发明名称 ROTORCRAFT FLIGHT STRUCTURE
摘要 The invention relates to the field of helicopter construction. A rotorcraft flight structure of the helicopter contains an additional device for increase the helicopter lift executed in the form of flat set of sections of wings or guiding blades located radially, which is located under the blades of rotor and attached on the housing of helicopter by supports. For prevention from engagement of the tips of blades of rotor with the wings or guides of blade at starting, the latter are equipped on external ends with a ring, which comes out upward above them. The components of the rotorcraft flight structure are made from light durable material, and the support are tubular or flat, placing them by their plane in the direction of the motion of helicopter. For increase of the plane of wings they are made in the form of sheared sectors.
申请公布号 UA76882(C2) 申请公布日期 2006.09.15
申请号 UA20041210394 申请日期 2004.12.17
申请人 "VODA" PRODUCTION TECHNOLOGICAL COMPANY", MUNICIPAL COMPANY 发明人 CHORNYI ANATOLII PETROVYCH;PETROSOV VALERII ALBERTOVYCH;HONCHARUK VOLODYMYR STEPANOVYCH;CAZACHEVICI ANDREI VEACESLAV
分类号 B64C27/00;B64C27/32;B64C29/00 主分类号 B64C27/00
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