Patent · US Active

Antivibration kit-of-parts and parts therefor, airfoil structure and aircraft provided therewith

US11840336B2 · kind B2 · utility

0Cited by
5References
18Claims
0Family size

Assignee

Inventors

Key dates

Filing dateMay 26, 2020
Grant dateDec 12, 2023
Priority date
Expiry dateAug 16, 2040

Classification

  • Technology area (CPC F)Mechanical Engineering; Lighting; Heating
  • CPC primaryF16F2238/022
  • WIPO fieldTransport
  • WIPO sectorMechanical engineering

Abstract

To reduce vibration of movable airfoil structures, such as rudders, elevators, and ailerons, a spring device, a leaf spring for example, is mounted to an airfoil mounting structure, such as a vertical tail plane, horizontal tail plane or the wings, such that the spring device exerts a force on a cam device, which transforms the spring force into an airfoil torque. The airfoil torque is applied to the airfoil structure and thus reduces a risk of vibration. The cam device is configured to redirect the spring force such that when the airfoil structure is moved in a first direction, torque decreases and when moved in the opposite second direction the torque is zero.

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