发明授权
US6074509A High strength, lightweight pressurized structure for use as the skin of a spacecraft or other vehicle 失效
高强度轻质加压结构,用作航天器或其他车辆的皮肤

High strength, lightweight pressurized structure for use as the skin of
a spacecraft or other vehicle
摘要:
A sandwich skin construction that is comprised of an internal structure comprising a plurality of cones disposed between two outer skins is disclosed. The interior contains a pressurized gas to give the resulting sandwich skin construction added strength over a similarly constructed non-pressurized structure of the same material with an equivalent mass. Various attributes of the cones can be adjusted, for example, size and angle, to optimize the performance of the sandwich skin construction to a variety of external stresses. Moreover, a method is provided for manufacturing the sandwich skin construction. The structure can be placed in a pressurized environment before attaching the outer skins.
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