Establishing System Requirements of an Aviation Piston Engine

Ersoy Kıvılcım; Beriş Banu

doi:10.4028/www.scientific.net/AMM.598.215

Paper Titles

The Study on the Influence of Gust Wind on Vehicle Stability
p.198

Study of Nonlinear Dynamics of Rotor-Bearing System Coupled with a Floating Raft Isolation Device
p.202

Numerical Simulation on the Performance of Vertical Jet Flowmeter of Natural Gas
p.206

Engine Fault Diagnosis Based on EEMD Difference Energy Spectrum
p.210

Establishing System Requirements of an Aviation Piston Engine
p.215

Development of New Vehicle Power Integration System
p.219

Simple Engine Exhaust Temperature Modeling and System Identification Based on Markov Chain Monte Carlo
p.224

FEM-Based Topological Optimization on the Spindle Box of Heavy Duty CNC Lathe Machine
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Effect of Excitation Waveforms on Biomimetic Cilia-Based Micromixing
p.233

HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vol. 598Establishing System Requirements of an Aviation...

Establishing System Requirements of an Aviation Piston Engine

Abstract:

This paper demonstrates how to establish the system level requirement set for an aviation piston engine, which is intended to be used for a MALE class UAV and for a Part 23 Normal category airplane. Here, it will be demonstrated, which requirements should be taken into account to construct the system level requirement set. This work is aimed to depict a methodology to create the system level requirement set.