Patent · US Active

Deflector for conduit inlet within a combustor section plenum

US11371700B2 · kind B2 · utility

1Cited by
11References
18Claims
0Family size

Assignee

Inventors

Key dates

Filing dateJul 15, 2020
Grant dateJun 28, 2022
Priority date
Expiry dateJul 15, 2040

Classification

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

Abstract

An assembly is provided for a gas turbine engine. This assembly includes a combustor wall, a case and an inlet. The combustor wall is configured with a quench aperture. The case is displaced from the combustor wall such that a plenum is formed by and extends between the combustor wall and the case. The case includes a case wall, a deflector and a conduit. The deflector projects out from the case wall into the plenum towards the combustor wall. The deflector is arranged upstream of the quench aperture. The inlet to the conduit is arranged next to and downstream of the deflector.

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