| 发明名称 |
AIRCRAFT PROPULSION ARCHITECTURE INTEGRATING AN ENERGY RECOVERY SYSTEM |
| 摘要 |
A drive system of at least one rotor of an aircraft via electrical energy in addition to or as a replacement of a mechanical system. The electrical energy is provided at least in part by at least one device for recovering thermal energy from hot gases of an internal combustion engine of the aircraft. |
| 申请公布号 |
US2014290208(A1) |
申请公布日期 |
2014.10.02 |
| 申请号 |
US201214236621 |
申请日期 |
2012.08.03 |
| 申请人 |
Rechain Bruno;Smaoui Hichem;Joubert Emmanuel;Bezes Gilles;Sautreuil Matthieu |
发明人 |
Rechain Bruno;Smaoui Hichem;Joubert Emmanuel;Bezes Gilles;Sautreuil Matthieu |
| 分类号 |
F02C9/16 |
主分类号 |
F02C9/16 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. An aircraft provided with at least one propulsion turbine and comprising an electrical power system for powering at least one item of equipment and comprising a thermal energy recuperation device, installed on the turbine, for generating electrical energy using thermal energy contained in exhaust gases of the turbine as its hot source and using one of the following working fluid as its cold source: ambient air, engine oil, fuel or turbine cooling fluid. |
| 地址 |
Paris FR |
