DE335101C - Veneer cladding for aircraft parts - Google Patents
Veneer cladding for aircraft partsInfo
- Publication number
- DE335101C DE335101C DENDAT335101D DE335101DD DE335101C DE 335101 C DE335101 C DE 335101C DE NDAT335101 D DENDAT335101 D DE NDAT335101D DE 335101D D DE335101D D DE 335101DD DE 335101 C DE335101 C DE 335101C
- Authority
- DE
- Germany
- Prior art keywords
- veneer
- aircraft parts
- cladding
- panels
- aircraft
- 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
Links
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
- B64C1/12—Construction or attachment of skin panels
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Finished Plywoods (AREA)
Description
Furnierbekleidung für Flugzeugteile. Infolge der anhaltenden Knappheit an Bespannungsstoffen für Flugzeuge ist man immer mehr dazu übergegangen, die Flügel und andere Teile der Flugzeuge mit Furnier zu verkleiden. Dies hat natürlich eine wesentliche Änderung in den Arbeitsverfahren des Flugzeugbaues mit sich gebracht.Veneer cladding for aircraft parts. As a result of the continuing shortage When it comes to covering fabrics for aircraft, more and more people have moved on to the wings and to clad other parts of the aircraft with veneer. This of course has one brought about significant change in the working procedures of aircraft construction.
Bislang wurden die Furnierplatten durch Aufnageln auf die Spieren usw. verbunden, was aber verschiedene Unbequemlichkeiten, namentlich bei Ausbesserungen der betreffenden Flugzeugteile, mit sich brachte. Nach der den Gegen-' stand der Erfindung bildenden Neuerung werden nun die Furnierplatten nicht durch Aufnageln verbunden, sondern sie werden mit einer Umfalzung versehen, und je zwei Umfalzungen werden mit einem dazwischen eingesetzten Steg. (als Ersatz der Spiere) durch Rohrniete o. dg1. vereinigt.Until now, the veneer panels were nailed to the spars etc., which, however, caused various inconveniences, especially when making repairs of the aircraft parts concerned. According to the subject of the Invention forming innovation are now the veneer panels not by nailing connected, but they are provided with a fold, and two folds each with a bar inserted in between. (to replace the spar) with tubular rivets o. dg1. united.
Fig. = der Zeichnung stellt diese Art der Anbringung von Furnierverkleidung schematisch dar. a und a1 sind zwei aneinanderstoßende Furnierplatten, b und e1 die umgefalzten Flächen, c ist der dazwischen eingesetzte Steg und d ein Rohrniet.Fig. = The drawing shows this type of attachment of veneer cladding a and a1 are two butting veneer panels, b and e1 the folded surfaces, c is the web inserted in between and d a tubular rivet.
Eine Abänderung dieser Verbindung ist in Fig: 2 der Zeichnung schematisch dargestellt. Hierbei werden die Furnierplatten a und a1 nicht umgefalzt, sondern sie sind miteinander und mit dem Steg c durch Winkel e, e1 aus Furnier, Metall o. dgl. vereinigt; diese Winkel sind am Rande jeder Furnierplatte durch Rohrniete dl, d2 befestigt. Die Zusammensetzung wird in derselben Weise, wie oben beschrieben, ausgeführt.A modification of this connection is shown schematically in FIG. 2 of the drawing shown. Here, the veneer panels a and a1 are not folded over, but they are with each other and with the web c by angles e, e1 made of veneer, metal o. like. united; these angles are on the edge of each veneer panel by tubular rivets dl, d2 attached. The composition is made in the same way as described above, executed.
Durch diese Art der Verkleidung ist man stets in der Lage, Ausbesserungen mit außerordentlich geringem Aufwand an Zeit und Material auszuführen. Außerdem bedingt die neue Anordnung eine erhöhte Festigkeit des ganzen Flügelsystems, welche durch die volle Ausnutzung der Holmhöhe und durch die Winkelaufsätze erzielt wird.With this type of cladding you are always able to make repairs to be carried out with extremely little expenditure of time and material. aside from that The new arrangement causes an increased strength of the entire wing system, which is achieved by fully utilizing the stile height and the angle attachments.
Claims (1)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE335101T |
Publications (1)
Publication Number | Publication Date |
---|---|
DE335101C true DE335101C (en) | 1921-03-26 |
Family
ID=6218937
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DENDAT335101D Expired DE335101C (en) | Veneer cladding for aircraft parts |
Country Status (1)
Country | Link |
---|---|
DE (1) | DE335101C (en) |
-
0
- DE DENDAT335101D patent/DE335101C/en not_active Expired
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