发明名称 Roller gear for a drive system
摘要 A roller gear 600 for use in a roller gear and sprocket configuration of a drive system, particularly for use in a landing gear drive system of an aircraft, comprises a body 601 having a core 602. The body includes at least two roller mounting members 611,612 and an array of rollers 605. A further roller mounting member 613 may be included and the gear may then include a second array of rollers 606. Rollers 604,607 are mounted on pins 608 extending through openings in the roller mounting members. Bushes 615 may be included between roller and pin. A locking ring 609 may be included to lock pins 608 to a roller mounting member.
申请公布号 GB2524246(A) 申请公布日期 2015.09.23
申请号 GB20140004727 申请日期 2014.03.17
申请人 AIRBUS OPERATIONS LIMITED 发明人 ARNAUD DIDEY;RICHARD BILLYEALD;IAN DICKASON;JAMES SETTER
分类号 B64C25/40;F16H1/00;F16H55/00 主分类号 B64C25/40
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