A fastening system to couple a first aircraft structure and a second aircraft structure is disclosed. The fastening system includes a fastener, a nutplate having a body defining an opening to receive the fastener, a flange extending from the body to engage an outer surface of the first structure, and a first sleeve protruding from the flange in a direction away from the body, the first sleeve to couple to a first bore formed in the first structure and prevents rotation of the nutplate relative to the first structure.
FASTENING SYSTEM FOR AIRCRAFT STRUCTURES
06.01.2022
Patent
Elektronische Ressource
Englisch
CNC Fastening of Large Aircraft Structures
SAE | 1993
|Fastening system and aircraft integrated with such fastening system
Europäisches Patentamt | 2024
|Spark protection cap, fastening system, fastening method and aircraft
Europäisches Patentamt | 2022
|