Patent · US Active

Actuator for use in aviation

US10421539B2 · kind B2 · utility

0Cited by

2References

16Claims

0Family size

Assignee

ZF FRIEDRICHSHAFEN AG · DE

Inventors

Jürgen Götte · Vellmar, DE
Uwe Arnold · Kassel, DE

Key dates

Filing date	Feb 25, 2016
Grant date	Sep 24, 2019
Priority date	—
Expiry date	May 14, 2036

Classification

Technology area (CPC F)Mechanical Engineering; Lighting; Heating
CPC primaryF16H2001/325
WIPO fieldMechanical elements
WIPO sectorMechanical engineering

Abstract

An actuator for a rotor blade adjustment having an electromechanical drive unit may be connected with an output drive via a gearbox. The drive unit may have at least two partial drives that can be operated independently from one another. The gearbox may be located at least partially between the at least two partial drives such that the at least two partial drives are spaced apart from one another.

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