Patent · US Active

Gas bleed arrangement

US10174681B2 · kind B2 · utility

3Cited by
7References
20Claims
0Family size

Assignee

Inventor

Key dates

Filing dateFeb 19, 2016
Grant dateJan 8, 2019
Priority date
Expiry dateApr 14, 2037

Classification

  • Technology area (CPC F)Mechanical Engineering; Lighting; Heating
  • CPC primaryF04D27/023
  • WIPO fieldEngines, pumps, turbines
  • WIPO sectorMechanical engineering

Abstract

A gas bleed arrangement for a gas turbine engine. The gas bleed arrangement includes an annular casing defining a main gas flow path. The annular casing has a plurality of bleed ducts each defining a respective bleed flow path. The arrangement further includes a blocking element having at least one aperture. The blocking element is moveable to align the at least one aperture at least partly between the main gas flow path and at least one of the bleed flow paths to control fluid communication between the main gas flow path and the at least one of the bleed flow paths through the aperture.

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