Patent · US Active

Bleed valves for gas turbine engines

US9964223B2 · kind B2 · utility

3Cited by
30References
11Claims
0Family size

Assignee

Inventors

Key dates

Filing dateJul 13, 2015
Grant dateMay 8, 2018
Priority date
Expiry dateJul 13, 2035

Classification

  • Technology area (CPC F)Mechanical Engineering; Lighting; Heating
  • CPC primaryF16K31/12
  • WIPO fieldMechanical elements
  • WIPO sectorMechanical engineering

Abstract

A bleed valve for a gas turbine engine compressor has a valve body and a flapper. The valve body defines a flow path and includes a flapper seat. The flow path extends through the valve body. The flapper is pivotally connected to the valve body and is movable between a closed position and an open position. In the closed position the flapper seats against the flapper seat and blocks the flow path. In the open position the flapper is angled towards the valve body inlet such that fluid moving through the valve body exerts force on the flapper, urging the flapper towards the closed position.

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