The Boeing Company

Ramon Augustin Burin

Stephen Roger Amorosi

Matthew Leroy Anderson

Mark A Barr

Michael R Severance

Structure for aircraft

Aero dynamic structure with fastener arrangement

Continuous skin leading edge slats are disclosed. A disclosed example leading edge slat for use with an aircraft includes a single-piece nose skin defining upper and lower external surfaces of the leading edge slat, where the single-piece nose skin is to extend between a fore end and an aft end of the leading edge slat, and a box spar coupled to an inner surface of the single-piece nose skin. The box spar includes lateral walls extending away from the inner surface of the single-piece nose skin. The lateral walls define at least one compartment of the box spar.

Growing community of inventors

Lake Stevens, WA, United States of America

Ramon Augustin Burin