Start systems for aero gas turbines

A.G. Pascoe (Lytham, Lancashire, UK)

Aircraft Engineering and Aerospace Technology

ISSN: 0002-2667

Publication date: 1 December 2005

Abstract

Purpose

This paper is an overview of aero gas turbine engine starting systems and discusses the system design considerations and integration with other aircraft systems.

Design/methodology/approach

Review of a range of recent publications on the subject, aiming to provide an introduction to modern aero gas turbine engine starting systems.

Findings

Provides basic information on starter types and their limitations, and why some starter types are more favoured in modern installations. The effects of altitude and temperature are discussed which may not be initially considered as variables affecting aero start systems.

Originality/value

This paper provides further information on the starting systems of modern aero gas turbines and the considerations associated with integration and efficiency.

Keywords

Citation

Pascoe, A. (2005), "Start systems for aero gas turbines", Aircraft Engineering and Aerospace Technology, Vol. 77 No. 6, pp. 448-454. https://doi.org/10.1108/00022660510628435

Download as .RIS

Publisher

:

Emerald Group Publishing Limited

Copyright © 2005, Emerald Group Publishing Limited

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