US1427447A - Supporting plane - Google Patents
Supporting plane Download PDFInfo
- Publication number
- US1427447A US1427447A US392553A US39255320A US1427447A US 1427447 A US1427447 A US 1427447A US 392553 A US392553 A US 392553A US 39255320 A US39255320 A US 39255320A US 1427447 A US1427447 A US 1427447A
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- US
- United States
- Prior art keywords
- supporting plane
- supporting
- ribs
- central member
- girder
- 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
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-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
Definitions
- My invention relates to flying machines and more especially. to a specially simple type of supporting planes particularly suitable for manufacture on a large scale.
- the subj ect matter of my invention relates to a supporting plane for flying machinesconsisting of a central hollow body, constructed after the manner of a box girder, and bagshaped front and rear members suitable for being manufactured separately and independently of each other, and, after their completion, of being fixed to the said box girder.
- the frontmember or say, the rear member
- the frontmember may, when damaged, be easily exchanged.
- the method of staying or stiffening by aid of wires, or the like, may be done away with in the case of this improved construction, as the light joint members may be fixed along their whole length immediately 'tothe central member, say for example, by
- the central member constituting a boxgirder, consists of an upper and a lowersolid plate having an intermediate support composed of a plurality of longitudinal girders running across the full breadth of the supporting plane, along with a plurality of transverse ribs arranged intermediately, and provided also the pocket shaped front and rear members consist each of a frame of pressed sheet iron, of a cross-section offering the least possible resistance to the air, across the large recesses of which, reinforced by being fianged, there isdrawn a thin cover composed of cloth, paper, or the like.
- spars may advaptageously be inserted at regular interva s.
- the central hollow body, forming a box girder may further be provided with spars on to the free ends of which the bag-shaped front or rear members, reinforced at regular intervals by means of independent spars, may be slipped on.
- Fig. 2 is a horizontal section of the same along line 22 in l.
- Figs. 3 to 5 are vertical sections along lines 33, 4-4, 55, respectively, in Fig. l of, respectively, the front, central, and rear portions of asupporting plane.
- the central member of the supporting plane consists of two outer, longitudinal sheet iron girders a a each of which is constructed to form a hollow frame, and which, when assembled, constitute a selfsupporting box girder by aid of sheet iron wall portions a, which act as ribs, and outside plates A, which serve as chords.
- Both the longitudinal girders a a, as also the ribs or, are provided with circular indent-ures, partly beaded at the edges.
- the central portions of the ribs or are provided on top and at bottom with an indenture each through which the rods a of the lattice work girder, dividing the box girder practically into a forward and rearward chamber, are passed.
- the ribs (1 are continued in the shape of front ribs or. riveted to the girder a".
- the front member of the supporting plane consists of a pressed sheet iron frame B, open, baglike, in the direction of the central member, having on top and at bottom indentures b reinforced by headings. At regular intervals there are inserted plates 5 essentially resembling the ribs a and serving to maintain the shape, respectively, to stay the independent front member. This latter, when assembling the supporting plane, is slipped on to the ribs a, fixed to the central member, in such wise that the said ribs and the plates 71 are caused to alternate in succession.
- the manner of securing the parts is efiected by the rims of llltl the plates 6 which face the central member, being riveted or screwed to the front longitudinal girder a the upper and lower edges of the ribs (0* being fastened in a like manner to the cover B of the frame.
- the rear portion of the supporting plane consists of a sheet metal frame G, likewise open after the manner of a bag in the direc tion of the central member, while its upper and lower sides are provided with large indentures 0 Stiflening plates 0 resembling ribs, serve, on the one hand, to maintain the shape of the structure, and onthe other, to secure the rear member to the longitudinal girder a of the central member.
- the front and rear portions or their indentures, respectively, are covered with a plaincover of cloth, paper, or the like, for the purpose of guiding the air.
- the entire supporting plane may be made of metal, without thereby becoming heavier in weight than the supporting planes hitherto in use which are made of wood and of a lattice work with continuously arranged ribs and cross beams.
