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- GLARE abstract "Glass laminate aluminium reinforced epoxy (GLARE) is a fiber metal laminate (FML) composed of several very thin layers of metal (usually aluminium) interspersed with layers of glass-fiber \"pre-preg\", bonded together with a matrix such as epoxy. The uni-directional pre-preg layers may be aligned in different directions to suit the predicted stress conditions.Although GLARE is a composite material, its material properties and fabrication are very similar to bulk aluminium metal sheets. It has far less in common with composite structures when it comes to design, manufacture, inspection or maintenance. GLARE parts are constructed and repaired using mostly conventional metal material techniques.Its major advantages over conventional aluminium are: Better \"damage tolerance\" behavior (especially impact and metal fatigue, as the elastic strain is larger than other metal material it can consume more impact energy. It is dented easier but has a higher penetration resistance ) Better corrosion resistance Better fire resistance Lower specific weightFurthermore, it is possible to \"tailor\" the material during design and manufacture such that the number, type and alignment of layers can suit the local stresses and shapes throughout the aircraft. This allows the production of double-curved sections, complex integrated panels or very large sheets, for example.While a simple manufactured sheet of GLARE will be more expensive than an equivalent sheet of aluminium, considerable production savings can be made using the aforementioned optimization. A structure properly designed for GLARE will be significantly lighter and less complex than an equivalent metal structure, and will require less inspection and maintenance and enjoy a much longer lifetime-till failure, making it a cheaper, lighter and safer option overall.".
- GLARE wikiPageExternalLink pagina.jsp?id=f75b9280-88fd-40e8-970d-6eff6dd33c85&lang=en.
- GLARE wikiPageExternalLink ORI-Aviation-Materials-2009.
- GLARE wikiPageID "908694".
- GLARE wikiPageLength "7619".
- GLARE wikiPageOutDegree "45".
- GLARE wikiPageRevisionID "681198321".
- GLARE wikiPageWikiLink 3M.
- GLARE wikiPageWikiLink Airbus_A380.
- GLARE wikiPageWikiLink AkzoNobel.
- GLARE wikiPageWikiLink Alcoa.
- GLARE wikiPageWikiLink Aluminium.
- GLARE wikiPageWikiLink Aramid.
- GLARE wikiPageWikiLink Boeing.
- GLARE wikiPageWikiLink Boeing_737.
- GLARE wikiPageWikiLink Boeing_C-17_Globemaster_III.
- GLARE wikiPageWikiLink Bombardier_Inc..
- GLARE wikiPageWikiLink Category:Composite_materials.
- GLARE wikiPageWikiLink Category:Heterogeneous_chemical_mixtures.
- GLARE wikiPageWikiLink Composite_material.
- GLARE wikiPageWikiLink Corrosion.
- GLARE wikiPageWikiLink Cytec_Industries.
- GLARE wikiPageWikiLink Damage_tolerance.
- GLARE wikiPageWikiLink De_Havilland.
- GLARE wikiPageWikiLink Delft_University_of_Technology.
- GLARE wikiPageWikiLink Epoxy.
- GLARE wikiPageWikiLink Fatigue_(material).
- GLARE wikiPageWikiLink Fiber_metal_laminate.
- GLARE wikiPageWikiLink Fire.
- GLARE wikiPageWikiLink Fokker.
- GLARE wikiPageWikiLink Glass-fiber.
- GLARE wikiPageWikiLink Impact_(mechanics).
- GLARE wikiPageWikiLink Learjet_45.
- GLARE wikiPageWikiLink McDonnell_Douglas.
- GLARE wikiPageWikiLink NASA.
- GLARE wikiPageWikiLink Pan_Am_Flight_103.
- GLARE wikiPageWikiLink Pre-preg.
- GLARE wikiPageWikiLink Research_and_development.
- GLARE wikiPageWikiLink Space_Shuttle.
- GLARE wikiPageWikiLink Specific_weight.
- GLARE wikiPageWikiLink Stork_B.V..
- GLARE wikiPageWikiLink Stress_(mechanics).
- GLARE wikiPageWikiLink TU_Delft_Faculty_of_Aerospace_Engineering.
- GLARE wikiPageWikiLink Unit_load_device.
- GLARE wikiPageWikiLink United_States_Air_Force.
- GLARE wikiPageWikiLinkText "GLARE".
- GLARE wikiPageUsesTemplate Template:!.
- GLARE wikiPageUsesTemplate Template:About.
- GLARE wikiPageUsesTemplate Template:Advert.
- GLARE subject Category:Composite_materials.
- GLARE subject Category:Heterogeneous_chemical_mixtures.
- GLARE hypernym Laminate.
- GLARE type Redirect.
- GLARE comment "Glass laminate aluminium reinforced epoxy (GLARE) is a fiber metal laminate (FML) composed of several very thin layers of metal (usually aluminium) interspersed with layers of glass-fiber \"pre-preg\", bonded together with a matrix such as epoxy. The uni-directional pre-preg layers may be aligned in different directions to suit the predicted stress conditions.Although GLARE is a composite material, its material properties and fabrication are very similar to bulk aluminium metal sheets.".
- GLARE label "GLARE".
- GLARE sameAs Q1529438.
- GLARE sameAs Glare.
- GLARE sameAs Glasfaserverstärktes_Aluminium.
- GLARE sameAs Vidrio_reforzado.
- GLARE sameAs GLARE.
- GLARE sameAs Glare.
- GLARE sameAs GLARE.
- GLARE sameAs m.03nyqd.
- GLARE sameAs GLARE.
- GLARE sameAs Q1529438.
- GLARE wasDerivedFrom GLARE?oldid=681198321.
- GLARE isPrimaryTopicOf GLARE.