<Record><identifier xmlns="http://purl.org/dc/elements/1.1/">URN:NBN:SI:doc-ECXEL153</identifier><date>1940</date><relation>documents/doc/E/URN_NBN_SI_doc-ECXEL153_001.pdf</relation><relation>documents/doc/E/URN_NBN_SI_doc-ECXEL153_001.txt</relation><relation>documents/doc/E/URN_NBN_SI_doc-ECXEL153_001.xml</relation><format format_type="main">4 strani</format><identifier identifier_type="COBISSID">32986883</identifier><identifier identifier_type="URN">URN:NBN:SI:doc-ECXEL153</identifier><language>slv</language><publisher>Uprava za zaštitu industriske svojine</publisher><source>Zrakoplovstvo</source><rights>PDM</rights><scans>id-32986883_112_scn-001.jp2</scans><scans>id-32986883_112_scn-002.jp2</scans><scans>id-32986883_112_scn-003.jp2</scans><scans>id-32986883_112_scn-004.jp2</scans><title>Metoda nevtraliziranja aerodinamičnega tlaka, ki deluje na površino strelnega orožja,
montiranega na krovu aeroplanov, in naprave za dosego te metode</title><title>patentni spis št. 16351</title><title>Razred 77a (Oddelek 4)</title></Record>