Open AccessA preliminary design of a schematic evaluation of low emission turbofan combustors
Author(s) -
Vamsi U Krishna,
N. V. Mitrokhov
Publication year - 2021
Publication title -
journal of physics. conference series
Language(s) - English
Resource type - Journals
SCImago Journal Rank - 0.21
H-Index - 85
eISSN - 1742-6596
pISSN - 1742-6588
DOI - 10.1088/1742-6596/1891/1/012026
Subject(s) - turbofan , schematic , aeronautics , thrust , aerospace engineering , automotive engineering , aviation , combustion , environmental science , computer science , engineering , electrical engineering , chemistry , organic chemistry
This paper examines low emission combustion technologies (LECT) schemes suitable to the sixth generation high-bypass Turbofan engines designed to operate on narrow-body aircraft with a rated thrust (F∞ in kN) of 90-250 kilo-Newton(kN) and an overall pressure ratio of (Π∞) ≥ 30. The examined schemes are based on 11 th regulatory standards of the Committee on Aviation Environmental Protection (CAEP). A brief overview on emissions is provided.