Aerospace MaterialsBrian Cantor, H Assender, P. Grant CRC Press, 06.05.2015 - 312 Seiten Aerospace Materials provides a grounding in state-of-the-art aerospace materials technology, including developments in aluminum, titanium, and nickel alloys, as well as polymers and polymer composites. Experts in each topic have contributed key overviews that summarize current knowledge and indicate future trends. The book begins by outlining the i |
Inhalt
3 | |
2 Advanced materials and process technologies for aerospace structures | 15 |
3 Materials for supersonic civil transport aircraft | 28 |
4 Aluminiumlithium alloys in helicopter airframes | 38 |
5 High performance polymers and advanced composites for space application | 47 |
6 Advanced polymer composite propeller blades | 59 |
7 Materials developments in aeroengine gas turbines | 71 |
8 Blading materials and systems in advanced aeroengines | 81 |
13 Matrix and fibre systems in polymer matrix composites | 179 |
14 Toughened thermoset resin matrix composites | 187 |
15 Hydrophobic epoxies for polymer matrix composites | 199 |
16 Technical and economic considerations influencing the role of advanced polymer composites in airframe applications | 213 |
17 TiAlbased alloys for aeroengine applications | 229 |
18 Titanium metal matrix composites | 241 |
19 Anisotropic creep in single crystal superalloys | 253 |
20 Microstructural evolution in single crystal nickelbased superalloys during high temperature creep | 265 |
9 Advances in aerospace materials and structures | 91 |
10 Fatigue optimization in aerospace aluminium alloys | 119 |
11 Bulk amorphous nanocrystalline and nanoquasicrystalline aluminium alloys | 150 |
12 High toughness metal matrix composites | 170 |
21 Effects of tantalum and rhenium on creep in single crystals of nickel20 chromium | 285 |
22 Thermal barrier coatings | 294 |
Back Cover | 311 |
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Häufige Begriffe und Wortgruppen
achieved aeroengine aerospace aircraft airframe Al-Li Al-Li alloys aluminium alloys aluminium-based alloys amorphous applications behaviour blade Burgers vector ceramic chapter Cl2-TGDDM closure components cost crack growth crack-tip creep deformation creep rate curves damage tolerance deformation density dislocations ductility effect electron engine epoxy fatigue crack fcc aluminium fracture toughness grain boundaries growth rates heat treatment high strength high temperature hot–wet icosahedral improved increase Inoue interface loading Lutjering manufacturing materials MCrAlY mechanical properties metal matrix composites microstructure modulus nickel optimization orientation oxidation particles performance phase plasma spraying plastic polyimide polymer polymer composites pre-preg produce reduce resin transfer moulding resistance rhenium shear strength shown in figure significant single crystal slip specimens strain stress structures superalloys superplastic superplastic forming tantalum tensile strength TGDDM thermal barrier coatings thermoplastic thickness TiAl-based alloys titanium alloys titanium MMCs toughening Trans vertical channels weight saving