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SUPPORT FOR A AIRCRAFT STRUCTURAL COMPONENT PRODUCED IN A SELECTIVE LASER MELTING METHOD, USE AND PRODUCTION METHOD
SUPPORT FOR A AIRCRAFT STRUCTURAL COMPONENT PRODUCED IN A SELECTIVE LASER MELTING METHOD, USE AND PRODUCTION METHOD
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机译:选择性激光熔化方法,用途和生产方法生产的飞机结构部件的支持
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摘要
The invention relates to an elongated supporting pillar for a high-strength structural component, wherein the supporting pillar is designed to absorb bending forces that act transversely to a longitudinal direction of extension of the supporting pillar. The supporting pillar comprises a wall which at least partially encloses an elongated cavity of the supporting pillar. A reinforcement structure is arranged within the cavity and transversely to the direction of longitudinal extension in such a manner that the reinforcement structure can absorb at least some of the bending forces. The reinforcement structure is designed integrally with the wall, wherein both the wall and the reinforcement structure comprise a meltable material.
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