Patent · US Expired

Segmentized flap system

US4892274A · kind A · utility

70Cited by
9References
5Claims
0Family size

Assignee

Inventors

Key dates

Filing dateAug 26, 1986
Grant dateJan 9, 1990
Priority date
Expiry dateAug 26, 2006

Classification

  • Technology area (CPC B)Performing Operations; Transporting
  • CPC primaryB64C9/16
  • WIPO fieldTransport
  • WIPO sectorMechanical engineering

Abstract

A flap system along the trailing edge of a transonic aircraft wing which system includes segments arranged in span direction, a driving system for protraction and retraction of the segments includes a plurality of spindle drives connected to the segments such that each segment is connected to at least two spindle drives; are controlled the spindle drives in such a manner that at least some of the drives are independently controlled from each other so that the segments can pivot on vertical axes, in addition to a regular pivoting about respective horizontal axes.

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