发明名称 Perfectionnements relatifs aux moteurs et méthode de réduction des vibrations dans les dits moteurs
摘要 511,941. Fluid-pressure engines. UNITED AIRCRAFT CORPORATION. Dec. 22, 1937, No. 35483. Convention date, Aug. 14. [Class 122 (iii)] [Also in Group XXVII] Engines with groups of radial, multiple cylinders connected to cranks by master-rods and subsidiary link rods have the master rods and/or the cranks so arranged as to reduce vibrations due to harmonics of the torque variation. The groups are arranged so that their vibrations balance out or neutralize. In the arrangement shown in Fig. 3, the cylinders of each group are staggered with respect to the cylinders in the adjacent group. The cranks of the adjacent groups are arranged oppositely, with their master rods 22, 34 respectively as nearly as possible in coincidence. The harmonic components of the torque curves of the respective groups when added together result in a reduction of the exciting vibratory forces. In an arrangement such as shown in Fig. 2, the master rods may remain as shown, and one of the crankpins moved through 180 degrees to bring it into axial alignment with the other crank pin.
申请公布号 FR840744(A) 申请公布日期 1939.05.03
申请号 FRD840744 申请日期 1938.07.16
申请人 UNITED AIRCRAFT CORPORATION 发明人
分类号 F02B75/22;F16F15/24 主分类号 F02B75/22
代理机构 代理人
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