| 发明名称 | Providing oxidation to a gas turbine engine | ||
| 摘要 | A gas turbine engine includes a compressor for compressing air from an environment; a combustor for receiving the compressed air from the compressor, mixing the compressed air with fuel, and combusting the fuel; a turbine coupled with the compressor for receiving exhaust gas from the combustion and powering the compressor; and an injector coupled with a source of oxidizer for injecting the oxidizer into the combustor. A method for operating a gas turbine engine includes compressing air from an environment; receiving the compressed air at a combustor; mixing the compressed air with fuel; injecting oxidizer into the combustor in addition to the air from the environment; combusting the fuel with the compressed air and the oxidizer; receiving exhaust gas from the combusted fuel; and powering the compression of the air from the environment using the exhaust gas. | ||
| 申请公布号 | US9638111(B2) | 申请公布日期 | 2017.05.02 |
| 申请号 | US201214344555 | 申请日期 | 2012.09.14 |
| 申请人 | Martinez Anthony R. | 发明人 | Martinez Anthony R. |
| 分类号 | F02D21/10;F02C3/14;F02C3/22;F02C3/24;F02C9/26 | 主分类号 | F02D21/10 |
| 代理机构 | Advent, LLP | 代理人 | Advent, LLP ;Antonson Erik M.;Keller Gerald M. |
| 主权项 | 1. A gas turbine engine comprising: a compressor for compressing air from an environment; a combustor for receiving the compressed air from the compressor, mixing the compressed air with fuel, and combusting the fuel; a turbine coupled with the compressor for receiving exhaust gas from the combustion and powering the compressor; an injector coupled with a source of oxidizer for injecting an oxidizer into the combustor; and a swirler having the injector for spraying the oxidizer into the combustor, wherein the oxidizer is mixed with the fuel in at least one of a fuel line or a fuel spray nozzle for supplying the fuel to the combustor. | ||
| 地址 | Westminster MD US | ||