发明名称 FLYING VEHICLE RETRACTABLE LANDING GEAR
摘要 FIELD: aeronautical engineering. SUBSTANCE: landing gear has leg 2 with breaker strut 7, wheeled bogie 5 with shock absorber 9. Wheeled bogie is articulated to strut by means of lever 11. Landing gear is provided with bogie turning mechanism which consists of system of articulated bell cranks 12 and 13 and rods 3 and 14. Double-arm bell crank 13 is articulated on strut; one arm of bell crank 13 is connected with rod 3 and other arm is connected to bell crank 12 by means of rod 14. EFFECT: enhanced efficiency of retracting the landing gear in fuselage. 3 cl, 7 dwg
申请公布号 RU95103116(A) 申请公布日期 1996.12.20
申请号 RU19950103116 申请日期 1995.02.28
申请人 AKTSIONERNOE OBSHCHESTVO OTKRYTOGO TIPA "OKB SUKHOGO" 发明人 DUBOVSKIJ EH.A.;FOKIN V.B.
分类号 B64C25/10 主分类号 B64C25/10
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