Share Email Print
cover

Proceedings Paper

Smart actuation of inlet guide vanes for small turbine engine
Author(s): Razvan Rusovici; Stephen Thiam-Choy Kwok Choon; Paavo Sepri; Joshuo Feys
Format Member Price Non-Member Price
PDF $14.40 $18.00

Paper Abstract

Unmanned Aerial Vehicles (UAVs) have gained popularity over the past few years to become an indispensable part of aerial missions that include reconnaissance, surveillance, and communication [1]. As a result, advancements in small jet-engine performance are needed to increase the performance (range, payload and efficiency) of the UAV. These jet engines designed especially for UAV's are characterized by thrust force on the order of 100N and due to their size and weight limitations, may lack advanced flow control devices such as IGV [2]. The goal of the current study was to present a conceptual design of an IGV smart-material based actuation mechanism that would be simple, compact and lightweight. The compressor section of an engine increases the pressure and conditions the flow before the air enters the combustion chamber [3]. The airflow entering the compressor is often turbulent due to the high angle of incidence between engine inlet and free-stream velocity, or existing atmospheric turbulence. Actuated IGV are used to help control the relative angle of incidence of the flow that enters the engine compressor, thereby preventing flow separation, compressor stall and thus extending the compressor's operating envelope [4]. Turbine jet- engines which employ variable IGV were developed by Rolls Royce (Trent DR-900) and General Electric (J79).

Paper Details

Date Published: 15 April 2011
PDF: 14 pages
Proc. SPIE 7981, Sensors and Smart Structures Technologies for Civil, Mechanical, and Aerospace Systems 2011, 79813F (15 April 2011); doi: 10.1117/12.881953
Show Author Affiliations
Razvan Rusovici, Florida Institute of Technology (United States)
Stephen Thiam-Choy Kwok Choon, Florida Institute of Technology (United States)
Paavo Sepri, Florida Institute of Technology (United States)
Joshuo Feys, Florida Institute of Technology (United States)


Published in SPIE Proceedings Vol. 7981:
Sensors and Smart Structures Technologies for Civil, Mechanical, and Aerospace Systems 2011
Masayoshi Tomizuka, Editor(s)

© SPIE. Terms of Use
Back to Top