发明名称 Cellular sandwich structure for aircraft panels - has continuous structure of truncated pyramids sandwiched between skin layers, with similar cellular structure defining each skin layer
摘要 The sandwich structure is formed by a series of hollow truncated pyramids arranged so that their lateral faces transmit loading forces. The array of pyramids is located between a pair of skin layers (34,36), with the truncated surfaces adjacent to the inner surfaces of the skins. At least one of the skin layers is itself formed by a similar structure of truncated pyramids (37,42) enclosed between a pair of cladding layers (38,40). The base edges of the adjacent pyramids are contiguous, and the lateral faces of the pyramids may be perforated. USE/ADVANTAGE - Cellular sandwich structure for panels of aircraft or other vehicles. Improved load-bearing properties and dimensional stability with reduced weight.
申请公布号 FR2696679(A1) 申请公布日期 1994.04.15
申请号 FR19920012034 申请日期 1992.10.09
申请人 AEROSPATIALE STE NATIONALE INDLE 发明人 COLLARD DUDLEY
分类号 B32B3/12;B64C3/20;(IPC1-7):B32B3/12 主分类号 B32B3/12
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