Patent · US Active

Demolding of large composite parts for aircraft

US11724421B2 · kind B2 · utility

0Cited by
2References
26Claims
0Family size

Assignee

Inventors

Key dates

Filing dateNov 10, 2021
Grant dateAug 15, 2023
Priority date
Expiry dateNov 10, 2041

Classification

  • Technology area (CPC B)Performing Operations; Transporting
  • CPC primaryB64C2001/0072
  • WIPO fieldOther special machines
  • WIPO sectorMechanical engineering

Abstract

Systems and methods are provided for demolding a composite part from a mandrel. The method includes mechanically coupling a first arm of an extraction tool to a first arcuate portion of a composite part that has been hardened onto a mandrel, mechanically coupling a second arm of an extraction tool to a second arcuate portion of the composite part, and separating the composite part from the mandrel by iteratively performing the following operations until the composite part no longer contacts the mandrel: elastically straining the first arcuate portion of the composite part via the first arm, and elastically straining the second arcuate portion of the composite part via the second arm.

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