Abstract: A gas turbine engine includes a compressor section and a turbine section arranged in serial flow order. A shaft is provided rotatable with at least a portion of the compressor section and with at least a portion of the turbine section. A bearing is also provided supporting rotation of the shaft, with a support element in turn supporting the bearing. The gas turbine engine also includes a superelastic member formed of a shape memory alloy supporting at least one of the support element or the bearing. The superelastic member is installed in a pre-stressed condition to enhance a dampening function of the superelastic member.
SOFT COPY ATTACHED IN PDF
| # | Name | Date |
|---|---|---|
| 1 | Power of Attorney [25-05-2016(online)].pdf | 2016-05-25 |
| 2 | Form 5 [25-05-2016(online)].pdf | 2016-05-25 |
| 3 | Form 3 [25-05-2016(online)].pdf | 2016-05-25 |
| 4 | Form 18 [25-05-2016(online)].pdf_15.pdf | 2016-05-25 |
| 5 | Form 18 [25-05-2016(online)].pdf | 2016-05-25 |
| 6 | Drawing [25-05-2016(online)].pdf | 2016-05-25 |
| 7 | Description(Complete) [25-05-2016(online)].pdf | 2016-05-25 |
| 8 | abstract 201641017921 .jpg | 2016-07-28 |
| 9 | Other Patent Document [18-10-2016(online)].pdf | 2016-10-18 |
| 10 | 201641017921-REQUEST FOR CERTIFIED COPY [08-11-2017(online)].pdf | 2017-11-08 |
| 11 | 201641017921-RELEVANT DOCUMENTS [01-03-2019(online)].pdf | 2019-03-01 |
| 12 | 201641017921-FORM 13 [01-03-2019(online)].pdf | 2019-03-01 |
| 13 | 201641017921-FER.pdf | 2019-07-23 |
| 14 | 201641017921-AbandonedLetter.pdf | 2020-01-27 |
| 1 | 2018-12-11_11-12-2018.pdf |