Patent · US Active

Gas turbine engine damping device

US9920637B2 · kind B2 · utility

1Cited by
8References
18Claims
0Family size

Assignee

Inventor

Key dates

Filing dateApr 7, 2015
Grant dateMar 20, 2018
Priority date
Expiry dateApr 15, 2036

Classification

  • Technology area (CPC F)Mechanical Engineering; Lighting; Heating
  • CPC primaryF05D2240/80
  • WIPO fieldEngines, pumps, turbines
  • WIPO sectorMechanical engineering

Abstract

An exemplary gas turbine engine assembly includes a damping device having a first side and a second side facing away from the first side. The first side is configured to hold a seal when the second side engages an extension from a gas turbine engine component. The first side is further configured to engage the extension when the second side holds the seal.

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