Patent · US Active

Adjustable air flow plenum with circumferential movable closure for a fan of a gas turbine engine

US11965528B1 · kind B1 · utility

0Cited by
36References
20Claims
0Family size

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Inventors

Key dates

Filing dateAug 16, 2023
Grant dateApr 23, 2024
Priority date
Expiry dateAug 16, 2043

Classification

  • Technology area (CPC F)Mechanical Engineering; Lighting; Heating
  • CPC primaryF05D2240/14
  • WIPO fieldEngines, pumps, turbines
  • WIPO sectorMechanical engineering

Abstract

A fan case assembly adapted for use with a gas turbine engine includes a case at extends circumferentially at least partway about an axis of the gas turbine engine and a plurality of vanes. The case is formed to define a plenum that extends circumferentially at least partway about the axis. The plurality of vanes are arranged in the plenum and spaced apart circumferentially about the axis to define a plurality of inlet openings in fluid communication with the plenum.

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