Patent · US Active

Wing for an aircraft including high-lift device hold-down arrangement

US12116130B2 · kind B2 · utility

0Cited by
2References
8Claims
0Family size

Assignee

Inventor

Key dates

Filing dateNov 17, 2020
Grant dateOct 15, 2024
Priority date
Expiry dateNov 17, 2040

Classification

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

Abstract

A wing for an aircraft is disclosed including a fixed wing, a high-lift device and a hold-down arrangement arranged between two supports of the high lift device having a first hold-down element attached to the high-lift device and a second hold-down element attached to the fixed wing. The first hold-down element contacts the second hold-down element when the high-lift device is in a retracted position in which it prevents a trailing edge of the high-lift device from detaching from an upper surface of the fixed wing when the fixed wing deforms in the spanwise direction. One of the hold-down elements is a load-limited hold-down element which comprises a hydraulic element that is configured to allow the high-lift device to move away from the fixed wing when a load acting through the hold-down arrangement exceeds an operational threshold.

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