发明名称 AIRCRAFT ADJUSTABLE ELEMENT DRIVE
摘要 FIELD: transport.SUBSTANCE: invention relates to aircraft and space engineering, particularly, to airship drives. Aircraft adjustable element drive comprises backup component, variable-volume chamber and controlled pump communicated via control line with said chamber. Proposed drive includes additional adjustable valve arranged at control pipe. Backup component consists of tubular vase accommodating working element made of alloy with shape memory effect, hot gas feed source communicated with tubular case, lock and working element loading means. Working element one end is secured at airship airframe while opposite end is connected with working element loading means. Aforesaid lock is arranged between airship airframe and aforesaid loading means.EFFECT: higher reliability.3 cl, 2 dwg
申请公布号 RU2497719(C2) 申请公布日期 2013.11.10
申请号 RU20110144456 申请日期 2011.11.02
申请人 FEDERAL'NOE GOSUDARSTVENNOE BJUDZHETNOE OBRAZOVATEL'NOE UCHREZHDENIE VYSSHEGO PROFESSIONAL'NOGO OBRAZOVANIJA "MOSKOVSKIJ AVIATSIONNYJ INSTITUT (NATSIONAL'NYJ ISSLEDOVATEL'SKIJ UNIVERSITET)" (MAI) 发明人 MATVEENKO ALEKSANDR MAKAROVICH;FATKULLIN OLEG KHIKMETOVICH;KHALOV MURAT OSMANOVICH
分类号 B64C25/18;B64C13/24 主分类号 B64C25/18
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