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
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