发明名称 САМОЛЕТНЫЙ ПРИЦЕЛ
摘要 FIELD: weapons and ammunition. ^ SUBSTANCE: invention relates to sights and can be used incorporated with fighter-interceptors for close-in dogfighting. The proposed invention aims at reducing the in-flight view time in attacking air target. To this end, the aircraft sight circuit additionally incorporates a delay circuit, while the aerial mirror drive shifting the said mirror along the inclined line is furnished with the 3rd control input, commutator and 3rd threshold device. Note here the 3rd threshold device signal input is connected to the drive code-shaft transducer, while its output and the 2nd threshold device output are connected, via the commutator signal inputs, to power amplifier input. The commutator control input is connected to the 3rd control input of the drive. Note also that the said delay device in connected in between the drive 3rd control input and memory output. ^ EFFECT: reducing the in-flight view time in attacking air target. ^ 4 dwg
申请公布号 RU2007117334(A) 申请公布日期 2008.11.20
申请号 RU20070117334 申请日期 2007.05.10
申请人 Открытое акционерное общество "Корпораци  "Фазотрон-Научно-исследовательский институт радиостроени " (RU) 发明人 Гуськов Юрий Николаевич (RU);Бушуев Сергей Николаевич (RU);Корнев Геннадий Иванович (RU)
分类号 F41G3/22 主分类号 F41G3/22
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