发明名称 FLEXBEAM TO ROTOR BLADE INTERFACE
摘要 A spar for a rotor blade assembly is provided including a generally hollow tubular body. A spacer protrudes from at least one surface of the body along a length of the body. A hole extends through the body and the spacer. The hole is configured to align with a through hole in an adjacent flexbeam assembly. The spacer is configured to contact a surface of the adjacent flexbeam assembly to create a match fit between the body and the flexbeam assembly.
申请公布号 EP2976259(A4) 申请公布日期 2016.12.14
申请号 EP20140798560 申请日期 2014.03.18
申请人 Sikorsky Aircraft Corporation 发明人 THOMAS, Justin;NUSSENBLATT, Eric Lucien;PARSONS, Eric S.;CASEY, Ryan Thomas;HUNTER, David H.
分类号 B64C27/33 主分类号 B64C27/33
代理机构 代理人
主权项
地址