"978-80-214-4358-7" . . "221961" . "Teardown analysis is an integral part of Damage Tolerance philosophy. The application of this philosophy for aircraft requires the determination of detectable flaw size, tolerated flaw size in term of residual strength, determining the periodicity of non-destructive inspection of principal structural elements. To determine these requirements is necessary to know a number of characteristics that are determined in the individual steps. These steps include the verification of nondestructive testing methods (Non-Destructive Testing, NDT). One aim of NDT is to determine the minimum detectable flaw size with 90% probability at 95% confidence level in the critical part and design procedures for the inspection of the airframe critical parts. To achieve this minimum detectable flaw size and probability, it is necessary to make so-called teardown analysis, which is the most accurate and reliable method of verifying the damages detected by the NDT method."@cs . "Postup Teardown anal\u00FDzy draku letounu"@cs . "Teardown anal\u00FDza je ned\u00EDlnou sou\u010D\u00E1st\u00ED filozofie Damage Tolerance. Aplikace t\u00E9to filozofie na letoun vy\u017Eaduje mimo jin\u00E9 stanoven\u00ED detekovateln\u00E9 velikosti po\u0161kozen\u00ED, p\u0159\u00EDpustn\u00E9 velikosti po\u0161kozen\u00ED z hlediska zbytkov\u00E9 pevnosti, stanoven\u00ED periodicity a zp\u016Fsobu nedestruktivn\u00EDch prohl\u00EDdek kritick\u00FDch m\u00EDst v konstrukci. Pro stanoven\u00ED t\u011Bchto po\u017Eadavk\u016F je nutn\u00E9 zn\u00E1t \u0159adu charakteristik, kter\u00E9 se stanovuj\u00ED v jednotliv\u00FDch d\u00EDl\u010D\u00EDch kroc\u00EDch. Mezi tyto jednotliv\u00E9 kroky pat\u0159\u00ED i verifikace nedestruktivn\u00EDch metod zkou\u0161en\u00ED (Non-Destructive Testing, NDT). Jedn\u00EDm z c\u00EDl\u016F NDT je stanoven\u00ED minim\u00E1ln\u00ED detekovateln\u00E9 d\u00E9lky (velikosti) po\u0161kozen\u00ED s 90% pravd\u011Bpodobnost\u00ED p\u0159i \u00FArovni spolehlivosti 95% v dan\u00E9m kritick\u00E9m m\u00EDst\u011B konstrukce a stanoven\u00ED metodik kontrol jednotliv\u00FDch kritick\u00FDch m\u00EDst draku letounu. Aby bylo t\u00E9to minim\u00E1ln\u00ED detekovateln\u00E9 d\u00E9lky a dan\u00E9 pravd\u011Bpodobnosti dosa\u017Eeno, je t\u0159eba prov\u00E9st tzv. Teardown anal\u00FDzu, kter\u00E1 je nejp\u0159esn\u011Bj\u0161\u00ED a nejspolehliv\u011Bj\u0161\u00ED metodou ov\u011B\u0159en\u00ED nalezen\u00FDch po\u0161kozen\u00ED danou NDT metodou."@en . . "Ostrava" . . . "2011-11-09+01:00"^^ . . "Postup Teardown anal\u00FDzy draku letounu" . "Postup Teardown anal\u00FDzy draku letounu"@cs . . . . . "Tiret" . . "Teardown analysis is an integral part of Damage Tolerance philosophy. The application of this philosophy for aircraft requires the determination of detectable flaw size, tolerated flaw size in term of residual strength, determining the periodicity of non-destructive inspection of principal structural elements. To determine these requirements is necessary to know a number of characteristics that are determined in the individual steps. These steps include the verification of nondestructive testing methods (Non-Destructive Testing, NDT). One aim of NDT is to determine the minimum detectable flaw size with 90% probability at 95% confidence level in the critical part and design procedures for the inspection of the airframe critical parts. To achieve this minimum detectable flaw size and probability, it is necessary to make so-called teardown analysis, which is the most accurate and reliable method of verifying the damages detected by the NDT method." . . . . "RIV/00010669:_____/11:#0001267!RIV12-MPO-00010669" . "Postup Teardown anal\u00FDzy draku letounu" . "RIV/00010669:_____/11:#0001267" . "I, P(FR-TI1/371)" . . "Teardown analysis procedures of airframe"@en . "NDE for Safety / Defektoskopie 2011" . "Boh\u00E1\u010Dov\u00E1, Marie" . . "6"^^ . "Teardown analysis; Damage Tolerance; Non-Destructive Testing; Probability of Detection; Confidence level"@en . . . "[9AE1825207DF]" . . "http://www.vzlu.cz/cz/transfer-vysledku/clanky-ve-sbornicich-d/" . "1"^^ . "Teardown analysis procedures of airframe"@en . . . "1"^^ .