Patent · US Active

Morphing control surface

US11186355B2 · kind B2 · utility

0Cited by

6References

15Claims

0Family size

Assignee

FACC AG · AT

Inventors

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

Key dates

Filing date	Apr 28, 2017
Grant date	Nov 30, 2021
Priority date	—
Expiry date	Feb 3, 2039

Classification

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

Abstract

The invention relates to an aerodynamic profiled body for an aircraft, in particular a winglet, comprising a front profiled element having a profile front edge, a rear profiled element having a profile rear edge, and an adjusting unit, which connects the front profiled element to the rear profiled element and by means of which the rear profiled element can be moved in relation to the front profiled element, wherein the adjusting unit has a front mounting device connected to the front profiled element, a rear mounting device connected to the rear profiled element, and a force-transmitting device, which connects the front mounting device and the rear mounting device to each other.

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