| 发明名称 | Integrated thermal system for a gas turbine engine | ||
| 摘要 | An integrated thermal system for a gas turbine engine includes an Air-Oil Cooler and an Air-Air PreCooler within a housing, the Air-Air PreCooler downstream of the Air-Oil Cooler. | ||
| 申请公布号 | US9080511(B2) | 申请公布日期 | 2015.07.14 |
| 申请号 | US201113278279 | 申请日期 | 2011.10.21 |
| 申请人 | UNITED TECHNOLOGIES CORPORATION | 发明人 | Suciu Gabriel L.;Penda Allan R.;Merry Brian D.;Dye Christopher M.;Snape Nathan |
| 分类号 | F02C7/12;F02C7/06;F02C7/08;F02C7/14;F02C7/18 | 主分类号 | F02C7/12 |
| 代理机构 | Carlson, Gaskey & Olds, P.C. | 代理人 | Carlson, Gaskey & Olds, P.C. |
| 主权项 | 1. An integrated thermal system for a gas turbine engine comprising: an Air-Air PreCooler immediately downstream and adjacent to an Air-Oil Cooler; a first pump downstream of a fan section in fluid communication with said Air-Oil Cooler and a fan bypass flow path, wherein said first pump is operable to provide a 1.4:1 pressure ratio from said fan bypass flow path of the gas turbine engine to said Air-Oil Cooler. | ||
| 地址 | Hartford CT US | ||