发明名称 ULTRA LOW MASS AIRPLANE
摘要 FIELD: transportation. ^ SUBSTANCE: airplane contains fuselage where are affixed wing, tail strut-framed assembly, running gear and power unit. Fuselage contains flight deck made of composite material, allowing floatation properties and low conductivity. Flap operation for three positive positions: for 0 degrees, for 20 degrees and for 40 degrees. Running gear is made with separated wheels braking and self-oriented nose-wheel. Airplane is outfitted by systems of life-support, operating and communication. ^ EFFECT: providing of safety and comfortable flight. ^ 4 cl, 3 dwg
申请公布号 RU2336200(C2) 申请公布日期 2008.10.20
申请号 RU20050109329 申请日期 2005.04.01
申请人 OBSHCHESTVO S OGRANICHENNOJ OTVETSTVENNOST'JU "REHMZ-AVIA" 发明人 KLJUJKIN STANISLAV ANATOL'EVICH;BEKHTER JURIJ ANATOL'EVICH;BESSMERTNYJ VLADIMIR ALEKSANDROVICH;ZINCHENKO GRIGORIJ IVANOVICH
分类号 B64C31/00;B64C1/06 主分类号 B64C31/00
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