发明名称 METHOD AND APPARATUS FOR REDUCING HIGH TRANSIENT MOUNT LOAD IN AIRCRAFT ENGINE MOUNTING SYSTEMS
摘要 Exemplary embodiments are provided to reduce the high transient mount load in an aircraft engine mounting system under extreme loading condition. The exemplary embodiments reduce the impact of the snubbing phenomenon without adding to the weight or space claim of the engine mounting system.
申请公布号 US2016009403(A1) 申请公布日期 2016.01.14
申请号 US201414327627 申请日期 2014.07.10
申请人 HONEYWELL INTERNATIONAL INC. 发明人 Kumar Avinash;Brockett Theodore;Chinthapally Srinivas;Kumbham Krishna Mohan;Khare Milind;Ganji Venkatarao;Kandula Rama Sateesh Venkata
分类号 B64D27/26;F02C7/20 主分类号 B64D27/26
代理机构 代理人
主权项 1. An apparatus for reducing the high transient mount load from an aircraft engine, the apparatus of the type including a housing with a sleeve for receiving a yoke pin, the apparatus comprising: a first wall having a first ovalized opening; and a second wall opposite the first wall, having a second ovalized opening; wherein the first ovalized opening and the second ovalized opening are for receiving the yoke pin therethrough.
地址 Morristown NJ US