发明名称 Metal aircraft structural member
摘要 <p>#CMT# #/CMT# Metal components for aircraft are made up of metal sheets (1, 2) connected by a butt joint. The edges of this are not straight, but have a periodically-repeating, interlocking shape. #CMT#USE : #/CMT# Metal components for aircraft, especially fuselage components. #CMT#ADVANTAGE : #/CMT# The components have improved tolerance to damage, especially spreading of fatigue cracking. #CMT#DESCRIPTION OF DRAWINGS : #/CMT# The drawing shows a perspective view of the joint in the component. 1, 2 : Metal sheets 5 : Weld bead 10 : Rib 11 : Central line of joint 14 : Axis of symmetry of joint #CMT#METALLURGY : #/CMT# Preferred features: The edges have a sinusoidal, sawtooth, labyrinthine, or trapezium-shape, or are made up of curved and straight sections. The thickness of the sheets increases towards the edges to be welded. The edge contour has a minimum amplitude (A) with respect to the center line of the joint of 5mm. The wavelength (lambda ) of the edge pattern is given by the relationship A/lambda = 0.1 - 2.The weld bead (5) has a breadth of 2 - 10mm.</p>
申请公布号 EP1902812(B1) 申请公布日期 2010.01.13
申请号 EP20070018361 申请日期 2007.09.19
申请人 FRAUNHOFER-GESELLSCHAFT ZUR FOERDERUNG DER ANGEWANDTEN FORSCHUNG E.V. 发明人 DIPL. -ING. DITTRICH, DIRK;DR.-ING HACKIUS, JENS;PROF. BRENNER, BERNDT;DR. RER. NAT. WINDERLICH, BERND;DR.-ING. STANDFUSS, JENS
分类号 B23K26/24;B23K26/28;B64C1/12 主分类号 B23K26/24
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