| タイトル | Effects of surface chemistry on hot corrosion life |
| 本文（外部サイト） | http://hdl.handle.net/2060/19860018615 |
| 著者（英） | Fryxell, R. E.; Leese, G. E. |
| 著者所属（英） | General Electric Co. |
| 発行日 | 1986-06-01 |
| 言語 | eng |
| 内容記述 | Burner rig tests were conducted under the following conditions: 900 C, hourly thermal cycling, 0.5 ppm sodium as NaCl in the gas stream, and Mach 0.3 velocity. The alloys tested were Udimet 700 (U700) and Rene 80, uncoated and with RT21, Codep, or NiCoCrAlY coatings. The tests, up to 1000 hours, included specimens in the as-processed condition and after aging at 1100 C in oxidizing or inert environments for up to 600 hours. Coil-inductance changes were measured for periodic nondestructive inspection of speciments and found useful in the following course of corrosion. Typical sulfidation observed in all cases was similar to that observed in service-run turbine components. Aging at 1100 C caused severe decrease in the hot corrosion life of RT21 and Codep coatings and a significant but lesser decrease in the life of NiCoCrAlY coatings. The extent of these decreases was much greater for all three coatings on U700 than on Rene substrates. A coating hot corrosion life-predicitin model was proposed. The model requires time/temperature information for a turbine component at takeoff conditions as well as environmental contaminant information. |
| NASA分類 | AIRCRAFT PROPULSION AND POWER |
| レポートNO | 86N28087
NAS 1.26:179471
NASA-CR-179471
R86AEB361 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/153807 |
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