Jorge Pablo Verde Preckler, Madrid ES

Patent application number	Description	Published
20090026311	Aircraft tail assembly - An aircraft tail assembly planform comprising curvilinear leading edges (	01-29-2009
20090140096	Impact resistant aircraft fuselage - The invention relates to a structural configuration of the rear fuselage (	06-04-2009
20090152400	Acoustically attenuated fuselage for aircraft - The invention relates to a covering (	06-18-2009
20090159741	Optimized configuration of engines for aircraft - The invention relates to a configuration of engines (	06-25-2009
20090159755	Aircraft control device - The invention relates to a control surface (	06-25-2009
20090256025	STABILIZING AND DIRECTIONAL-CONTROL SURFACE OF AIRCRAFT - Stabilizing and directional-control surface of an aircraft, said surface comprising a vertical stabilizer (	10-15-2009
20100001121	SYSTEM FOR TILTING A POWER UNIT - System for tilting a power unit (	01-07-2010
20110127374	METHODS AND SYSTEMS FOR MINIMIZING FLOW DISTURBANCES IN AIRCRAFT PROPELLER BLADES CAUSED BY UPSTREAM PYLONS - Methods for minimizing the effects of pylori induced disturbances of the airflow at the propeller blades (	06-02-2011

Patent applications by Jorge Pablo Verde Preckler, Madrid ES