Patent · US Active

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US10443736B2 · kind B2 · utility

0Cited by
7References
17Claims
0Family size

Assignee

Inventor

Key dates

Filing dateOct 1, 2015
Grant dateOct 15, 2019
Priority date
Expiry dateFeb 7, 2036

Classification

  • Technology area (CPC F)Mechanical Engineering; Lighting; Heating
  • CPC primaryF05D2240/55
  • WIPO fieldEngines, pumps, turbines
  • WIPO sectorMechanical engineering

Abstract

A sealing system for a gas turbine engine includes a first surface and a second surface spaced a dimension away from the first surface defining a gap through which a fluid can flow. At least one recess is formed in one of the first surface and the second surface and is oriented such that the fluid flow through the gap crosses the at least one recess. The recess is configured to restrict the fluid flow through the gap in comparison to if the at least one recess were not present, all other things being equal.

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