Abstract: CMC ARTICLES HAVING SMALL COMPLEX FEATURES FOR ADVANCED FILM COOLING ABSTRACT An engine component for a gas turbine engine generating hot combustion gas flow is provided. The engine component can include a substrate constructed from a CMC material and having a hot surface facing the hot combustion gas flow and a cooling surface facing a cooling fluid flow. The hot combustion gas flow defines an upstream direction and a downstream direction relative to the hot surface. The substrate also defines a film hole extending through the substrate and having an inlet provided on the cooling surface, an outlet provided on the hot surface, and a passage connecting the inlet and the outlet. The passage comprises a metering section; and a diffusing section, with the diffusing section including a shelf, a first outer lobe and a second outer lobe. Fig.1
Claims:As Attached , Description:As Attached
| # | Name | Date |
|---|---|---|
| 1 | Correspondence by Agent_Assignment _22-02-2017.pdf | 2017-02-22 |
| 1 | Power of Attorney [29-09-2016(online)].pdf | 2016-09-29 |
| 2 | Form 5 [29-09-2016(online)].pdf | 2016-09-29 |
| 2 | Other Patent Document [21-02-2017(online)].pdf | 2017-02-21 |
| 3 | abstract 201644033305.jpg | 2016-11-04 |
| 3 | Form 3 [29-09-2016(online)].pdf | 2016-09-29 |
| 4 | Description(Complete) [29-09-2016(online)].pdf | 2016-09-29 |
| 4 | Drawing [29-09-2016(online)].pdf | 2016-09-29 |
| 5 | Description(Complete) [29-09-2016(online)].pdf | 2016-09-29 |
| 5 | Drawing [29-09-2016(online)].pdf | 2016-09-29 |
| 6 | abstract 201644033305.jpg | 2016-11-04 |
| 6 | Form 3 [29-09-2016(online)].pdf | 2016-09-29 |
| 7 | Form 5 [29-09-2016(online)].pdf | 2016-09-29 |
| 7 | Other Patent Document [21-02-2017(online)].pdf | 2017-02-21 |
| 8 | Correspondence by Agent_Assignment _22-02-2017.pdf | 2017-02-22 |
| 8 | Power of Attorney [29-09-2016(online)].pdf | 2016-09-29 |