DE1640339U - CLADDING SCREW CLAMP FOR AIRCRAFT CONSTRUCTION. - Google Patents
CLADDING SCREW CLAMP FOR AIRCRAFT CONSTRUCTION.Info
- Publication number
- DE1640339U DE1640339U DE1952D0004125 DED0004125U DE1640339U DE 1640339 U DE1640339 U DE 1640339U DE 1952D0004125 DE1952D0004125 DE 1952D0004125 DE D0004125 U DED0004125 U DE D0004125U DE 1640339 U DE1640339 U DE 1640339U
- Authority
- DE
- Germany
- Prior art keywords
- screw clamp
- planking
- clamps
- screw
- cladding
- 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
- 238000005253 cladding Methods 0.000 title claims description 6
- 238000010276 construction Methods 0.000 title description 3
- 229910000831 Steel Inorganic materials 0.000 description 3
- 239000010959 steel Substances 0.000 description 3
- 239000003292 glue Substances 0.000 description 2
- 238000004026 adhesive bonding Methods 0.000 description 1
- 239000000463 material Substances 0.000 description 1
Landscapes
- Clamps And Clips (AREA)
- Gripping Jigs, Holding Jigs, And Positioning Jigs (AREA)
Description
AnmeldungeinesGebrauchsmusters 1. Gegenstand Beplankungsschraubzwinge
für den Flugzeugbau 2. Erfinder Ing. Herbert Panne, Carthausen/Westf.
4. Beschreibung Die Tragfläche eines in Holzbauweise hergestellten Flugzeuges wird in der Regel aus der vorderen und der einteren Hälfte zusammengesetzt, wobei die beiden Hälften vor dem Zusammenbau mit der Beplankung versehen werden. Die Beplankung wird aufgeleimt und es istv schwierig dieses gleichmäßig auszuführen. Die Beplankungssohraubzwinge soll hierbei als Hil@smittel dienen und die notwendigen gleichmäßigen Verleimungsdrlcke erzeugen.4. Description The wing of a wooden structure The aircraft is usually composed of the front and the first half, the two halves are provided with the planking prior to assembly. The planking is glued on and it is difficult to do this evenly. The planking screw clamp should serve as an aid and provide the necessary Generate even gluing pressure.
Die Beplankungsschraubzwinge besteht aus folgenden Einzelteilen : 1. Stahl schiene (a) 2. Schraubzwingenpaar (b und o) 3. Hilfszwingen (d und e) Die beiden Schraubzwingenpaare sind verschiebbar und feststellbar auf der Stahlschiene (a) angeordnet. Nach Auftragen der Leimschicht und Auflagen des Beplankungsmaterials werden die überstehenden Enden der Beplankung (f und g) an beiden Seiten in die Schraubzwingen gespannt. Anschließend werden die Hilfskreuzzwingen (d u. e) bekannter Konstruktion auf die Stahlsohiene gesetzt und so fest gegen den Holm (h) gedreht bis die Beplankung fest anliegt. The cladding screw clamp consists of the following individual parts: 1. Steel rail (a) 2. Pair of screw clamps (b and o) 3. Auxiliary clamps (d and e) Die Both pairs of screw clamps can be moved and locked on the steel rail (a) arranged. After applying the glue layer and placing the cladding material the protruding ends of the planking (f and g) on both sides are inserted into the Screw clamps tensioned. Then the auxiliary cross clamps (d and e) become more familiar The construction is placed on the steel rail and so firmly rotated against the stile (h) until the planking is tight.
Nachdem die Leimschicht gebunden hat kann die Spannung gelöst werden. After the glue layer has bonded, the tension can be released.
Um an den Enden der Beplankung gleichmäßige Druckkräfte zu erzeugen empfiehlt es sich die Beplankungszwingen in möglichst kurzen Abständen anzusetzen. In order to generate even pressure forces at the ends of the planking it is recommended to use the cladding clamps as short as possible.
Claims (4)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE1952D0004125 DE1640339U (en) | 1952-04-24 | 1952-04-24 | CLADDING SCREW CLAMP FOR AIRCRAFT CONSTRUCTION. |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE1952D0004125 DE1640339U (en) | 1952-04-24 | 1952-04-24 | CLADDING SCREW CLAMP FOR AIRCRAFT CONSTRUCTION. |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| DE1640339U true DE1640339U (en) | 1952-07-03 |
Family
ID=30453196
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| DE1952D0004125 Expired DE1640339U (en) | 1952-04-24 | 1952-04-24 | CLADDING SCREW CLAMP FOR AIRCRAFT CONSTRUCTION. |
Country Status (1)
| Country | Link |
|---|---|
| DE (1) | DE1640339U (en) |
-
1952
- 1952-04-24 DE DE1952D0004125 patent/DE1640339U/en not_active Expired
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