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

Department of Aeronautical Engineering

Istanbul Technical University

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

3 Citations (Scopus)

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.

Original language	English
Title of host publication	2017 8th International Conference on Mechanical and Aerospace Engineering, ICMAE 2017
Publisher	Institute of Electrical and Electronics Engineers Inc.
Pages	391-394
Number of pages	4
ISBN (Electronic)	9781538633052
DOIs	https://doi.org/10.1109/ICMAE.2017.8038678
Publication status	Published - 14 Sept 2017
Event	8th International Conference on Mechanical and Aerospace Engineering, ICMAE 2017 - Prague, Czech Republic Duration: 22 Jul 2017 → 25 Jul 2017

Publication series

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

Conference

Conference	8th International Conference on Mechanical and Aerospace Engineering, ICMAE 2017
Country/Territory	Czech Republic
City	Prague
Period	22/07/17 → 25/07/17

Bibliographical note

Publisher Copyright:
© 2017 IEEE.

Keywords

analyze
design
landing gear
landing loads
main landing gear
nose landing gear

UN SDGs

This output contributes to the following UN Sustainable Development Goals (SDGs)

Access to Document

10.1109/ICMAE.2017.8038678

Cite this

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). Article 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,

day = "14",

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.",

pages = "391--394",

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

address = "United States",

}

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).

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

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

UR - http://www.scopus.com/inward/record.url?scp=85032331449&partnerID=8YFLogxK

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

Abstract

Publication series

Conference

Bibliographical note

Keywords

UN SDGs

Access to Document

Other files and links

Fingerprint

Cite this