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 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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