发明名称 GYROPLANE TAKE-OFF METHOD
摘要 FIELD: flight vehicles. ^ SUBSTANCE: gyroplane take-off method include a maximum driving up the lift rotor by the running power plant with the minimum angle of total pitch to rpm exceeding the flight magnitude, cutting of the lift rotor, increasing the thrust to the maximum and take-off run on the surface. Here, the lift rotor is kept neutral or at a negative angle to the flow, the total pitch of the rotor blades has a minimum magnitude. Unsticking is effected on reaching the required speed by increasing the total pitch the lift rotor to the flight magnitude or to that exceeding the above by a safe difference. ^ EFFECT: higher safety of take-off, higher power efficiency of gyroplane. ^ 4 dwg
申请公布号 RU2327603(C1) 申请公布日期 2008.06.27
申请号 RU20060136311 申请日期 2006.10.13
申请人 OTKRYTOE AKTSIONERNOE OBSHCHESTVO "NAUCHNO-PROIZVODSTVENNAJA KORPORATSIJA "IRKUT" (OAO "KORPORATSIJA "IRKUT") 发明人 KALMYKOV ALEKSEJ ALEKSANDROVICH;BARSUK VLADIMIR EVGEN'EVICH;TATARNIKOV ANDREJ PAVLOVICH;MOROZOV MAKSIM VENIAMINOVICH;RANTSAN JANIS JANISOVICH
分类号 B64C27/02 主分类号 B64C27/02
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