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By W. J. G. Bunk (auth.), Dr. Horst Buhl (eds.)

ISBN-10: 3642501591

ISBN-13: 9783642501593

ISBN-10: 3642501613

ISBN-13: 9783642501616

Very gentle, very powerful. tremendous trustworthy -aircraft and aerospace engineers are. and feature to be. very hard companions within the fabrics group. the result of their examine and improvement paintings isn't just the most important for one specific zone of purposes. yet may also paved the way to new recommendations in lots of different parts of complicated know-how. Springer-Verlag and the undersigned editor are happy to provide during this quantity. an outline of the various points of fabrics technological know-how and know-how which were the target of in depth and systematic study paintings in the course of earlier many years within the laboratories of the German Aerospace examine institution. Its contents exhibits in actual fact the interrelations among ambitions outlined by way of the consumer. basics supplied by way of the scientists and attainable options constructed via the sensible engineer. the actual personalized effect which has been given to this quantity via its authors in dedicating it as a farewell current to Professor Wolfgang Bunk. inspiring sci­ entist and director of the DLR Intitute of fabrics study for greater than twenty years. has evidently given an extra worth to this significant book. definitely. this actually cooperative endeavour will render a precious carrier to a wide interna­ tional group of readers. lots of them having own hyperlinks to the Institute. its director and its staff.

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By this treatment the size and volume fraction of the grain boundary precipitates is increased. The RRA treatment cannot readily be applied to thick sections because of the short time interval in stage (2). 2. Metallic Materials and Metal Matrix Composites 32 The need for high strength and higher toughness alloys stimulated extensive development programmes which led to alloy 7475. The main cause for the high fracture toughness of this alloy is a considerable reduction of the levels of iron and silicon impurities and thus a decrease in the volume fraction of coarse constituent particles, which are always detrimental for high fracture toughness.

Nevertheless, this behaviour of increased overaged toughness is advantageous for 7XXX alloys, which are used in the overaged T7 tempers because of their better corrosion properties. 2XXX alloys behave similarly. 2 [33]. With the development of damage tolerant, high strength, high toughness, and corrosion resistant 2XXX and 7XXX aerospace aluminium alloys a standard has been achieved at which considerable improvements cannot be expected for the same alloy systems. One example for a new promising alloy system is the use of lithium as a major alloying element to provide substantial weight savings.

The aging sequence can be given as SSSS ---+ GP zones -> 13' ---+ ~ (Mg2Si). The 6XXX alloys are medium strength alloys which are mostly corrosion resistant and readily weldable. One of them, 6061, is a general purpose alloy which is used for aircraft parts where no particular design characteristics are required. The alloy 6013, which has a higher copper content, is considerably stronger than 6061. Its properties in the T6 condition are comparable to 2024-T3; it is about 3% lighter and has excellent stretch forming characteristics.

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Advanced Aerospace Materials by W. J. G. Bunk (auth.), Dr. Horst Buhl (eds.)

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