发明名称 Rotor balancing arrangement for gas-turbine engine, has inward aligned strips provided in outer collar of rotor disk, and axial aligned retaining groove provided in strips for balancing bodies that engage in strips and stuck onto strips
摘要 <p>The arrangement has three balancing bodies (8) arranged in a circular axial aligned retaining groove (7) at an outer collar (3) of a rotor disk (2). Radially inward aligned strips (5) are provided in the collar, where the groove is provided in the strips for the balancing bodies, which engage in the strips and stuck onto the strips. The strips form partial areas of a flange (4) that radially runs on inner side of the collar. The groove has a radial inlet opening that includes an angle of more than 90 degrees and less than 180 degrees, where each body is formed from a cylindrical shaft.</p>
申请公布号 DE102008016329(A1) 申请公布日期 2009.10.01
申请号 DE20081016329 申请日期 2008.03.28
申请人 ROLLS-ROYCE DEUTSCHLAND LTD &amp, CO KG 发明人 KNIGHT, MARK;WIRTH, MORITZ
分类号 F16F15/28;F01D5/16 主分类号 F16F15/28
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