metal girder for light metal structures

Publications (1)

Publication Number Publication Date
US1571239A true US1571239A (en) 1926-02-02

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US619696A Expired - Lifetime US1571239A (en) 1923-02-17 1923-02-17 Metal girder for light metal structures

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20080245928A1 (en) * 2007-04-05 2008-10-09 Kulesha Richard L Methods and systems for composite structural truss

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20080245928A1 (en) * 2007-04-05 2008-10-09 Kulesha Richard L Methods and systems for composite structural truss
US8490362B2 (en) * 2007-04-05 2013-07-23 The Boeing Company Methods and systems for composite structural truss

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