"Uplatn\u011Bn\u00ED hi-tech kompozitn\u00EDch materi\u00E1l\u016F v prim\u00E1rn\u00ED konstrukci trupu civiln\u00EDho dopravn\u00EDho letadla v kategorii CS 23 / FAR 23." . "Applying of hi-tech composite materials in fuselage primary structure of commercial aeroplane in the category CS 23/ FAR 23."@en . . "http://www.isvav.cz/projectDetail.do?rowId=FT-TA3/153"^^ . . "Research in the field of advanced composite materials application in the aeroplane fuselage design and structural and technological study of composite aeroplane fuselage in category CS 23/ FAR 23. Principal aim of the project is creation a design of the fuselage by advanced composite materials on a model section. The static, dynamic and environmental tests will be developed and carried out according to the authorized certification methodology. The final issue of the project will be an integrated set of data as base for development and certification process of the composite fuselage in accordance with CAA (Civil Aviation Authority) procedures."@en . . . "V\u00FDzkum v oblasti aplikace \u0161pi\u010Dkov\u00FDch kompozitn\u00EDch materi\u00E1l\u016F v konstrukci trupu a zpracov\u00E1n\u00ED konstruk\u010Dn\u00ED a technologick\u00E9 studie kompozitn\u00EDho trupu letounu v kategorii CS 23/ FAR 23, realizovateln\u00E1 a\u017E do st\u00E1dia modelov\u00E9 sekce. Budou vyvinuty a provedeny statick\u00E9, dynamick\u00E9 a klimatotechnologick\u00E9 zkou\u0161ky, jako podklad pro vytvo\u0159en\u00ED certifika\u010Dn\u00ED metodiky. C\u00EDlem jsou ucelen\u00E9 podklady pro v\u00FDvoj a certifikaci kompozitn\u00EDho trupu." . "1"^^ . "3"^^ . . " NDT" . "2009-12-31+01:00"^^ . "2009-12-04+01:00"^^ . . . "0"^^ . . "2010-06-21+02:00"^^ . " aeroplane structure testing" . . . "12"^^ . . "12"^^ . . "Navr\u017Een celokompozitn\u00ED trup mal\u00E9ho dopravn\u00EDho letounu. N\u00E1vrh ov\u011B\u0159en v\u00FDrobou zku\u0161ebn\u00EDch sekc\u00ED, kter\u00E9 byly podrobeny zkou\u0161k\u00E1m. Trup je o 20% leh\u010D\u00ED, obsahuje o 85% m\u00E9n\u011B d\u00EDl\u016F a je o 7% levn\u011Bj\u0161\u00ED ne\u017E srovnateln\u00E1 kovov\u00E1 varianta."@cs . " aeroplane fuselage" . . . "Design of the small transport aircraft has been performed. It has been verified by production of test sections subjected to tests. Designed all composite fuselage is 20% lighter, contain 85% less parts and it is 7% cheaper then comparable fuselage metal."@en . "composite materials; primary aeroplane structure; aeroplane fuselage; aeroplane structure testing; NDT; certification"@en . "FT-TA3/153" . . . . . "composite materials" . " primary aeroplane structure" . . "2006-01-11+01:00"^^ .