Patent · US Active

Control surface element

US10562607B2 · kind B2 · utility

1Cited by

24References

6Claims

0Family size

Assignee

FACC AG · AT

Inventors

Hermann Filsegger · Ried im Innkreis, AT
Walter Stephan · St. Martin, AT

Key dates

Filing date	Apr 22, 2016
Grant date	Feb 18, 2020
Priority date	—
Expiry date	Apr 22, 2036

Classification

Technology area (CPC Y)Emerging Cross-Sectional Technologies
CPC primaryY02T50/40
WIPO fieldOther special machines
WIPO sectorMechanical engineering

Abstract

A control surface element for an aircraft, more particularly a spoiler, comprising an upper outer skin element that has an outer air flow face; comprising a lower outer skin element; comprising at least one reinforcement rib; and comprising a core element made of a foam material; wherein the reinforcement rib is positioned between two core segments of the core element.

Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.