DE2449932A1 - Lightweight strong structural element - has aluminium sheeting combined with hard foam plastics material - Google Patents
Lightweight strong structural element - has aluminium sheeting combined with hard foam plastics materialInfo
- Publication number
- DE2449932A1 DE2449932A1 DE19742449932 DE2449932A DE2449932A1 DE 2449932 A1 DE2449932 A1 DE 2449932A1 DE 19742449932 DE19742449932 DE 19742449932 DE 2449932 A DE2449932 A DE 2449932A DE 2449932 A1 DE2449932 A1 DE 2449932A1
- Authority
- DE
- Germany
- Prior art keywords
- sheet
- combined
- structural element
- plastics material
- hard foam
- 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.)
- Pending
Links
- 239000006260 foam Substances 0.000 title abstract description 6
- 239000004033 plastic Substances 0.000 title abstract 3
- 229920003023 plastic Polymers 0.000 title abstract 3
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 title 1
- 229910052782 aluminium Inorganic materials 0.000 title 1
- 239000004411 aluminium Substances 0.000 title 1
- 239000000463 material Substances 0.000 title 1
- 238000010276 construction Methods 0.000 claims description 9
- 239000002984 plastic foam Substances 0.000 claims description 6
- 229910052751 metal Inorganic materials 0.000 abstract description 5
- 239000002184 metal Substances 0.000 abstract description 5
- 239000000853 adhesive Substances 0.000 abstract description 3
- 230000001070 adhesive effect Effects 0.000 abstract description 3
- 238000005452 bending Methods 0.000 abstract description 3
- 238000004519 manufacturing process Methods 0.000 abstract description 3
- 229910000838 Al alloy Inorganic materials 0.000 abstract description 2
- 238000005253 cladding Methods 0.000 abstract 2
- 239000002131 composite material Substances 0.000 abstract 1
- 239000000945 filler Substances 0.000 abstract 1
- 238000005728 strengthening Methods 0.000 abstract 1
- 238000000034 method Methods 0.000 description 1
- 229920002635 polyurethane Polymers 0.000 description 1
- 239000004814 polyurethane Substances 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 238000004381 surface treatment Methods 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B15/00—Layered products comprising a layer of metal
- B32B15/04—Layered products comprising a layer of metal comprising metal as the main or only constituent of a layer, which is next to another layer of the same or of a different material
- B32B15/08—Layered products comprising a layer of metal comprising metal as the main or only constituent of a layer, which is next to another layer of the same or of a different material of synthetic resin
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B15/00—Layered products comprising a layer of metal
- B32B15/04—Layered products comprising a layer of metal comprising metal as the main or only constituent of a layer, which is next to another layer of the same or of a different material
- B32B15/046—Layered products comprising a layer of metal comprising metal as the main or only constituent of a layer, which is next to another layer of the same or of a different material of foam
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B15/00—Layered products comprising a layer of metal
- B32B15/20—Layered products comprising a layer of metal comprising aluminium or copper
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B5/00—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
- B32B5/18—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by features of a layer of foamed material
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B7/00—Layered products characterised by the relation between layers; Layered products characterised by the relative orientation of features between layers, or by the relative values of a measurable parameter between layers, i.e. products comprising layers having different physical, chemical or physicochemical properties; Layered products characterised by the interconnection of layers
- B32B7/04—Interconnection of layers
- B32B7/12—Interconnection of layers using interposed adhesives or interposed materials with bonding properties
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/20—Integral or sandwich constructions
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2307/00—Properties of the layers or laminate
- B32B2307/50—Properties of the layers or laminate having particular mechanical properties
- B32B2307/544—Torsion strength; Torsion stiffness
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2307/00—Properties of the layers or laminate
- B32B2307/70—Other properties
- B32B2307/718—Weight, e.g. weight per square meter
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2605/00—Vehicles
- B32B2605/18—Aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Laminated Bodies (AREA)
- Toys (AREA)
Abstract
Description
Dünnblech-Kunststoffschaum-Sauweise Es hanaelt sich hier um eine ibeichtbauweise bestehend aus festen Leichtmetallblechen in Kombination mit harten Kunststoffschäumen.Dabei werden die optimalen Widerstandsmomente der Bleche (möglichst große Entfernung von der Biege- bzw. Torsionsachse -hauptsächlich Außentragend ) voll amsgenutzt.Thin sheet plastic foam method of construction It is a case of a lightweight construction Consists of solid light metal sheets in combination with hard plastic foams the optimum moments of resistance of the sheets (as large as possible from the bending or torsion axis - mainly external load-bearing) is fully utilized.
