The Impact of Damage to the Compressor on the Operating Parameters of the Pratt & Whitney 206B2 Turbine Engine

The article presents the impact of damage to the centrifugal compressor of the P&W 206B2 turbine engine, built in the EC-135p2 helicopters EC-135p2. The damages are caused by sucking the foreign bodies to the inlet, what results in the changes of exploitation parameters of the engine and thermod...

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Bibliographic Details
Published in:Problemy Mechatroniki
Main Authors: Bartosz PRZYBYŁA, Zbigniew ZAPAŁOWICZ
Format: Article
Language:English
Published: Military University of Technology, Warsaw 2018-03-01
Subjects:
mechanics
aircraft engines
compressor centrifugal
compressor damage
Online Access:http://promechjournal.pl/gicid/01.3001.0011.7179

Internet

http://promechjournal.pl/gicid/01.3001.0011.7179

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