发明名称 |
HYBRID PROPULSION POWER SYSTEM FOR AERIAL VEHICLES |
摘要 |
This disclosure generally relates to a hybrid solid-state propulsion system for aerial vehicles. The hybrid propulsion system includes a combustor, a thermophotovoltaic generator, and a thermoelectric generator. The combustor burns a chemical based fuel to produce radiation and heat that are converted into electricity used to power the aerial vehicle. The thermophotovoltaic generator is positioned to receive radiation and remnant heat generated by flames in the combustor while the thermoelectric generator receives heat from exhausted flue gases from the combustor. |
申请公布号 |
US2016090184(A1) |
申请公布日期 |
2016.03.31 |
申请号 |
US201514867152 |
申请日期 |
2015.09.28 |
申请人 |
REEBEEZ, INC |
发明人 |
Ghoshal Ankita |
分类号 |
B64D27/24;H02P31/00;H02S10/30;B64C39/02;H01L35/30 |
主分类号 |
B64D27/24 |
代理机构 |
|
代理人 |
|
主权项 |
1. A propulsion system, comprising:
a combustor; a thermophotovoltaic generator; and a thermoelectric generator. |
地址 |
Austin TX US |