2017
DOI: 10.1007/s11668-017-0289-0
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Application of Direct Metal Deposition Process for Failure Prevention of Oil Pump Gear Shaft in an Aero Engine

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Cited by 4 publications
(2 citation statements)
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“…A turbo shaft is the main driving part of an aeroengine. Since the engine often runs at a temperature greater than 500 degrees, under catalysis of metal, carbon deposition (CD) can be produced on the inner surface of a turbo shaft after a series of oxidation reactions, pyrolysis, cracking, dehydrogenation, coking, and polymerization from the fuel in the engine (Tumuluri et al, 2017).…”
Section: Introductionmentioning
confidence: 99%
“…A turbo shaft is the main driving part of an aeroengine. Since the engine often runs at a temperature greater than 500 degrees, under catalysis of metal, carbon deposition (CD) can be produced on the inner surface of a turbo shaft after a series of oxidation reactions, pyrolysis, cracking, dehydrogenation, coking, and polymerization from the fuel in the engine (Tumuluri et al, 2017).…”
Section: Introductionmentioning
confidence: 99%
“…Gear pumps are widely used in lubrication and cooling systems of aircraft. 13 The requirements for aircraft weight reduction have spurred developments aimed at high-speed miniaturization of gear pumps. 46 Wear is aggravated during high-speed operation of the pump, and the journal bearing is the most worn part of the pump.…”
Section: Introductionmentioning
confidence: 99%