Airbus (sas)

Airbus Operations Gmbh

Avinash Kumar Yadav

Vinayak Ramachandra Patil

Matthias S Schroeder

Jesus Miguel Batanero Benito

Srivats Srinivasan

Abhishek Vyas

Sven Hardy Werner

Pradeep Gajakosh

Gayathri Swaminathan

Akshay Srinivasamurthy

Rakshith Raghavan Belur

Jason Kuruvilla

Sumit Kumar Malik

Matthias Schroeder

Sven Werner

A fuselage assembly for an aircraft including a stringer extending longitudinally along the fuselage. The stringer defines a fluid channel. The fluid channel is configured to form at least part of a distribution duct of a cabin air distribution system.

Fuselage assembly for an aircraft

A stiffener for an aircraft assembly is disclosed. The stiffener provides structural stability to the aircraft assembly. The stiffener has a first stiffener part having a planar web portion and a second stiffener part arranged with the first stiffener part. The second stiffener part includes a corrugated web portion having a corrugation. The present application also relates to an aircraft assembly, a fuselage for an aircraft, an aircraft and a method of forming a stiffener for an aircraft assembly.

Stiffener for an aircraft assembly

A control surface actuation mechanism for moving a control surface relative to a fixed aerofoil portion of an aircraft is disclosed including an articulating support, a sliding member on the articulating support and coupled to the control surface, the sliding member arranged to slide relative to the articulating support, a track with a path for attachment on the fixed aerofoil portion, and a rigid connecting element connected to the first track and to the sliding member. The first end of the first rigid connecting element is configured to move passively along the path, as the sliding member is driven to slide relative to the articulating support by an actuator.

Control surface actuation mechanism

Growing community of inventors

Bristol, United Kingdom

Avinash Kumar Yadav