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    • 5. 发明申请
    • MICRO THRUSTER USES AND IMPROVEMENTS
    • MICRO THRUSTER使用和改进
    • WO2014035531A2
    • 2014-03-06
    • PCT/US2013045879
    • 2013-06-14
    • GAME CHANGERS LLC
    • GARBUZ PIOTR ASANCHEZ JASON D
    • F02G1/043F03H99/00H02S99/00
    • 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.
    • NMSET和相关设备对生成的力量使用和改进。 层状流量控制系统受益于NMSET和相关设备,因为它们简化了安装,并且更容易在现有飞机上进行改造。 通过使用不同能量调节系数的侧面的加热材料,可以产生必要的温度梯度。 表面几何可用于增加产生的力。 光伏膜可以嵌入膜中,提供能够抵消所需推力所需功率的能量源。 进气勺改善通过微型推进器和表面几何形状的气流,气流扩散器增加与较热表面的气流相互作用,导致更高的推力输出。