loadpatents
Patent applications and USPTO patent grants for Schrauf; Geza.The latest application filed is for "leading edge structure for a flow control system of an aircraft".
Patent | Date |
---|---|
Leading edge structure for a flow control system of an aircraft Grant 11,040,769 - Schrauf , et al. June 22, 2 | 2021-06-22 |
Leading Edge Structure For A Flow Control System Of An Aircraft App 20190016444 - SCHRAUF; Geza ;   et al. | 2019-01-17 |
Aircraft having an aircraft fuselage and an air sucking fuselage component Grant 9,623,959 - Schrauf , et al. April 18, 2 | 2017-04-18 |
Flow body, in particular for aircraft Grant 8,702,042 - Gerber , et al. April 22, 2 | 2014-04-22 |
Aircraft Having An Aircraft Fuselage And An Air Sucking Fuselage Component App 20130270390 - Schrauf; Geza ;   et al. | 2013-10-17 |
Flow Body, In Particular For Aircraft App 20130025727 - Gerber; Martin ;   et al. | 2013-01-31 |
Cooling system on the basis of suction of a boundary layer Grant 8,191,834 - Westenberger , et al. June 5, 2 | 2012-06-05 |
Method and device for suctioning the boundary layer Grant 7,757,994 - Schrauf July 20, 2 | 2010-07-20 |
Method And Device For Suctioning The Boundary Layer App 20090020653 - Schrauf; Geza | 2009-01-22 |
Cooling system on the basis of suction of a boundary layer App 20090014593 - Westenberger; Andreas ;   et al. | 2009-01-15 |
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