发明名称 AIRCRAFT FUSELAGE
摘要 FIELD: aircraft engineering.SUBSTANCE: aircraft fuselage comprises nose section with control cabin and front landing gear, mid section with wings attachment elements and tail section with jet engine with tail unit. Connecting link and lattice truss curved in arc is arranged between said mid and tail sections, lattice area being greater than jet engine suction nozzle. Said connecting link is composed of solid/hollow body component. Pipelines and electric cables are laid in connecting link to allow operation of jet engine and tail unit rotary elements.EFFECT: higher safety of aircraft.5 cl, 7 dwg
申请公布号 RU2544055(C1) 申请公布日期 2015.03.10
申请号 RU20130157605 申请日期 2013.12.24
申请人 SHCHEPOCHKINA JULIJA ALEKSEEVNA 发明人 SHCHEPOCHKINA JULIJA ALEKSEEVNA
分类号 B64D27/20;B60R19/52;B64D33/02;F02C7/055 主分类号 B64D27/20
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