<p>A laminated composite stringer having a termination at one end in its longitudinal direction, and including a laminated stack of composite structural plies, wherein internal plies in the stack are terminated consecutively towards the stringer termination to provide a taper of reducing stack thickness. Also, a composite structure comprising a panel and the stringer; and a method of manufacturing the stringer. The composite structure may be used in aircraft.</p>
申请公布号
WO2011003844(A3)
申请公布日期
2011.06.30
申请号
WO2010EP59521
申请日期
2010.07.05
申请人
AIRBUS OPERATIONS LIMITED;AIRBUS OPERATIONS GMBH;BORGHINI-LILLI, MATTEO;HADLEY, PAUL;PHILLIPS, NATHAN