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 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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