Abstract: TURBINE ENGINE AND METHOD OF ASSEMBLING THEREOF ABSTRACT A turbine engine (10) is provided. The turbine engine (10) includes a compressor (14) configured to discharge a flow of air (104) at a first flow angle and a combustor (16) coupled downstream from the compressor (14). The combustor (16) is configured to combust the flow of air (104) with fuel to form a flow of combustion gas (106) discharged from the combustor (16) at a second flow angle. The turbine engine (10) also includes a turbine (18) coupled downstream from the combustor (16). The turbine (18) includes an inlet (122) configured to receive the flow of combustion gas (106) having a flow angle within a predetermined range, wherein the combustor (16) is oriented such that the second flow angle is within the predetermined range. FIG. 1
Claims:As Attached , Description:As Attached
| # | Name | Date |
|---|---|---|
| 1 | abstract 6661-CHE-2015.jpg | 2016-08-05 |
| 1 | Power of Attorney [11-12-2015(online)].pdf | 2015-12-11 |
| 2 | 6661-CHE-2015-Correspondence-PA-NOTARIAL CERTIFICATE-020616.pdf | 2016-07-21 |
| 2 | Form 5 [11-12-2015(online)].pdf | 2015-12-11 |
| 3 | 6661-CHE-2015-PA-NOTARIAL CERTIFICATE-020616.pdf | 2016-07-21 |
| 3 | Form 3 [11-12-2015(online)].pdf | 2015-12-11 |
| 4 | 6661-CHE-2015-Power of Attorney-020616.pdf | 2016-07-21 |
| 4 | Drawing [11-12-2015(online)].pdf | 2015-12-11 |
| 5 | Description(Complete) [11-12-2015(online)].pdf | 2015-12-11 |
| 6 | 6661-CHE-2015-Power of Attorney-020616.pdf | 2016-07-21 |
| 6 | Drawing [11-12-2015(online)].pdf | 2015-12-11 |
| 7 | 6661-CHE-2015-PA-NOTARIAL CERTIFICATE-020616.pdf | 2016-07-21 |
| 7 | Form 3 [11-12-2015(online)].pdf | 2015-12-11 |
| 8 | 6661-CHE-2015-Correspondence-PA-NOTARIAL CERTIFICATE-020616.pdf | 2016-07-21 |
| 8 | Form 5 [11-12-2015(online)].pdf | 2015-12-11 |
| 9 | abstract 6661-CHE-2015.jpg | 2016-08-05 |
| 9 | Power of Attorney [11-12-2015(online)].pdf | 2015-12-11 |