A rotorcraft rotor blade (400) assembly includes a stub spar (402) extending less than a full span of the rotor blade assembly (400). An upper skin portion (404) extends substantially the full span of the rotor blade assembly (400). A lower skin portion (406) extends substantially the full span of the rotor blade assembly (400). The stub spar (402) is positioned between the upper skin portion (404) and the lower skin portion (406).
申请公布号
EP3115296(A1)
申请公布日期
2017.01.11
申请号
EP20160170417
申请日期
2016.05.19
申请人
Bell Helicopter Textron Inc.
发明人
Oldroyd, Paul K.;Sutton, Drew;Maresh, Andrew;Foskey, Christopher