发明名称 LAUNCHING SYSTEM AND INSTALLATION
摘要 FIELD: transport. ^ SUBSTANCE: invention relates to aircraft engineering, namely, to aircraft launching system and installation. Proposed launching system comprises aircraft, towing installation for launching. Launching installation comprises aircraft, mounted with the help of slings on wing body to allow arrangement of aircraft head section in upward direction with engine striated in air by consecutive cutting off of one and, then, all other slings. Method of launching consists in that aircraft takes off from launching installation mounted on its top or bottom surface. Launching installation detaches from aircraft after lifting to launching height. Aircraft detached from wing body, it is launched. Method of launching in compliance with second version consists in that launching installation is mounted in aircraft freight compartment. ^ EFFECT: simplified launching. ^ 16 cl, 13 dwg
申请公布号 RU2438940(C2) 申请公布日期 2012.01.10
申请号 RU20090149740 申请日期 2009.12.30
申请人 MITSUBISI KHEHVI INDASTRIZ, LTD. 发明人 KURODA JOSIKHATSU;KAVAMATA JOSIKHIRO;SINGO MIKA
分类号 B64C37/02;B64D5/00;B64G3/00;F41F3/00 主分类号 B64C37/02
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