- a main supporting portion forming a box girder and separate front and rear portions adapted to be fixed thereto and serving mainly for guiding the air, said front and rear portions being formed each of a pressed sheet metal frame bent into shape and adapted to be connected with said main portion by its free edges.
- a main supporting portion forming a box girder and separate front and rear-portions adapted to be fixed thereto and serving mainly for guiding the air, said front and rear portions being formed each of a pressed sheet metal frame bent into shape, flanged indentures provided in said frames and a skin of suitable thin material covering said indentures.
- a main supporting portion forming a box girder .and separate front and rear portions adapted to be fixed thereto and serving mainly for guiding the air, said front and rear portions being formed each of a pressed sheet metal frame bent into shape and bent spars serving to stiffen said frames and to connect them wlthsaid main portion.
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Connection Of Plates (AREA)
Description
C. DORNIER.
SUPPORTING PLANE. APPLICATION FILED JUNE 28, 1920.
. 1 jagg yp q?" Y Patented Aug. 29, 1922.,
' Inventor:
UNE'HED STATES PATENT orsics.
CLAUDIUS DORNIER, OF 'FRIEDRICHSHAFEN, GERMANY, ASSIGNOR OF ONE-HALF TO DORNIER, METALLCBAUTEN, GESELLSCHAFT MIT BESCHRANKTER HAFTUNG,
OF FRIEDRICHSHAIEEN, GERMANY.
SUPPORTING ELAN E.
amas.
Application filed June 28,
T 0 all whom it may concern Be it known that I, CLAUDIUS DORNIER, a citizen of the German Empire, residing at Friedrichshafen, Germany, have invented certain new and useful Improvements in Supporting Planes (for which I have filed an application in Germany June 17, 1918), of which the following is a specification.
My invention relates to flying machines and more especially. to a specially simple type of supporting planes particularly suitable for manufacture on a large scale.
In accordance with the foregoing, the subj ect matter of my invention relates to a supporting plane for flying machinesconsisting of a central hollow body, constructed after the manner of a box girder, and bagshaped front and rear members suitable for being manufactured separately and independently of each other, and, after their completion, of being fixed to the said box girder. By the peculiar subdivision into a supporting central member, and two outside members, subjected to less strain and essentially only serving to conduct and dismiss the air, the construction of the said supporting plane is rendered specially simple; for each of the said three parts may, as said, be made separately, and all three may then readily be assembled to form a complete supporting plane. Moreover, in the caseof defects, the frontmember, or say, the rear member, may, when damaged, be easily exchanged. The method of staying or stiffening by aid of wires, or the like, may be done away with in the case of this improved construction, as the light joint members may be fixed along their whole length immediately 'tothe central member, say for example, by
riveting or screwing on. The manufacturing process will prove especially favorable, provided the central member, constituting a boxgirder, consists of an upper and a lowersolid plate having an intermediate support composed of a plurality of longitudinal girders running across the full breadth of the supporting plane, along with a plurality of transverse ribs arranged intermediately, and provided also the pocket shaped front and rear members consist each of a frame of pressed sheet iron, of a cross-section offering the least possible resistance to the air, across the large recesses of which, reinforced by being fianged, there isdrawn a thin cover composed of cloth, paper, or the like. For the better maintaining of the Specification of Letters Patent.
Patented Aug. 29, 1922.
1920. sc im No. 392,553.-
shape of the joint members, spars may advaptageously be inserted at regular interva s.
The central hollow body, forming a box girder may further be provided with spars on to the free ends of which the bag-shaped front or rear members, reinforced at regular intervals by means of independent spars, may be slipped on.
The preferred form of a supporting plane according to my present invention is 111118- trated in the accompanying drawings forming part of this specification. In the draw- 1ngs- F i 1 is a vertical section along line 1--1 in Fig. 2 of a supporting plane;
Fig. 2 is a horizontal section of the same along line 22 in l.
