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首页> 外文期刊>SAE International Journal of Aerospace >Propulsion of Photovoltaic Cruiser-Feeder Airships Dimensioning by Constructal Design for Efficiency Method
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Propulsion of Photovoltaic Cruiser-Feeder Airships Dimensioning by Constructal Design for Efficiency Method

机译:通过效率法的结构设计来推进光伏巡洋舰-飞艇的尺寸确定

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摘要

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MAAT(用于运输的多体高级飞艇)正在根据巡洋舰支线客机的概念来设计用于人员和货物运输的运输系统。该项目定义了新颖的飞艇概念,能够比过去将氢作为浮力气体更安全地进行处理。特别是,它探索了新颖的可变形状飞艇概念,这也显示出内在的能量优势。最近,它有助于基于结构原理的创新设计方法的定义,该方法适用于大型运输车辆,并可以针对特定任务执行有效的能量优化和有效的优化。传统的构造方法采用自上而下的方法进行优化,但它产生了两个阶段的优化过程:第一个阶段定义了系统的最佳特性,该系统被理解为一个整体系统,以实现所需的性能;第二部分分析子系统,检查最不利的子系统,以优化其性能以实现期望的目标。它已经在传统形状的飞艇上进行了深入测试,从而可以验证变化体积的飞艇具有比固定体积的飞艇具有更好的能量表现。本文对巡洋舰/支线多体飞艇的设计方法进行了初步分析,该方法将在MAAT项目内部进行设计。提出的模型定义了系统优化的指导原则,其中考虑了飞行物理学中涉及的幅度以实现能量自给自足的目标。

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