Invention Grant
- Patent Title: Micro thruster uses and improvements
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Application No.: US14407814Application Date: 2013-06-14
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Publication No.: US09863364B2Publication Date: 2018-01-09
- Inventor: Piotr A. Garbuz , Jason D. Sanchez
- Applicant: GAME CHANGERS, LLC
- Applicant Address: US NY New York
- Assignee: GAME CHANGERS, LLC
- Current Assignee: GAME CHANGERS, LLC
- Current Assignee Address: US NY New York
- Agency: Buchanan Ingersoll & Rooney PC
- International Application: PCT/US2013/045879 WO 20130614
- International Announcement: WO2014/035531 WO 20140306
- Main IPC: F02G1/043
- IPC: F02G1/043 ; F03H99/00 ; H02S99/00

Abstract:
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.
Public/Granted literature
- US20150176525A1 MICRO THRUSTER USES AND IMPROVEMENTS Public/Granted day:2015-06-25
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