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- W1977769419 abstract "An assessment is currently being made of the behaviour of six coatings on first-stage high pressure blades in the engines of two long-range maritime patrol aircraft operated by the Royal Australian Air Force. The trial engines contain blades coated with each of the coatings to allow comparison of their relative performances under identical operating conditions. The aim of the trial is to find a coating which will last for 4000 engine operating hours, because the current coating, a conventional nickel aluminide, has a greater than 60% rejection rate after 2000 h. Blades extracted from the trial engines after 500 h and 1000 h of operation already show noticeable trends in the behaviour of the different coating systems. The two aluminides modified with precious metals and the two conventional nickel aluminide coatings are in much better condition than the aluminide coatings modified with either silicon or chromium plus manganese." @default.
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- W1977769419 date "1988-12-01" @default.
- W1977769419 modified "2023-09-27" @default.
- W1977769419 title "Comparative durability of six coating systems on first-stage gas turbine blades in the engines of a long-range maritime patrol aircraft" @default.
- W1977769419 cites W1995570306 @default.
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- W1977769419 doi "https://doi.org/10.1016/0257-8972(88)90134-x" @default.
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