| 发明名称 |
HYPERSONIC AIRCRAFT WING IN AERODYNAMIC HEATING CONDITIONS |
| 摘要 |
FIELD: transport. ^ SUBSTANCE: invention relates to space and aircraft engineering. Proposed wing comprises element arranged inside it to take up heat emitted by wing skin heated inner surface and divert it to wing sections less heated. Aforesaid element is made from electrically conducting material. It is arranged inside wing and connected via self-contained onboard power supply with wing skin. ^ EFFECT: higher structural reliability. ^ 5 cl, 1 dwg |
| 申请公布号 |
RU2430857(C2) |
申请公布日期 |
2011.10.10 |
| 申请号 |
RU20090144640 |
申请日期 |
2009.12.01 |
| 申请人 |
GOSUDARSTVENNOE OBRAZOVATEL'NOE UCHREZHDENIE VYSSHEGO PROFESSIONAL'NOGO OBRAZOVANIJA BALTIJSKIJ GOSUDARSTVENNYJ TEKHNICHESKIJ UNIVERSITET "VOENMEKH" IM. D.F. USTINOVA (BGTU "VOENMEKH") |
发明人 |
KERNOZHITSKIJ VLADIMIR ANDREEVICH;KOLYCHEV ALEKSEJ VASIL'EVICH;OKHOCHINSKIJ DMITRIJ MIKHAJLOVICH |
| 分类号 |
B64C1/38 |
主分类号 |
B64C1/38 |
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