发明名称 |
METHOD OF ADJUSTING SUPERSONIC AIR INTAKE |
摘要 |
FIELD: transport. ^ SUBSTANCE: method of adjusting mouth area and position of compression shocks by simultaneous turn of the front adjustable panel and rear adjustable panel. Axis of said front panel rotation is aligned with interaction of first and second steps of one of arrow-shape wedge, not perpendicular incident flow. Axis of said rear panel rotation is located in zone of rear edge of rear adjustable panel and is directed subject to location of the point of intersection with front panel rotational axis. In turn of both said panels, their side edges displace relative to channel shaped side surfaces with making clearances there between. ^ EFFECT: improved gas dynamic characteristics, stealth properties. ^ 4 cl, 8 dwg |
申请公布号 |
RU2460892(C1) |
申请公布日期 |
2012.09.10 |
申请号 |
RU20110116972 |
申请日期 |
2011.04.29 |
申请人 |
OTKRYTOE AKTSIONERNOE OBSHCHESTVO "OKB SUKHOGO";OTKRYTOE AKTSIONERNOE OBSHCHESTVO "AVIATSIONNAJA KHOLDINGOVAJA KOMPANIJA "SUKHOJ" |
发明人 |
DAVIDENKO ALEKSANDR NIKOLAEVICH;STRELETS MIKHAIL JUR'EVICH;RUNISHEV VLADIMIR ALEKSANDROVICH;BIBIKOV SERGEJ JUR'EVICH;POLJAKOVA NATAL'JA BORISOVNA;ANDREEV ROMAN VIKTOROVICH;SMIRNOV ALEKSANDR ALEKSEEVICH;ASTASHKIN ALEKSEJ VLADIMIROVICH;SUTSKEVER ANATOLIJ ISAAKOVICH;KOSITSIN ALEKSANDR ANATOL'EVICH |
分类号 |
F02C7/042 |
主分类号 |
F02C7/042 |
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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