. "The compressor was designed using GE Aviation internal programs and differs from the WE type by the number of stator vanes and by highly 3D-profiled airfoils. The essential change in the design compared to the M601 engine is an application of the blisk technology (bladed disks) that represents a disk integrated with blades."@en . "Hork\u00FD, Vojt\u011Bch" . . . "1st AK H80, 2st AK H80" . . . "Funk\u010Dn\u00ED vzorek prvn\u00EDch dvou stup\u0148\u016F axi\u00E1ln\u00EDho kompresoru maleho turb\u00EDnov\u00E9ho motoru"@cs . . "Funk\u010Dn\u00ED vzorek prvn\u00EDch dvou stup\u0148\u016F axi\u00E1ln\u00EDho kompresoru maleho turb\u00EDnov\u00E9ho motoru" . "Aerospace; Engine; combustion; compressor; thermodynamic"@en . "Izol\u00E1tor v\u00FDvojov\u00FDch d\u00EDl\u016F" . . "Funk\u010Dn\u00ED vzorek prvn\u00EDch dvou stup\u0148\u016F axi\u00E1ln\u00EDho kompresoru maleho turb\u00EDnov\u00E9ho motoru" . . . . "Two stages of the axial flow compressor of small turbine engine"@en . . . "Dob\u0159ichovsk\u00FD, Jan" . "RIV/27928845:_____/10:#0000002!RIV11-MPO-27928845" . "[6531DDE41F13]" . . "260045" . "V\u00FDsledn\u00FD funk\u010Dn\u00ED vzorek je pou\u017Eit jako kritick\u00E1 \u010D\u00E1st nov\u00E9ho motoru GE H80. GEAC je p\u0159\u00EDjemcem i u\u017Eivatelem v\u00FDsledku. GEAC uzav\u0159ela smlouvu o vyu\u017Eit\u00ED v\u00FDsledk\u016F v\u00FDzkumu a v\u00FDvoje 2010/FT-TA5/034 s Ministerstvem pr\u016Fmyslu a obchodu. I\u010C: 47609109, dne 8.6.2010" . "Koldus, Vlastislav" . . "4"^^ . "Motor GE H80, jeho\u017E sou\u010D\u00E1st\u00ED je v\u00FDsledn\u00FD optimalizovan\u00FD prvn\u00ED a druh\u00FD stupe\u0148 axi\u00E1ln\u00EDho kompresoru, bude uveden do prodeje teprve po dokon\u010Den\u00ED certifikace EASA, jej\u00ED\u017E dokon\u010Den\u00ED je pl\u00E1nov\u00E1no v prvn\u00ED polovin\u011B roku 2011" . "P\u0159i n\u00E1vrhu prvn\u00EDch dvou stup\u0148\u016F axi\u00E1ln\u00EDho kompresoru byla pou\u017Eita intern\u00ED technologie GE Aviation. V\u00FDsledn\u00FD produkt se li\u0161\u00ED od d\u0159\u00EDve pou\u017Eit\u00FDch typ\u016F v po\u010Dtu lopatek a d\u00E1le je cel\u00FD stupe\u0148 vytvo\u0159en z jednoho kusu materi\u00E1lu." . "RIV/27928845:_____/10:#0000002" . "Two stages of the axial flow compressor of small turbine engine"@en . "Konvalinka, Michael" . . . . . . "P\u0159i n\u00E1vrhu prvn\u00EDch dvou stup\u0148\u016F axi\u00E1ln\u00EDho kompresoru byla pou\u017Eita intern\u00ED technologie GE Aviation. V\u00FDsledn\u00FD produkt se li\u0161\u00ED od d\u0159\u00EDve pou\u017Eit\u00FDch typ\u016F v po\u010Dtu lopatek a d\u00E1le je cel\u00FD stupe\u0148 vytvo\u0159en z jednoho kusu materi\u00E1lu."@cs . "5"^^ . . "Funk\u010Dn\u00ED vzorek prvn\u00EDch dvou stup\u0148\u016F axi\u00E1ln\u00EDho kompresoru maleho turb\u00EDnov\u00E9ho motoru"@cs . "Neve\u010De\u0159al, Jarom\u00EDr" . "P(FT-TA5/034)" . . . . .