Patent · US Active

Seal for hardware segments

US10221712B2 · kind B2 · utility

4Cited by
13References
20Claims
0Family size

Assignee

Inventors

Key dates

Filing dateMay 16, 2016
Grant dateMar 5, 2019
Priority date
Expiry dateDec 14, 2036

Classification

  • Technology area (CPC Y)Emerging Cross-Sectional Technologies
  • CPC primaryY02T50/60
  • WIPO fieldEngines, pumps, turbines
  • WIPO sectorMechanical engineering

Abstract

The present disclosure is directed to a shroud assembly for a gas turbine engine that includes a first shroud segment, a second shroud segment spaced from the first shroud segment, and a third shroud segment spaced from the first shroud segment. The first and the second shroud segments define a gap therebetween, and the first and the third shroud segments define a gap therebetween. A first seal portion is positioned at least partially on the first and the third shroud segments and at least partially covers the gap defined by the first and the third shroud segments. A second seal portion is positioned at least partially on the first and the second shroud segments and at least partially covers the gap defined by the first and the second shroud segments. A third seal portion extends between and couples the first and the second seal portions.

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