My Account Log in

1 option

Exergo-environmental Analysis of Basic and Intercooled-Recuperated Gas Turbine based Aviation Auxiliary Power Unit The National Institute of Technology Jamshedpur

SAE Technical Papers (1906-current) Available online

View online
Format:
Conference/Event
Author/Creator:
Sahu, Sahu, author.
Contributor:
R, Sanjay
Sahu, Mithilesh Kumar
Conference Name:
WCX World Congress Experience (2018-04-10 : Detroit, Michigan, United States)
Language:
English
Physical Description:
1 online resource
Place of Publication:
Warrendale, PA SAE International 2018
Summary:
AbstractThis paper deals with the exergo-environmental analysis of gas turbine with possible application as aviation auxiliary-power-unit (APU). The present work reports a comparison of thermodynamic performance, NOx and CO emission for basic gas turbine cycle (BGT) and intercooled-recuperated gas turbine (IcRcGT) cycle based engines for possible use by the aviation industry as auxiliary power unit (APU). In addition to this environmental sustainability index of these two cycles is also presented. Various cycle operating parameters such as compressor-pressure-ratio (rp,c), combustor-primary-zone-temperature, equivalence-ratio, and residence time have been chosen for analysis of the cycles. Mathematical modeling of the cycles has been done and the same have been coded in MATLAB. Results show that IcRcGT cycle exhibits higher gas turbine power output and gas turbine efficiency in comparison to BGT cycle for the same rp,c and turbine inlet temperature (TIT). Percentage exergy destruction for combustion chamber has been found to be lower for IcRcGT cycle as compared to BGT cycle. NOx and CO emission are higher in case of IcRcGT cycle as compared to BGT cycle. Adoption of the proposed scheme id est IcRcGT cycle based APU promises to deliver enhanced performance id est thermal efficiency of around 10.62 percentage points higher thermal efficiency as compared to traditional BGT based APU (rp,c = 2.6 and TIT = 1400K). Also for the proposed APU system, percentage exergy destruction for combustion chamber is reduced by around 14.95% and by 13.18% for the overall cycle (rp,c = 3.8 and TIT = 1300K). Also, IcRcGT cycle is more sustainable aviation APU technology as compared to BGT cycle
Notes:
Vendor supplied data
Publisher Number:
2018-01-1376
Access Restriction:
Restricted for use by site license

The Penn Libraries is committed to describing library materials using current, accurate, and responsible language. If you discover outdated or inaccurate language, please fill out this feedback form to report it and suggest alternative language.

Find

Home Release notes

My Account

Shelf Request an item Bookmarks Fines and fees Settings

Guides

Using the Find catalog Using Articles+ Using your account