发明名称 APPLICATION OF HEAT TRAP
摘要 FIELD: engines and pumps.SUBSTANCE: invention relates to countermeasures against guided missiles including the application of heat trap. Proposed method is based on detection of guided missile with thermal homing head. It consists in determination of aircraft current speed for adjustment of thrust and actuation of heat trap jet engine. Blow-out charge is fired along with heat trap thermal substance, heat trap is ejected and its flight is stabilised in required direction. Then, heat trap jet engine is switched on to drive the trap by engine thrust at required speed.EFFECT: increased range of heat trap flight.2 dwg
申请公布号 RU2519573(C2) 申请公布日期 2014.06.20
申请号 RU20120113748 申请日期 2012.04.06
申请人 FEDERAL'NOE GOSUDARSTVENNOE VOENNOE OBRAZOVATEL'NOE UCHREZHDENIE VYSSHEGO PROFESSIONAL'NOGO OBRAZOVANIJA "VOENNYJ AVIATSIONNYJ INZHENERNYJ UNIVERSITET" (G. VORONEZH) MINISTERSTVA OBORONY ROSSIJSKOJ FEDERATSII 发明人 KOZIRATSKIJ JURIJ LEONT'EVICH;KULESHOV PAVEL EVGEN'EVICH;PROKHOROV DMITRIJ VLADIMIROVICH;PLEVE VIKTOR VJACHESLAVOVICH;OSTROVSKIJ DMITRIJ BORISOVICH
分类号 F42B5/15;F41H11/02;F41H11/04;F42B12/70 主分类号 F42B5/15
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