A Preliminary Technology Readiness Assessment of Morphing Technology Applied to Case Studies

Author:

Miceli Marco Fabio1,Ameduri Salvatore2,Dimino Ignazio2ORCID,Pecora Rosario3ORCID,Concilio Antonio2ORCID

Affiliation:

1. ALI—Aerospace Laboratory for Innovative components, 80146 Napoli, Italy

2. Department of Adaptive Structures, The Italian Aerospace Research Centre (CIRA), 81043 Capua, Italy

3. Department of Industrial Engineering, University of Naples “Federico II”, 80125 Napoli, Italy

Abstract

In an innovative system, it is essential to keep under control the crucial development phases, which should consider several aspects involving, for instance, the modeling or the assessment of suitable analytical representations. Aiming to pursue a final demonstration to verify the actual capability of an engineering idea, however, some fundamental elements may have been partially considered. Many projects state the initial and final technology readiness level based on the famous scale introduced by the US National and Aeronautics Space Administration (NASA) many years ago and now widespread in many fields of technology innovation. Its nine-step definition provides a high-level indication of the maturity of the observed innovative system. Trivially, the resolution of that macroscopic meter is not made for catching advancement details, but it rather provides comprehensive information on the examined technology. It is, therefore, necessary to refer to more sophisticated analysis tools that can show a more accurate picture of the development stage and helps designers to highlight points that deserve further attention and deeper analysis. The risk is to perform a very good demonstration test that can miss generality and remain confined only to that specific experimental campaign. Moving on to these assumptions, the authors expose three realizations of theirs concerning aeronautic morphing systems, to the analysis of a well-assessed Technology Readiness Level instrument. The aim is to define the aspects to be further assessed, the aspect to be considered fully mature, and even aspects that could miss some elementary point to attain full maturation. Such studies are not so frequent in the literature, and the authors believe to give a valuable, yet preliminary, contribution to the engineering of breakthrough systems. Without losing generality, the paper refers to the 2.2 version of a tool set up by the US Air Force Research Laboratory (AFRL), and NASA, with the aim to standardize the evaluation process of the mentioned nine-step TRL.

Publisher

MDPI AG

Subject

Molecular Medicine,Biomedical Engineering,Biochemistry,Biomaterials,Bioengineering,Biotechnology

Reference49 articles.

1. Kennet, L. (2003). Military Aviation, Government Printing Office: Air University Press. Reprint of the Clement Ader’s work, L’Aviation Militaire; Levrault: Paris, France, 1909.

2. Holle, A.A. (1917). Plane and the like for Aeroplanes. (N.1225711), U.S. Patent.

3. Parker, H.F. (1920). The Parker Variable Camber Wing, NACA Technical Report 77.

4. Hardy, R. (1983, January 23–24). AFTI/F-111 mission adaptive wing technology demonstration program. Proceedings of the 1983 AIAA Aircraft Prototype and Technology Demonstrator Symposium, Air Force Museum, Dayton, OH, USA.

5. Bonnema, K.L. (1988). AFTI/F-111 Mission Adaptive Wing Briefing to Industry. Air Force Wright Aeronautical Laboratories, Air Force Systems Command, Wright-Patterson Air Force Base, Defense Technical Information Center. AFWAL Technical Report TR-88-3082, ADA202467.

Cited by 2 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

同舟云学术

1.学者识别学者识别

2.学术分析学术分析

3.人才评估人才评估

"同舟云学术"是以全球学者为主线,采集、加工和组织学术论文而形成的新型学术文献查询和分析系统,可以对全球学者进行文献检索和人才价值评估。用户可以通过关注某些学科领域的顶尖人物而持续追踪该领域的学科进展和研究前沿。经过近期的数据扩容,当前同舟云学术共收录了国内外主流学术期刊6万余种,收集的期刊论文及会议论文总量共计约1.5亿篇,并以每天添加12000余篇中外论文的速度递增。我们也可以为用户提供个性化、定制化的学者数据。欢迎来电咨询!咨询电话:010-8811{复制后删除}0370

www.globalauthorid.com

TOP

Copyright © 2019-2024 北京同舟云网络信息技术有限公司
京公网安备11010802033243号  京ICP备18003416号-3