KENTSEL HAVA TAŞIMACILIĞINDA KULLANILACAK DİKEY İNİŞ-KALKIŞ KABİLİYETİNE SAHİP BİR HAVA ARACININ KAVRAMSAL TASARIMI VE MENZİL HESABI

Year 2022, Volume: 10 Issue: 3, 649 - 664, 01.09.2022

Tolunay Dağ , Tarık Ünler , Engin Hasan Çopur , Uğur Çakın

https://doi.org/10.36306/konjes.1090492

Abstract

Son zamanlarda meydana gelen trafik yoğunluğu ve ulaşım ihtiyacı nedeniyle kentsel hava taşımacılığına ilgi giderek artmaktadır. Birçok firma kentsel hava taşımacılığında kullanılmak üzere araçlar tasarlayarak bu sektöre yön vermek istemektedir. Buna bağlı olarak şehirlerde, hava taksiler ve uçan araç konsept fikirleri yaygınlaşmaktadır. Hem kişisel hem de kamu alanlarında kullanımı yaygınlaşacak olan bu hava araçlarının elektrikli motorlar ile çalışarak karbon salınımını en alt seviyelere taşıması düşünülmektedir. Bu çalışmada şehir içinde yaygın şekilde kullanıma sunulabilecek bir hava aracının tasarımı ve ulaşabileceği maksimum menzil değerinde iyileştirmeler gerçekleştirilmiştir. Tasarlanan araç, şehir içinde hem kargo hem de sağlık alanında güvenli ulaşım olanağı sağlayabilmektedir. Aracın yaklaşık 45 km menzili ve 30 dakika havada kalma süresine sahip olduğu belirlenmiştir. Bu değerler orta ölçekli bir şehirde taşımacılık yapılabilmesi için uygundur.

Keywords

Dikey iniş-kalkış, Elektrikli motor, Menzil, Şehir içi hava taşımacılığı, Taşıma+seyir konsept

Supporting Institution

Türk Havacılık ve Uzay Sanayii AŞ ve TÜBİTAK

Thanks

TÜBİTAK 2209-B Üniversite Öğrencileri Sanayiye Yönelik Araştırma Projeleri Desteği projesi ve TUSAŞ Lift Up programı kapsamında yürütülen bu projede desteklerinden ötürü Türkiye Bilimsel ve Teknolojik Araştırma kurumuna ve Türk Havacılık ve Uzay Sanayii AŞ’ye minnettarız.

Conceptual Design and Range Calculation of a Vertical Landing-Takeoff Aircraft to be Used in Urban Air Mobility

Abstract

Due to the recent traffic density and the need for transportation, interest in urban air mobility is increasing. Many companies want to direct this sector by designing vehicles to be used in urban air mobility. Accordingly, air taxis and flying vehicle concept ideas are becoming widespread in cities. It is thought that these vehicle, which will be used in both personal and public areas, will work with electric motors to bring carbon emissions to the lowest levels. In this study, improvements have been made in the design of an aircraft that can be used widely in the city and in the maximum range it can reach. The designed vehicle can provide safe transportation in the city, both in the field of cargo and health. It has been determined that the vehicle has a range of approximately 45 km and an endurance of 30 minutes. These values are suitable for transportation in a medium-sized city.

Keywords

Vertical take-off and landing, Electric motor, Range, Urban air mobility, Lift+cruise concept

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