发明名称 FORWARD FUSELAGE (VERSIONS)
摘要 FIELD: aircraft engineering.SUBSTANCE: forward fuselage comprises control cabin with truncated cone-shape nose elongated forward and provided with plate secured to cone vertex and made from refractory material. It is located perpendicular or inclined to approach flow. Ring fitted by its rib on truncated cone base is made from refractory material and located perpendicular or inclined to approach flow. Ring rib features variable height.EFFECT: decreased aerodynamic heating of forward fuselage.3 cl, 8 dwg
申请公布号 RU2534489(C1) 申请公布日期 2014.11.27
申请号 RU20130146932 申请日期 2013.10.21
申请人 SHCHEPOCHKINA JULIJA ALEKSEEVNA 发明人 SHCHEPOCHKINA JULIJA ALEKSEEVNA
分类号 B64C1/38 主分类号 B64C1/38
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