量子微型推进器的设计模型

Design Model of the Quantum Micro-Propulsion

在航空航天领域飞行器的微型化进程中,各种推进器必须携带燃料,这增加了系统的复杂性．有效提取真空中的“零点能”并以此作为驱动能源,可以消除长期以来微型飞行器须携带燃料的问题．从理论上阐述了真空“零点能”及Casimir力,对真空中的两平行平板结构和矩形腔等结构内的Casimir力、真空“零点能”进行了研究,得到不同边界下力随距离的变化规律,提出以Casimir力作为驱动力的量子微型推进系统设计模型,利用该模型可有效地提取真空零点能．

During the course of the miniation of future aircraft, many of the mirco-propulsions have to carry fuels and this makes the system complex. Extracting the zero-point energy effectively and making it be impetus of micro aircraft is of great importance for the aviation industry. It helps the micro aircraft work not having to carry fuels and reduces the weight of the aircraft greatly. Theories of zero-point energy coupling with the Casimir force are demonstrated. The Casimir force between the conductive parallel plates and the force in the rectangular cavities are presented in this paper. As a result, the transformation law between force and seperation boundaries is obtained. The design and characterization mode of the quantum micro-propulsion driven by Casimir force is also given and with which one can extract the zero-point energy effectively.