发明名称 LIGHT SUPERSONIC MULTI-PURPOSE AIRCRAFT
摘要 FIELD: aeronautical engineering. ^ SUBSTANCE: proposed aircraft is provided with main power plant including supersonic engines, additional power plant located in lower section of fuselage behind crew cabin and integral complex of onboard radio electronic equipment , aircraft complex control system, shipboard equipment control system, aircraft complex power supply system, electronic display complex and self-contained onboard oxygen system. Proposed aircraft may be used under varying flight conditions including conditions of using autonomous home airfield in case of separation from main airfield. ^ EFFECT: enhanced efficiency. ^ 3 cl, 15 dwg
申请公布号 RU2271305(C1) 申请公布日期 2006.03.10
申请号 RU20040132176 申请日期 2004.11.05
申请人 发明人 DEMCHENKO OLEG FEDOROVICH;DOLZHENKOV NIKOLAJ NIKOLAEVICH;MATVEEV ANDREJ IVANOVICH;POPOVICH KONSTANTIN FEDOROVICH;GURTOVOJ ARKADIJ IOSIFOVICH;SHKOLIN VLADIMIR PETROVICH;KODOLA VALERIJ GRIGOR'EVICH
分类号 B64C13/00;B64C3/14 主分类号 B64C13/00
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