发明名称 METHOD TO REDUCE LOADS AND VIBRATION IN AIRCRAFT WITH MULTI-BLADE SCREW PROPELLERS WITH EVEN NUMBER OF BLADES
摘要 FIELD: transport. ^ SUBSTANCE: invention relates to aircraft engineering, particularly, to air screws. Proposed method comprises irregular arrangement of blades, mounted impairs in symmetry about screw orthogonal axes, varying screw types, determining mathematical model of computing harmonic components of variable-load vectors for every blade depending upon angles between axes of adjacent pairs of blades ö¿1. It includes also summation of load vectors from every blade along three axes OY1, OX1, OZ1 of rotary system of coordinates with initial point at screw hub center, projecting obtained vectors onto fixed axes of aircraft coordinates OfXf and OfZf, performing harmonic analysis of projection of load vectors onto lengthwise OfXf and crosswise OfZf axes and constructing dependencies of amplitudes of said harmonic components upon angles ö¿1 and selection of designed angles corresponding to minimum level of variable load harmonics. ^ EFFECT: increased life. ^ 2 cl, 7 dwg
申请公布号 RU2385262(C1) 申请公布日期 2010.03.27
申请号 RU20080144838 申请日期 2008.11.14
申请人 FEDERAL'NOE GOSUDARSTVENNOE UNITARNOE PREDPRIJATIE "LETNO-ISSLEDOVATEL'SKIJ INSTITUT IMENI M.M. GROMOVA" 发明人 LOSEV VIKTOR SEMENOVICH;GOLUBTSOV SERAFIM ALEKSEEVICH;SHCHUKINA VALENTINA IVANOVNA
分类号 B64C11/04 主分类号 B64C11/04
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