SUPPORT PYLON FOR AN AIRCRAFT TURBINE ENGINE

• Main Authors: DERENES, Jacky, Raphaël, Michel, BERTIN, Michael, Daniel, Joël, GRENIER, Etienne, Romain, Pascal
• Format: Patent
• Language: English; French; German
• Published: 12.02.2020
• Subjects: AIRCRAFT; AVIATION; BLASTING; COSMONAUTICS; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; ENGINE PLANTS IN GENERAL; GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLYADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR; HEATING; LIGHTING; MACHINES OR ENGINES IN GENERAL; MEASURING; MECHANICAL ENGINEERING; NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES; PERFORMING OPERATIONS; PHYSICS; STEAM ENGINES; TESTING; TESTING STATIC OR DYNAMIC BALANCE OF MACHINES ORSTRUCTURES; TESTING STRUCTURES OR APPARATUS NOT OTHERWISE PROVIDED FOR; TRANSPORTING; WEAPONS

L'invention concerne un pylône (1) de support d'une turbomachine (T) d'aéronef, en particulier pour un banc d'essai, le pylône ayant une forme générale allongée le long d'un axe (A-A) et comportant, à une première extrémité longitudinale (1a), des premiers organes de fixatio...