Protection for elements made from composite material
ES2382765A1
Aircraft notebook design
ES2372123A1
Procedure for the repair of aircraft panels.
ES2379371A1
Device for sealing the union of aircraft torsion drawers.
ES2383863A1
Composite material part with great thickness change.
ES2349521A1
WIND TUNNEL WITH A CLOSED SECTION FOR AEROACUSTIC MEASUREMENTS WITH AN ANECOIC COATING.
ES2378702A1
Tools for the catch of the vertical stabilizer of tail of an aircraft.
ES2377637A1
Plane with alar configuration in lambda box.
ES2384920A1
Piece of material with a ramp between two zones.
US2010106471A1
Computer-aided method for a cost-optimized calculation of aerodynamic forces on an aircraft
ES2369451A1
MEAT SYSTEM FOR AIRCRAFT HORIZONTAL STABILIZER AND INSTALLATION PROCEDURE OF SUCH SYSTEM.
ES2367935A1
AIRCRAFT STABILIZING SURFACE OUTPUT EDGE.
ES2385993A1
Rear fuselage of an aircraft with a load introduction zone of a horizontal tail stabilizer and a vertical tail stabilizer comprising load receiving elements of said stabilizers attached to structural elements of the fuselage.
ES2372828A1
Rib-hardware.
ES2373812A1
Aircraft horizontal stabilizing surface.
ES2365884A1
AIRCRAFT MOBILE SURFACES WITH SEALED SLOTS.
ES2382062A1
Stabilizing and directional aircraft control surface
WO2009056459A1
Method and system for assisting in the design of mobile surfaces of an aircraft
US2010019083A1
Control surface of aircraft
ES2351411A1
METHODS AND SYSTEMS TO ADAPT THE TOPOLOGY OF A MULTI-BLOCK STRUCTURED MESH OF AN OBJECT TO A MODIFICATION OF ITS GEOMETRY.
