发明名称 ROCKET-CARRIER ROCKET TAIL COMPARTMENT BOTTOM PROTECTION
摘要 FIELD: transport, space engineering. ^ SUBSTANCE: invention can be used for protection of rocket-carrier against gasdynamic effects of working engine jets. Proposed protection, according to this invention, contains the mobile ring screen with the spherical surface, fitted on the rotary combustion chamber of the carrier engine, the motionless screen and a slot-like gap between the said screens. Note here that the motionless screen represents an end face spherical surface of the tail compartment casing, formed by the radius from the centre of rotation of a rotary part of the engine. The mobile ring screen overlaps the motionless screen over its spherical surface. The said slot-like gap is located in the zone of overlapping of said spherical surfaces of screens to allow changing the direction of gas flows affecting the aforesaid compartment. ^ EFFECT: decreased weight of bottom protection, higher reliability and efficiency. ^ 2 dwg
申请公布号 RU2347725(C2) 申请公布日期 2009.02.27
申请号 RU20060140931 申请日期 2006.11.20
申请人 FEDERAL'NOE GOSUDARSTVENNOE UNITARNOE PREDPRIJATIE GOSUDARSTVENNYJ NAUCHNO-PROIZVODSTVENNYJ RAKETNO-KOSMICHESKIJ TSENTR "TSSKB-PROGRESS" (FGUP GNPRKTS "TSSKB-PROGRESS") 发明人 BOGDANOV SERGEJ DMITRIEVICH;CHIKALOV VIKTOR GRIGOR'EVICH;ANSHAKOV GENNADIJ FEDOROVICH
分类号 B64G1/52;B64G1/40 主分类号 B64G1/52
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