Vorderkantenleisten mit Kontinuierlicher Haut

Details

Veröffentlichungs-Nr.

EP3816039

Aktenzeichen

EP20198634

Anmeldetag

28. September 2020

Veröffentlichung

3. April 2024

Erteilung

3. April 2024

Rechtsraum

EP

IPC

B64C3/28B64C9/24B64C9/34B64C3/50B64C9/22

Abstract

Continuous skin leading edge slats are disclosed. A disclosed example leading edge slat (400) for use with an aircraft includes a single-piece nose skin (402) defining upper (412) and lower (414) 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 (508) coupled to an inner surface of the single-piece nose skin. The box spar (508) includes lateral walls (520) extending away from the inner surface of the single-piece nose skin. The lateral walls define at least one compartment (528) of the box spar.

Anmelder

Firma

The Boeing Company

Land

🇺🇸 USA

Fachgebiete