Gas turbine engine variable bleed valve for ice extraction

Patent metadata

Field	Value
Publication number	US-9982598-B2
Application number	US-201213657193-A
Country	US
Kind code	B2
Filing date	Oct 22, 2012
Priority date	Oct 22, 2012
Publication date	May 29, 2018
Grant date	May 29, 2018

Abstract

A variable bleed valve includes a variable bleed valve door disposed in a bleed inlet in transition duct and rotatable about an axis at or near a forward end of door. Valve is operable to open and close a bleed slot open to a booster bleed flowpath located outwardly of transition duct and having an airflow restrictor. Airflow restrictor may be variable such as a flapper valve. Booster bleed flowpath may pass through a bifurcated bleed duct including an inner passage radially bound by spaced apart inner and middle bleed walls and an outer passage radially bound by middle bleed wall and an outer bleed wall. Airflow restrictor may include an outlet area smaller than an inlet area of inner passage. Door seals against middle bleed wall to open inner passage and against outer bleed wall to open both passages.

First claim

What is claimed is:

1. A gas turbine engine variable bleed apparatus comprising:
a variable bleed valve including a variable bleed valve door disposed in a bleed inlet in a transition duct;
a forward lip and an aft lip located at respective upstream and downstream ends of the variable bleed valve door, wherein the variable bleed valve door is pivotable or rotatable about an axis at a forward end of the variable bleed valve door,
wherein the variable bleed valve is operable to open and close a bleed slot open to a plurality of bleed duct passages forming a booster bleed flowpath located radially outward of the transition duct,
wherein the bleed slot extends radially outwardly from an outer annular wall of the transition duct at the bleed inlet to the aft lip,
wherein the aft lip forms a seal with the transition duct when the variable bleed valve is in a first closed position and wherein the aft lip forms a seal with each of the plurality of bleed duct passages when the variable bleed valve is in a first open position and when the variable bleed valve is in a second open position to modulate an amount of bleed air flowing through the plurality of bleed duct passages,
wherein the booster bleed flowpath extends through a bifurcated bleed duct, the bifurcated bleed duct including an inner passage and an outer passage, an inner bleed wall and a middle bleed wall that are radially spaced apart to radially bound the inner passage, and wherein the middle bleed wall and an outer bleed wall are radially spaced apart and radially bound the outer passage;
an airflow restrictor located in the booster bleed flowpath at an inner passage exit of the inner passage, wherein the airflow restrictor includes an outlet area of the inner passage at the inner passage exit larger than an inlet area of the inner passage,
wherein the variable bleed valve door is operable to cooperate with and seal the aft lip at the aft end of the variable bleed valve door against the middle bleed wall to fully open the inner passage and wherein the variable bleed valve door is operable to cooperate with and seal the aft lip against the outer bleed wall to fully open the inner passage and the outer passage.

2. A gas turbine engine variable bleed apparatus comprising:
a variable bleed valve including a variable bleed valve door disposed in a bleed inlet in a transition duct;
a forward lip and an aft lip located at respective upstream and downstream ends of the variable bleed valve door, wherein the variable bleed valve door is pivotable or rotatable about an axis at a forward end of the variable bleed valve door,
wherein the variable bleed valve is operable to open and close a bleed slot open to a plurality of bleed duct passages forming a booster bleed flowpath located radially outward of the transition duct,
wherein the bleed slot extends radially outwardly from an outer annular wall of the transition duct at the bleed inlet to the aft lip,
wherein the aft lip forms a seal with the transition duct when the variable bleed valve is in a first closed position and wherein the aft lip forms a seal with each of the plurality of bleed duct passages when the variable bleed valve is in a first open position and when the variable bleed valve is in a second open position to modulate an amount of bleed air flowing through the plurality of bleed duct passages, the transition duct having a transition duct conical angle with respect to an engine centerline, a booster outer shroud upstream and adjacent the transition duct,
wherein the booster bleed flowpath extends through a bifurcated bleed duct, the bifurcated bleed duct including an inner passage and an outer passage, an inner bleed wall and a middle bleed wall that are radially spaced apart to radially bound the inner passage, and wherein the middle bleed wall and an outer bleed wall are radially spaced apart and radially bound the outer passage;
an airflow restrictor located in the booster bleed flowpath at an inner passage exit of the inner passage, wherein the airflow restrictor includes an outlet area of the inner passage at the inner passage exit larger than an inlet area of the inner passage,
wherein the variable bleed valve door is operable to cooperate with and seal the aft lip at the aft end of the variable bleed valve door against the middle bleed wall to fully open the inner passage and wherein the variable bleed valve door is operable to cooperate with and seal the aft lip against the outer bleed wall to fully open the inner passage and the outer passage.

Assignees

• Gen Electric

Inventors

• Pritchard Jr Byron Andrew
• Califf Charles Daniel
• Wood Peter John
• Holm Raymond Gust
• Van De Wall Allan George
• Pezzi Peter Alfred

Classifications

• F02K3/075

  controlling flow ratio between flows · CPC title

• F02C6/08

  the gas being bled from the gas-turbine compressor · CPC title

• F04D27/023

  Details or means for fluid extraction · CPC title

• F02C9/18

  by bleeding, bypassing or acting on variable working fluid interconnections between turbines or compressors or their stages {(F02C3/113 takes precedence)} · CPC title

• F05D2260/606

  Bypassing the fluid · CPC title