Evaluation of critical parameters in the design of a trainer aircraft landing gear

Burhan Cetinkaya; Ibrahim Ozkol

doi:10.1109/ICMAE.2017.8038678

Evaluation of critical parameters in the design of a trainer aircraft landing gear

Burhan Cetinkaya
, Ibrahim Ozkol

Uçak Mühendisliği Bölümü

Istanbul Technical University

Araştırma sonucu: Kitap/Rapor/Konferans Bildirisinde Bölüm › Konferans katkısı › bilirkişi

4 Atıf (Scopus)

Özet

In this study, the ways of analysis to evaluate best-fit landing gears for an aircraft considered is explicitly conducted. The configurations are designed then analyzed in order to obtained optimum landing gears designed. The dynamic equations of the wheelbase and wheel track which described the aircraft can be laterally stabilized on the ground are given. The dimensioning of the shock absorbers which are the basic components of the landing gears and stroke, the dimensions and pressure of landing gear wheels are obtained. Landing gear components and links are exposed important loads during the touch-down. These external and internal loads are applied to the models. Under the effect of these loads the structural behavior of the landing gear components are analyzed.

Orijinal dil	İngilizce
Ana bilgisayar yayını başlığı	2017 8th International Conference on Mechanical and Aerospace Engineering, ICMAE 2017
Yayınlayan	Institute of Electrical and Electronics Engineers Inc.
Sayfalar	391-394
Sayfa sayısı	4
ISBN (Elektronik)	9781538633052
DOI'lar	https://doi.org/10.1109/ICMAE.2017.8038678
Yayın durumu	Yayınlandı - 14 Eyl 2017
Etkinlik	8th International Conference on Mechanical and Aerospace Engineering, ICMAE 2017 - Prague, Czech Republic Süre: 22 Tem 2017 → 25 Tem 2017

Yayın serisi

Adı	2017 8th International Conference on Mechanical and Aerospace Engineering, ICMAE 2017

???event.eventtypes.event.conference???

???event.eventtypes.event.conference???	8th International Conference on Mechanical and Aerospace Engineering, ICMAE 2017
Ülke/Bölge	Czech Republic
Şehir	Prague
Periyot	22/07/17 → 25/07/17

Bibliyografik not

Publisher Copyright:
© 2017 IEEE.

BM SKH

Bu sonuç, aşağıdaki Sürdürülebilir Kalkınma Hedefine/Hedeflerine katkıda bulunur

SKH 3 Sağlık ve Kaliteli Yaşam

Belgeye Erişim

10.1109/ICMAE.2017.8038678

Diğer Dosyalar ve Linkler

Link to publication in Scopus

Alıntı Yap

Cetinkaya, B., & Ozkol, I. (2017). Evaluation of critical parameters in the design of a trainer aircraft landing gear. In 2017 8th International Conference on Mechanical and Aerospace Engineering, ICMAE 2017 (pp. 391-394). Makale 8038678 (2017 8th International Conference on Mechanical and Aerospace Engineering, ICMAE 2017). Institute of Electrical and Electronics Engineers Inc.. https://doi.org/10.1109/ICMAE.2017.8038678

Cetinkaya, Burhan ; Ozkol, Ibrahim. / Evaluation of critical parameters in the design of a trainer aircraft landing gear. 2017 8th International Conference on Mechanical and Aerospace Engineering, ICMAE 2017. Institute of Electrical and Electronics Engineers Inc., 2017. pp. 391-394 (2017 8th International Conference on Mechanical and Aerospace Engineering, ICMAE 2017).

@inproceedings{42b7565f54294baa941689c3067736b7,

title = "Evaluation of critical parameters in the design of a trainer aircraft landing gear",

abstract = "In this study, the ways of analysis to evaluate best-fit landing gears for an aircraft considered is explicitly conducted. The configurations are designed then analyzed in order to obtained optimum landing gears designed. The dynamic equations of the wheelbase and wheel track which described the aircraft can be laterally stabilized on the ground are given. The dimensioning of the shock absorbers which are the basic components of the landing gears and stroke, the dimensions and pressure of landing gear wheels are obtained. Landing gear components and links are exposed important loads during the touch-down. These external and internal loads are applied to the models. Under the effect of these loads the structural behavior of the landing gear components are analyzed.",

keywords = "analyze, design, landing gear, landing loads, main landing gear, nose landing gear",

author = "Burhan Cetinkaya and Ibrahim Ozkol",

note = "Publisher Copyright: {\textcopyright} 2017 IEEE.; 8th International Conference on Mechanical and Aerospace Engineering, ICMAE 2017 ; Conference date: 22-07-2017 Through 25-07-2017",

year = "2017",

month = sep,

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doi = "10.1109/ICMAE.2017.8038678",

language = "English",

series = "2017 8th International Conference on Mechanical and Aerospace Engineering, ICMAE 2017",

publisher = "Institute of Electrical and Electronics Engineers Inc.",

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booktitle = "2017 8th International Conference on Mechanical and Aerospace Engineering, ICMAE 2017",

