发明名称 |
MICRO THRUSTER USES AND IMPROVEMENTS |
摘要 |
NMSET and related device uses and improvements to the forces generated. Laminar flow control systems benefit from NMSET and related devices as they simplify installation and are easier to retrofit on existing aircraft. Necessary temperature gradients can me generated by using a heated material with the sides at different energy accommodation coefficients. Surface geometries can be used to increase the force generated. Photovoltaic film can be embedded into the membrane, providing a source of energy that can offset the power required for desired thrust. Intake scoops improve the air flow through the micro thrusters and surface geometries, and airflow diffusers increase air flow interaction with the hotter surface resulting in higher thrust outputs. |
申请公布号 |
US2015176525(A1) |
申请公布日期 |
2015.06.25 |
申请号 |
US201314407814 |
申请日期 |
2013.06.14 |
申请人 |
GAME CHANGERS, LLC |
发明人 |
Garbuz Piotr A.;Sanchez Jason D. |
分类号 |
F02G1/043 |
主分类号 |
F02G1/043 |
代理机构 |
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代理人 |
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主权项 |
1. A method of combining power generation and propulsion comprising:
integrating a power generating membrane with a thrust generating membrane; and wherein said power generating membrane is integrated on the thrust generating membrane. |
地址 |
New York NY US |