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  • 1
    Electronic Resource
    Electronic Resource
    Weinheim : Wiley-Blackwell
    Chemie Ingenieur Technik - CIT 48 (1976), S. 765-773 
    ISSN: 0009-286X
    Keywords: Chemistry ; Polymer and Materials Science
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Chemistry and Pharmacology , Process Engineering, Biotechnology, Nutrition Technology
    Notes: Fortschrittliche faserverstärkte Verbundwerkstoffe basieren auf Endlos-Fasern, welche im Unterschied zu den seit Jahren verwendeten Glasfasern nicht nur hohe Festigkeit, sondern auch hohe Steifigkeit bei geringer Dichte (hoher spezifischer E-Modul) aufweisen. Es wird der Stand der Technik in bezug auf die Herstellung, Eigenschaften, Verfügbarkeit und Kosten folgender Verstärkungsfasern besprochen: organische Fasern (Polyaramid-Fasern), Kohlenstoff-Fasern aus PAN und Pechprecursor, Bor- und SiC-Fasern und Al2O3-Fasern. Es werden die erzielbaren mechanischen Eigenschaften von faserverstärkten Polymeren mit diesen Fasertypen aufgezeigt.
    Additional Material: 17 Ill.
    Type of Medium: Electronic Resource
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  • 2
    Publication Date: 1984-01-01
    Print ISSN: 0008-6223
    Electronic ISSN: 1873-3891
    Topics: Chemistry and Pharmacology , Geosciences
    Published by Elsevier
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  • 3
    Publication Date: 2004-12-03
    Description: Materials and manufacturing technology are critical to advanced aircraft and permeate all disciplines. Current aircraft systems employ a variety of materials, each selected to provide the best vehicle design in terms of performance, safety, reliability, manufacturability, and life cycle cost. However, a mistake in materials selection could bankrupt an airframe or engine manufacturer. Thus, the introduction of new materials is a slow process. Generally, new materials are used initially in noncritical components until their performance in service can be confirmed. Then, as confidence grows, they are used in more and more critical applications. Finally, if appropriate, new materials are used in critical, static elements and then in dynamic components. Thus, because the nominal time for development of a conventional monolithic material ranges from 5 to 10 years there is a 10- to 15- year lag between laboratory effort and introduction into service. Therefore, to assure the availability of materials suitable for production aircraft and engines in the year 2000, the concepts already must have been identified and must be progressing along evolutionary paths toward application. Trends, actual and projected, in the use of materials for commercial engines are shown in Figure 4-1. Related military applications are projected to follow similar paths. The new actor will be composites. The panel examined a wide range of materials important to all aspects of aircraft development, airframe structures, propulsion systems and for other important aircraft subsystems. These are addressed in the body of the report in terms of the current state of the art, opportunities for improvement, and barriers to achievement of projected benefits. This is followed by projections of the progress of technology that could be realized by the year 2000 with the application of appropriate resources.
    Keywords: Composite Materials
    Type: Aeronautics Technology Possibilities for 2000: Report of a Workshop; 99-128; NASA-CR-205283
    Format: text
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