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Cetinkaya, B & Ozkol, I 2017, Evaluation of critical parameters in the design of a trainer aircraft landing gear. in 2017 8th International Conference on Mechanical and Aerospace Engineering, ICMAE 2017., 8038678, 2017 8th International Conference on Mechanical and Aerospace Engineering, ICMAE 2017, Institute of Electrical and Electronics Engineers Inc., pp. 391-394, 8th International Conference on Mechanical and Aerospace Engineering, ICMAE 2017, Prague, Czech Republic, 22/07/17. https://doi.org/10.1109/ICMAE.2017.8038678

Evaluation of critical parameters in the design of a trainer aircraft landing gear. / Cetinkaya, Burhan; Ozkol, Ibrahim.
2017 8th International Conference on Mechanical and Aerospace Engineering, ICMAE 2017. Institute of Electrical and Electronics Engineers Inc., 2017. p. 391-394 8038678 (2017 8th International Conference on Mechanical and Aerospace Engineering, ICMAE 2017).

Araştırma sonucu: Kitap/Rapor/Konferans Bildirisinde Bölüm › Konferans katkısı › bilirkişi

TY - GEN

T1 - Evaluation of critical parameters in the design of a trainer aircraft landing gear

AU - Cetinkaya, Burhan

AU - Ozkol, Ibrahim

PY - 2017/9/14

Y1 - 2017/9/14

N2 - In this study, the ways of analysis to evaluate best-fit landing gears for an aircraft considered is explicitly conducted. The configurations are designed then analyzed in order to obtained optimum landing gears designed. The dynamic equations of the wheelbase and wheel track which described the aircraft can be laterally stabilized on the ground are given. The dimensioning of the shock absorbers which are the basic components of the landing gears and stroke, the dimensions and pressure of landing gear wheels are obtained. Landing gear components and links are exposed important loads during the touch-down. These external and internal loads are applied to the models. Under the effect of these loads the structural behavior of the landing gear components are analyzed.

AB - In this study, the ways of analysis to evaluate best-fit landing gears for an aircraft considered is explicitly conducted. The configurations are designed then analyzed in order to obtained optimum landing gears designed. The dynamic equations of the wheelbase and wheel track which described the aircraft can be laterally stabilized on the ground are given. The dimensioning of the shock absorbers which are the basic components of the landing gears and stroke, the dimensions and pressure of landing gear wheels are obtained. Landing gear components and links are exposed important loads during the touch-down. These external and internal loads are applied to the models. Under the effect of these loads the structural behavior of the landing gear components are analyzed.

KW - analyze

KW - design

KW - landing gear

KW - landing loads

KW - main landing gear

KW - nose landing gear

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U2 - 10.1109/ICMAE.2017.8038678

DO - 10.1109/ICMAE.2017.8038678

M3 - Conference contribution

AN - SCOPUS:85032331449

T3 - 2017 8th International Conference on Mechanical and Aerospace Engineering, ICMAE 2017

SP - 391

EP - 394

BT - 2017 8th International Conference on Mechanical and Aerospace Engineering, ICMAE 2017

PB - Institute of Electrical and Electronics Engineers Inc.

T2 - 8th International Conference on Mechanical and Aerospace Engineering, ICMAE 2017

Y2 - 22 July 2017 through 25 July 2017

ER -

Cetinkaya B, Ozkol I. Evaluation of critical parameters in the design of a trainer aircraft landing gear. In 2017 8th International Conference on Mechanical and Aerospace Engineering, ICMAE 2017. Institute of Electrical and Electronics Engineers Inc. 2017. p. 391-394. 8038678. (2017 8th International Conference on Mechanical and Aerospace Engineering, ICMAE 2017). doi: 10.1109/ICMAE.2017.8038678

Evaluation of critical parameters in the design of a trainer aircraft landing gear

Özet

Yayın serisi

???event.eventtypes.event.conference???

Bibliyografik not

BM SKH

Belgeye Erişim

Diğer Dosyalar ve Linkler

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