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.