Design and manufacture of nacelles for small turboprop aircraft

Author:

Dudziak Jacek1,Guła Paweł1,Gawlik Arkadiusz1,Kondracki Jerzy1

Affiliation:

1. Institute of Aviation, Center of New Technologies, Warsaw, Poland

Abstract

The aim of this paper is to present the results of prepreg nacelles design and manufacturing for I-31T aircraft. The work was part of the European Union project ‘Efficient Systems and Propulsion for Small Aircraft’ (ESPOSA). The new engine cowling design was preceded by computational fluid dynamics numerical analyses stage. Use of TP100 engine was assumed, which was installed on the I-31T aircraft in the framework of the ESPOSA project. This article presents the process of external geometry adjustment, chosen results of numerical analyses, 3D model design, manufacturing process and tests results. The new cowlings underwent ground and in-flight tests. Monitoring during the test included external and internal cowling temperatures. The collected test data were further analysed. Throughout accumulated energy in hot parts of the engine the temperature inside the engine nacelles rises. ‘Hot’ composite nacelles were used in order to withstand the impact of high temperature. In majority of modern aircraft propulsion systems, cowlings are made of composite. Currently, there is a trend to manufacture initially solution treated materials – i.e. glass and carbon fiber pre-pregs in out-of-autoclave process. Such an approach allows to accelerate the fabric layup process and achieve highly repeatable structure. Materials that are currently available in the market allow to manufacture the cowlings and simultaneous weight minimization. Owing to the applied 3D software for both design and manufacture of machining tools, it is possible to shorten the time of manufacturing a complete element. The cowlings were designed in cooperation with the NLR – Netherlands Aerospace Centre, who was a partner in the ESPOSA project and has experience in prepreg elements design. NLR was responsible for material selection and final part manufacturing. Tooling has been designed and manufactured in the Institute of Aviation in Warsaw. The assembly works were carried out by Zakłady lotnicze Margański & Mysłowski.

Publisher

SAGE Publications

Subject

Mechanical Engineering,Aerospace Engineering

Cited by 7 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