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Low cost composite fabrication methods applied to low observable structure

机译:适用于低可观察结构的低成本复合材料制造方法

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McDonnell Douglas Technologies Incorporated (MDTI) is focused on adapting state-of-the-art low cost composite fabrication techniques to high performance, low observable (LO) structure. With increasing emphasis on affordability, future radar cross section (RCS) goals may not be realizable due to the high costs typically associated with LO technology. Much of the cost associated with high performance LO structure is attributed to composite manufacturing techniques that require considerable touch labor and expensive, limited shelf life materials. Rigid foam and honeycomb, for example, require extensive machining to achieve desired final net shapes. The use of a mold-to-net-shape foam core eliminates expensive machining. This paper focuses on the building block approach MDTI used to demonstrate affordable material and process approaches for fabrication of a large LO structure. This approach consisted of simultaneous development of: 1) an MDTI mold-to-net-shape core material identified as thermoplastic syntactic foam (TPSF), and 2) resin film infusion (RFI) technology applied to LO materials and structural configurations. The demonstration article selected for this technology was an eight-foot-long leading edge. MDTI was successful with first time fabrication of the eight-foot-long leading edge because of the building block approach described herein. Developments from this program are applicable to current and future, manned and unmanned aircraft.
机译:McDonnell Douglas Technologies Incorporated(MDTI)致力于使最新的低成本复合材料制造技术适应高性能,低可观察性(LO)的结构。随着人们越来越重视负担能力,由于与LO技术相关的高昂成本,未来的雷达横截面(RCS)目标可能无法实现。与高性能LO结构相关的大部分成本都归因于复合制造技术,该技术需要大量的触摸劳动和昂贵的,有限的保质期材料。例如,硬质泡沫和蜂窝需要大量加工才能获得所需的最终网状形状。使用模制到最终形状的泡沫芯消除了昂贵的机加工。本文着重于MDTI的构建块方法,该方法用来演示用于制造大型LO结构的价格合理的材料和工艺方法。这种方法包括同时开发:1)被确定为热塑性复合泡沫(TPSF)的MDTI模制到网状芯材,以及2)适用于LO材料和结构配置的树脂薄膜灌注(RFI)技术。选择用于该技术的演示文章是一个八英尺长的前沿。由于本文所述的构造方法,MDTI在首次制造8英尺长的前缘时获得了成功。该计划的发展适用于当前和未来的有人和无人飞机。

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