| タイトル | Pratt and Whitney cryogenic turbopump bearing experience |
| 本文（外部サイト） | http://hdl.handle.net/2060/19900019308 |
| 著者（英） | Poole, W. E.; Bursey, R. W., Jr. |
| 著者所属（英） | Pratt and Whitney Aircraft |
| 発行日 | 1988-09-01 |
| 言語 | eng |
| 内容記述 | Successful, reusable bearings require lubrication, traditionally, a transfer film from sacrificial cage wear. Early testing included materials screening programs to identify suitable cryogenic cage materials. A specially developed element tester that simulated the function of a ball bearing cage was used. Suitable materials must provide lubrication with an acceptably low wear rate, without abrading contacting surfaces. The most promising materials were tested in full scale bearings at speeds up to 4 MDN. Teflon, filled with 40 percent bronze powder, was the best performing material. A variety of bearings were designed and successfully tested in LH2 and LOX. Bearings with bronze filled Teflon cages were successfully tested for 150 hrs. In overload tests, the same design was tested for 5 hrs at maximum Hertz stresses above 450 ksi and an additional 5 hrs with a maximum Hertz stress exceeding 500 ksi. Four bearings were tested in LOX for 25 hrs, with a maximum time per bearing of 10 hrs. |
| NASA分類 | MECHANICAL ENGINEERING |
| レポートNO | 90N28624 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/136302 |
|
