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Blending modern multifunctional materials with traditional structures: An approach for a greener and cleaner future

机译:用传统结构混合现代多功能材料:一种绿色和更清洁的未来的方法

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The objective of the project is to propose a multifunctional composite material system for next generation rotorcraft's structural components. In particular, a hybrid composite termed as Piezo-Battery Fiber Reinforced Composite (P-BFRC) comprising of piezoelectric and battery fibers is proposed for the rotorcraft blades, which are arranged in an appropriate optimized fashion. The optimized layout will depend on the characteristic of vibrations in the rotor blades and associated structural components. For the fuselage skin panels, use of Battery Fiber Reinforced Composite (BFRC) is proposed. In the rotor blades and the regions where vibration amplitudes are larger, the P-BFRC structure aims to extract electrical energy from the structural vibrations using the piezoelectric panels and store it within the battery panels embedded in the structure itself. In the fuselage, the battery composite skin panels, upon charging from ground station, can serve as power source for operation for several rotorcraft's electrical and electronic components. Importantly, the proposed multifunctional structure is optimized such that the structural characteristics of the existing rotorcraft is not compromised, while simultaneously performing its multiple functions. In other words, introducing such multifunctional material does not increase overall weight nor reduce the structural load carrying capability. In addition, the proposed material system intend to make minimal modifications in the existing system as far as structure and power management systems are concerned, thereby a re-design of entire structural/power system is not necessary. Preliminary analyses have been conducted for to study the energy harvesting and storage characteristics of the multifunctional structure. This work focuses on detailed quantification of energy harvesting and storage capabilities of the proposed multifunctional system through appropriate electro-mechanical models. Altogether, the multifunctional structural system is found to be a promising step towards a cleaner and sustainable aviation.
机译:该项目的目的是为下一代旋翼飞行器的结构部件提出多功能复合材料系统。特别地,提出了一种称为包含压电和电池纤维的压电和电池纤维的压电纤维增强复合材料(P-BFRC)的混合复合材料,其以适当的优化方式布置。优化的布局将取决于转子叶片和相关的结构部件中的振动的特性。对于机身皮板,提出了使用电池纤维增强复合材料(BFRC)。在转子叶片和振动幅度较大的区域中,P-BFRC结构旨在使用压电板从结构振动中提取电能,并将其存储在嵌入结构本身的电池板内。在机身中,电池复合皮肤面板在从地面电站充电时可以用作用于多个旋翼电气和电子元件的操作的电源。重要的是,所提出的多功能结构被优化,使得现有旋翼飞机的结构特性不会受到损害,同时执行其多个功能。换句话说,引入这种多功能材料不会增加总体重量,也不会降低结构承载能力。此外,就结构和电源管理系统而言,所提出的材料系统打算在现有系统中进行最小的修改,从而不需要重新设计整个结构/电力系统。已经进行了初步分析,用于研究多功能结构的能量收集和储存特性。这项工作侧重于通过适当的机电模型进行详细量化所提出的多功能系统的能量收集和储存能力。完全,多功能结构系统被发现是迈向清洁和可持续航空的有希望的一步。

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