A method of making a thin-skin support member, comprising: forging a mounting interface (608); forging a mid-body support (504) having a cylinder (606) extending from the mid-body support; and welding sheet metal (700, 702, 704, 706) to the mid-body support and the mounting interface
AERODYNAMIC NOISE REDUCING THIN-SKIN LANDING GEAR STRUCTURE
VERRINGERUNG VON AERODYNAMISCHEM LÄRM DURCH DÜNNWANDIGE FAHRWERKSTRUKTUR
RÉDUCTION DU BRUIT AÉRODYNAMIQUE D'UNE STRUCTURE DE TRAIN D'ATTERRISSAGE À FINE PELLICULE
2021-05-26
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
Aerodynamic noise reducing thin-skin landing gear structure
Europäisches Patentamt | 2019
|Aerodynamic noise reducing thin-skin landing gear structure
Europäisches Patentamt | 2021
|AERODYNAMIC NOISE REDUCING THIN-SKIN LANDING GEAR STRUCTURE
Europäisches Patentamt | 2017
|AERODYNAMIC NOISE REDUCING THIN-SKIN LANDING GEAR STRUCTURE
Europäisches Patentamt | 2019
|AERODYNAMIC NOISE REDUCTION THIN-SKIN LANDING GEAR STRUCTURE
Europäisches Patentamt | 2021
|