Abstract: A combustor assembly (100) for a gas turbine engine is provided. The combustor assembly (100) generally includes an annular dome and a liner. The liner at least partially defines a combustion chamber (114) and includes the forward end received within a slot defined by the annular dome. Additionally, a heat shield (142) is provided. The heat shield (142) includes an end also received within the slot defined by the annular dome. A mounting assembly attaches the forward end of the liner and the end of the heat shield (142) to the annular dome, such that the forward end of the liner and the end of the heat shield (142) are co-mounted within the slot defined by the annular dome. FIG.l
SOFT COPY ATTACHED IN PDF
| # | Name | Date |
|---|---|---|
| 1 | Correspondence by Agent_Nortaized Assignment_25-01-2017.pdf | 2017-01-25 |
| 1 | Power of Attorney [31-08-2016(online)].pdf | 2016-08-31 |
| 2 | Form 5 [31-08-2016(online)].pdf | 2016-08-31 |
| 2 | Nortaized Certificate_Assignment_25-01-2017.pdf | 2017-01-25 |
| 3 | Form 3 [31-08-2016(online)].pdf | 2016-08-31 |
| 3 | Other Patent Document [25-01-2017(online)].pdf | 2017-01-25 |
| 4 | abstract 201644029723.jpg | 2016-10-03 |
| 4 | Drawing [31-08-2016(online)].pdf | 2016-08-31 |
| 5 | Description(Complete) [31-08-2016(online)].pdf | 2016-08-31 |
| 6 | abstract 201644029723.jpg | 2016-10-03 |
| 6 | Drawing [31-08-2016(online)].pdf | 2016-08-31 |
| 7 | Form 3 [31-08-2016(online)].pdf | 2016-08-31 |
| 7 | Other Patent Document [25-01-2017(online)].pdf | 2017-01-25 |
| 8 | Form 5 [31-08-2016(online)].pdf | 2016-08-31 |
| 8 | Nortaized Certificate_Assignment_25-01-2017.pdf | 2017-01-25 |
| 9 | Correspondence by Agent_Nortaized Assignment_25-01-2017.pdf | 2017-01-25 |
| 9 | Power of Attorney [31-08-2016(online)].pdf | 2016-08-31 |