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 |
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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