Works related to identification of harmful exhaust components from
aviation engines have continued since the second half of the last
century. These works focus on high-thrust turbine engines. For
this, group testing and standardization procedures have been
developed containing the admissible limits of exhaust components.
Since 2007 works have been underway related to the identification
of harmful exhaust components from engines of low power output that
have not yet been included in the emissions legislation. These
actions are particularly related to the measurements of the exhaust
emissions from piston aviation engines and they are focused on the
fuel applied for these engines. This book presents the results of
the author's own research work related to the issues of exhaust
emissions from powertrains of aircraft and helicopters fitted with
piston or turbine engines not yet included in the emission
legislation. Research has been presented for turbocharged piston
and jet engines aircraft. Test procedures have been presented
related to the measurement of the exhaust emission under actual
conditions of operation. The study presents analyses of the
operating conditions of aviation engines, for which data from the
on-board recording devices (flight parameters) have been used.
Tests have been developed related to the engines operating under
actual operating (in-flight) conditions. The methodology of the
developed test has been validated based on a test dedicated for an
aircraft fitted with a jet engine. The test results have been
subject to a comparison with the results of tests applicable in the
homologation procedures. Eventually, the authors proposed exhaust
emissions tests dedicated to individual aircraft groups.
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