Patent Leaderboard
USPTO Patent Rankings Data through Dec 31, 2025
Home › Connecting arrangement for joining two stiffening elements having different cross-sectional profiles for an aircraft or spacecraft, and shell component

Connecting arrangement for joining two stiffening elements having different cross-sectional profiles for an aircraft or spacecraft, and shell component

US Patent 8528865 · Granted Sep 10, 2013

Assignee

Inventors

View full patent text on Google Patents →

More Patents by These Inventors

Manufacturing method for manufacturing a profile rail, profile rail obtainable t2025
Fiber composite part for an aircraft or spacecraft2017
Method for the production of a connecting element, connecting element, and aircr2017
Method for the production of a connecting element, connecting element, and aircr2017
Component arrangement on an aircraft structure, and a method for the installatio2016
Component arrangement on an aircraft structure, and a method for the installatio2016
Method and a device for the preparation of a dry textile preform2016
Aircraft door arrangement2015
Method and device for the production of tubular structural components2015
Method and device for the production of tubular structural components2015
Apparatus for the forming of a lay-up of fibre composite material2015
Shell component for an aircraft or spacecraft2015