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Propulsion of Photovoltaic Cruiser-Feeder Airships Dimensioning by Constructal Design for Efficiency Method

机译:用效率法设计光伏巡洋舰 - 馈线飞艇尺寸尺寸

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The European project MAAT (Multi-body Advanced Airship for Transport) is producing the design of a transportation system for transport of people and goods, based on the cruiser feeder concept. This project defined novel airship concepts capable of handling safer than in the past hydrogen as a buoyant gas. In particular, it has explored novel variable shape airship concepts, which presents also intrinsic energetic advantages. It has recently conduced to the definition of an innovative design method based on the constructal principle, which applies to large transport vehicles and allows performing an effective energetic optimization and an effective optimization for the specific mission. While the traditional constructal method performs an optimization with a down-to-top approach, it produces an optimization process in two stages: the first one defines the optimal characteristics of the system understood as a unitary system to achieve the desired performances; the second analyzes the subsystems, examining those most disadvantaged, in order to optimize its performance for the desired goal. It has been deeply tested on a traditional shaped airship allowing verifying that a changing volume airship has globally better energetic performances than a fixed volume one. This paper performs a preliminary analysis of the method for the design of a cruiser/feeder multibody airship such as the one, which is going to be designed inside the MAAT project. The model presented defines the guidelines for the optimization of the system considering the magnitudes involved in flight physics to achieve the goal of energetic self-sufficiency.
机译:欧洲项目玛拉特(多机身先进飞艇)正在制造基于巡洋舰饲养者概念的人员和货物运输运输系统的设计。该项目定义了能够处理更安全的小型飞艇概念,而不是过去的氢气作为浮动气体。特别是,它已经探索了新型可变形状的飞艇概念,这也存在本质的能量优势。它最近涉及基于构造原则的创新设计方法的定义,该方法适用于大型运输车辆,并允许对特定任务进行有效的能量优化和有效优化。虽然传统的构造方法以脚踏方法进行优化,但它在两个阶段产生优化过程:第一个定义系统的最佳特性被理解为整体系统以实现所需的性能;第二个分析子系统,检查最不利地位的那些,以优化其所需目标的性能。它对传统形状的飞艇进行了深刻的测试,允许验证变化的体积飞艇比固定的体积更好地具有高度充满活力的表演。本文对设计巡洋舰/饲养者/饲养者多体飞艇的方法进行了初步分析,如将设计在Maat项目内部。提出的模型定义了考虑到飞行物理学中所涉及的大小来实现能量自给自足的目标的制度指导方针。

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