Figs. 3 to 5 are vertical sections along lines 33, 4-4, 55, respectively, in Fig. l of, respectively, the front, central, and rear portions of asupporting plane.
The central member of the supporting plane consists of two outer, longitudinal sheet iron girders a a each of which is constructed to form a hollow frame, and which, when assembled, constitute a selfsupporting box girder by aid of sheet iron wall portions a, which act as ribs, and outside plates A, which serve as chords. Both the longitudinal girders a a, as also the ribs or, are provided with circular indent-ures, partly beaded at the edges. The central portions of the ribs or are provided on top and at bottom with an indenture each through which the rods a of the lattice work girder, dividing the box girder practically into a forward and rearward chamber, are passed. Beyond the longitudinal girder a the ribs (1 are continued in the shape of front ribs or. riveted to the girder a".
The front member of the supporting plane consists of a pressed sheet iron frame B, open, baglike, in the direction of the central member, having on top and at bottom indentures b reinforced by headings. At regular intervals there are inserted plates 5 essentially resembling the ribs a and serving to maintain the shape, respectively, to stay the independent front member. This latter, when assembling the supporting plane, is slipped on to the ribs a, fixed to the central member, in such wise that the said ribs and the plates 71 are caused to alternate in succession. The manner of securing the parts is efiected by the rims of llltl the plates 6 which face the central member, being riveted or screwed to the front longitudinal girder a the upper and lower edges of the ribs (0* being fastened in a like manner to the cover B of the frame.
The rear portion of the supporting plane, consists of a sheet metal frame G, likewise open after the manner of a bag in the direc tion of the central member, while its upper and lower sides are provided with large indentures 0 Stiflening plates 0 resembling ribs, serve, on the one hand, to maintain the shape of the structure, and onthe other, to secure the rear member to the longitudinal girder a of the central member.
After the three single parts, primarily constructed per se, have been combined to form the complete supporting plane, the front and rear portions or their indentures, respectively, are covered with a plaincover of cloth, paper, or the like, for the purpose of guiding the air.
Apartfrom this cover, the entire supporting plane may be made of metal, without thereby becoming heavier in weight than the supporting planes hitherto in use which are made of wood and of a lattice work with continuously arranged ribs and cross beams.
I claim 1. In a, supporting surface in combination,
a main supporting portion forming a box girder and separate front and rear portions adapted to be fixed thereto and serving mainly for guiding the air, said front and rear portions being formed each of a pressed sheet metal frame bent into shape and adapted to be connected with said main portion by its free edges.
2. In a supporting surface in combination, a main supporting portion forming a box girder and separate front and rear-portions adapted to be fixed thereto and serving mainly for guiding the air, said front and rear portions being formed each of a pressed sheet metal frame bent into shape, flanged indentures provided in said frames and a skin of suitable thin material covering said indentures.
3. In a supporting surface in combination, a main supporting portion forming a box girder .and separate front and rear portions adapted to be fixed thereto and serving mainly for guiding the air, said front and rear portions being formed each of a pressed sheet metal frame bent into shape and bent spars serving to stiffen said frames and to connect them wlthsaid main portion.
In testimony whereof I affix my signature.
oLAUDiUs DORNIER.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US392553A US1427447A (en) | 1920-06-28 | 1920-06-28 | Supporting plane |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US392553A US1427447A (en) | 1920-06-28 | 1920-06-28 | Supporting plane |
Publications (1)
Publication Number | Publication Date |
---|---|
US1427447A true US1427447A (en) | 1922-08-29 |
Family
ID=23551037
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US392553A Expired - Lifetime US1427447A (en) | 1920-06-28 | 1920-06-28 | Supporting plane |
Country Status (1)
Country | Link |
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US (1) | US1427447A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2451454A (en) * | 1943-06-28 | 1948-10-12 | Budd Co | Method of fabricating airfoils |
-
1920
- 1920-06-28 US US392553A patent/US1427447A/en not_active Expired - Lifetime
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2451454A (en) * | 1943-06-28 | 1948-10-12 | Budd Co | Method of fabricating airfoils |
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