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Base on a concrete engine model, this paper aims to provide an acceptable method of compliance to the engine icing operation and ice ingestion requirements which are demanded by the US airworthiness standards of aircraft engines, i.e., Federal Aviation Administration 14 CFR Part 33, and introduce the application of critical point analysis and experimental arrangement in engine icing certification.
This study shows how the crankshaft design and consequently the crankshaft compliance influence the EHD behaviour of the engine.
The stiffness of the elastic foundation can be different in the vertical and horizontal planes, thereby considering the anisotropy of the engine block compliance with respect to the crankshaft rotation.
This paper presents an application of global sensitivity analysis for system safety analysis and airworthiness compliance of reciprocating aircraft engine.
The silence of the engine worries you.
Power of the engine motor (kW).
The drone of the engine.
The engine and compressor were operated at steady state using approximately 25% of the engine's rated full load.
Begin disassembling the rest of the engine.
Inspect the inside of the engine.
The power and torque of the engine.
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