Mit dem dazwischenliegenden bzw. umgebenden Kunststoffschaum wird die Knicksteifigkeit des Dünnbleches erhöht.With the intermediate or surrounding plastic foam the buckling resistance of the thin sheet is increased.
Beispiel: Flugzeugleitwerk 4 m Spannweite Zugeschnittenes 0,5 mm Blech ( Al-Legierung) wird in eine zweiteilige Form gelegt und zugleich mit dem Schließen um die Nasenkante gebogen (die Endseiten des Profils werden dabei mit einem Metallkleber zusammengeklebt).Mit hartem Tolyurethan-Leichtschaum wird die Form ausgegossen.Dabei wird das @lech in die Form gepreßt. (siehe Zeichnung Abb.3) Die Vorteile dieser Bauweise gegenüber den entsprechenden jetzigen technischen Stand (Schaum mit GfK umgeben) liegt hauptsächlich in der schnellen Fertigung.Example: Aircraft tail unit 4 m span Cut 0.5 mm sheet metal (Al alloy) is placed in a two-part mold and at the same time as it is closed bent around the edge of the nose (the end sides of the profile are attached with a metal adhesive The mold is filled with hard polyurethane lightweight foam the @lech is pressed into the mold. (see drawing Fig.3) The advantages of this Construction method compared to the corresponding current technical status (foam with GRP surrounded) is mainly due to the fast production.
-3ei Einzelanfertigung oder großen Teilen kann auf die Form verzichtet werden,wenn durch innere Stützbleche ein Ausbeulen des bleches verhindert wird (siehe Abb.4).- In the case of one-off production or large parts, the shape can be dispensed with if the inner support plates prevent the plate from buckling (see Fig.4).
Für genügende Verbindung zwischen Schaum und Blech sorgt meistens der Jchaurm selbst. Oberflächenbearbeitungen sind nicht mehr nötig. An höher beanspruchten Teilen können zusätzlich Versteifurgen eingebracht werden oder der Schaum verdichtst werden.A sufficient connection between foam and sheet metal is usually provided the Jchaurm itself. Surface treatments are no longer necessary. At higher stressed Parts can also be stiffened or the foam can be compressed will.
Anwendungsgebiete: Flugzeugbau,Fahrzeugbau,allgemeiner Bausektor usw.Areas of application: aircraft construction, vehicle construction, general construction sector, etc.
Claims (1)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE19742449932 DE2449932A1 (en) | 1974-10-21 | 1974-10-21 | Lightweight strong structural element - has aluminium sheeting combined with hard foam plastics material |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE19742449932 DE2449932A1 (en) | 1974-10-21 | 1974-10-21 | Lightweight strong structural element - has aluminium sheeting combined with hard foam plastics material |
Publications (1)
Publication Number | Publication Date |
---|---|
DE2449932A1 true DE2449932A1 (en) | 1976-04-29 |
Family
ID=5928758
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE19742449932 Pending DE2449932A1 (en) | 1974-10-21 | 1974-10-21 | Lightweight strong structural element - has aluminium sheeting combined with hard foam plastics material |
Country Status (1)
Country | Link |
---|---|
DE (1) | DE2449932A1 (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE2814166A1 (en) * | 1978-04-01 | 1979-10-04 | Focke & Co | PARTITION WALL, IN PARTICULAR MANHOLE WALL FOR CIGARETTE MAGAZINE AND PROCESS AND DEVICE FOR PRODUCING THE SAME |
EP2377757A1 (en) * | 2010-04-19 | 2011-10-19 | Gatewing NV | A wing for an unmanned aircraft |
-
1974
- 1974-10-21 DE DE19742449932 patent/DE2449932A1/en active Pending
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE2814166A1 (en) * | 1978-04-01 | 1979-10-04 | Focke & Co | PARTITION WALL, IN PARTICULAR MANHOLE WALL FOR CIGARETTE MAGAZINE AND PROCESS AND DEVICE FOR PRODUCING THE SAME |
EP2377757A1 (en) * | 2010-04-19 | 2011-10-19 | Gatewing NV | A wing for an unmanned aircraft |
WO2011131382A1 (en) * | 2010-04-19 | 2011-10-27 | Gatewing Nv | A wing for an unmanned aircraft |
CN102858630A (en) * | 2010-04-19 | 2013-01-02 | 加特温股份有限公司 | A wing for an unmanned aircraft |
US8827206B2 (en) | 2010-04-19 | 2014-09-09 | Gatewing Nv | Wing for an unmanned aircraft |
CN102858630B (en) * | 2010-04-19 | 2015-09-09 | 加特温股份有限公司 | For the unmanned plane of image acquisition or supervision |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
OHJ | Non-payment of the annual fee |