"The report summarizes the specifications of Aviation Regulations for UL 2, LTF-UL and CS-VLA. Load on engine mount in flight and emergency cases is solved according to these specifications. Force decomposition on the rod mount system was carried out using the finite element method. Based on this set of force effects strength analysis of individual parts of the engine mount were performed using analytical methods of calculation."@en . "Zat\u00ED\u017Een\u00ED a pevnostn\u00ED kontrola motorov\u00E9ho lo\u017Ee letounu UL-39" . "Zat\u00ED\u017Een\u00ED a pevnostn\u00ED kontrola motorov\u00E9ho lo\u017Ee letounu UL-39"@cs . . . "Helmich, Martin" . . . . . "1"^^ . . "Ve zpr\u00E1v\u011B byla shrnuta specifikace leteck\u00FDch p\u0159edpis\u016F UL 2, LTF-UL a CS-VLA, a dle nich \u0159e\u0161eno zat\u00ED\u017Een\u00ED motorov\u00E9ho lo\u017Ee v letov\u00FDch a havarijn\u00EDch p\u0159\u00EDpadech. Byl proveden silov\u00FD rozklad prutov\u00E9 soustavy lo\u017Ee, kter\u00FD byl realizov\u00E1n pomoc\u00ED metody kone\u010Dn\u00FDch prvk\u016F. Na z\u00E1klad\u011B takto stanoven\u00FDch silov\u00FDch \u00FA\u010Dink\u016F je provedena pevnostn\u00ED kontrola jednotliv\u00FDch \u010D\u00E1st\u00ED motorov\u00E9ho lo\u017Ee vyu\u017E\u00EDvaj\u00EDc\u00ED analytick\u00E9 postupy v\u00FDpo\u010Dtu." . "Engine mount; Load; Strength analysis"@en . . "Load and strength tests of the engine mount of the UL-39 aircraft"@en . "1"^^ . "RIV/68407700:21220/12:00201150!RIV13-MPO-21220___" . "[FD1E229800D2]" . "Zat\u00ED\u017Een\u00ED a pevnostn\u00ED kontrola motorov\u00E9ho lo\u017Ee letounu UL-39"@cs . "21220" . . . "P(FR-TI3/527)" . . "182057" . "Zat\u00ED\u017Een\u00ED a pevnostn\u00ED kontrola motorov\u00E9ho lo\u017Ee letounu UL-39" . "RIV/68407700:21220/12:00201150" . . "Ve zpr\u00E1v\u011B byla shrnuta specifikace leteck\u00FDch p\u0159edpis\u016F UL 2, LTF-UL a CS-VLA, a dle nich \u0159e\u0161eno zat\u00ED\u017Een\u00ED motorov\u00E9ho lo\u017Ee v letov\u00FDch a havarijn\u00EDch p\u0159\u00EDpadech. Byl proveden silov\u00FD rozklad prutov\u00E9 soustavy lo\u017Ee, kter\u00FD byl realizov\u00E1n pomoc\u00ED metody kone\u010Dn\u00FDch prvk\u016F. Na z\u00E1klad\u011B takto stanoven\u00FDch silov\u00FDch \u00FA\u010Dink\u016F je provedena pevnostn\u00ED kontrola jednotliv\u00FDch \u010D\u00E1st\u00ED motorov\u00E9ho lo\u017Ee vyu\u017E\u00EDvaj\u00EDc\u00ED analytick\u00E9 postupy v\u00FDpo\u010Dtu."@cs . "Load and strength tests of the engine mount of the UL-39 aircraft"@en . . . . .