Particle separator

Patent metadata

Field	Value
Publication number	US-11073083-B2
Application number	US-201916269267-A
Country	US
Kind code	B2
Filing date	Feb 6, 2019
Priority date	Aug 16, 2013
Publication date	Jul 27, 2021
Grant date	Jul 27, 2021

Abstract

An air-inlet duct includes an outer wall, an inner wall, and a splitter. The splitter cooperates with the outer wall to establish a particle separator which separates particles entrained in an inlet flow moving through the air-inlet duct to provide a clean flow of air to a compressor section of a gas turbine engine.

First claim

What is claimed is:

1. An air-inlet duct for a gas-turbine engine, the air-inlet duct comprising
an outer wall spaced apart from an engine rotation axis,
an inner wall located between the outer wall and the engine rotation axis, the inner wall and the outer wall defining an air-inlet passageway therebetween,
a splitter located between the outer wall and the inner wall and including an outer splitter surface cooperating with the outer wall to define a first channel therebetween and an inner splitter surface cooperating with the inner wall to define a second channel therebetween, and
a flow regulator configured to regulate a portion of an inlet flow including particles, the flow regulator including a series of flow control devices arranged to extend between the outer wall and the outer splitter surface,
wherein the series of flow control devices includes a set of movable flow diverters located between the outer wall and the splitter, the set of movable flow diverters configured to separate the inlet flow into a clean flow substantially free from the particles and a dirty flow containing the particles so that the dirty flow is captured in the first channel,
wherein the series of flow control devices further includes a set of stationary particle diverters located in spaced-apart relation to the set of movable flow diverters at an inlet which opens into the second channel, and the set of stationary particle diverters configured to deflect any of the particles into the first channel, and
wherein the set of movable flow diverters includes at least three movable flow diverters spaced apart relative to each other and each movable flow diverter of the set of movable flow diverters is configured to rotate about an associated rotation axis.

2. The air-inlet duct of claim 1 , further comprising a sensor located downstream of an inlet of the second channel and configured to detect a signal associated with at least one of a size and a quantity of particles entering the second channel, and wherein the set of movable flow diverters are configured to move in response to the signal detected by the sensor.

3. The air-inlet duct of claim 1 , wherein each movable flow diverter of the set of movable flow diverters is configured to move independently of the other movable flow diverters.

4. An air-inlet duct for a gas-turbine engine, the air-inlet duct comprising
an outer wall spaced apart from an engine rotation axis,
an inner wall located between the outer wall and the engine rotation axis, the inner wall and the outer wall defining an air-inlet passageway therebetween,
a splitter located between the outer wall and the inner wall and including an outer splitter surface cooperating with the outer wall to define a scavenge channel therebetween and an inner splitter surface cooperating with the inner wall to define an engine channel therebetween, and
a flow regulator configured to regulate a portion of an inlet flow including particles to cause a size and duration of a separated flow region formed along the outer wall and upstream of a scavenge inlet to the scavenge channel to be minimized so that the particles are collected in the scavenge channel and an amount of the particles entering the engine channel are minimized,
wherein the flow regulator includes a set of movable flow diverters located between the outer wall and the splitter, the set of movable flow diverters configured to separate the inlet flow entering the air-inlet duct into a clean flow substantially free from the particles and a dirty flow containing the particles so that the dirty flow is captured in the scavenge channel,
wherein the set of movable flow diverters includes at least three movable flow diverters spaced apart relative to each other, and
wherein each movable flow diverter of the set of movable flow diverters is configured to rotate about an associated rotation axis.

5. The air-inlet duct of claim 4 , further comprising a sensor located downstream of an engine inlet of the engine channel and configured to detect a signal associated with at least one of a size and a quantity of the particles entering the engine channel, and wherein the set of movable flow diverters are configured to move in response to the signal detected by the sensor to minimize the particles entering the engine channel.

6. The air-inlet duct of claim 5 , wherein each movable flow diverter of the set of movable flow diverters is configured to move independently of the other movable flow diverters.

7. The air-inlet duct of claim 4 , wherein the flow regulator further includes a set of stationary particle diverters located in spaced-apart relation to the set of movable flow diverters at an engine inlet which opens into the engine channel, and the set of stationary particle diverters configured to deflect any of the particles which may bounce off of the outer wall and originally miss the scavenge channel.

8. An air-inlet duct for a gas-turbine engine, the air-inlet duct comprising
an outer wall spaced apart from an engine rotation axis,
an inner wall located between the outer wall and the engine rotation axis, the inner wall and the outer wall defining an air-inlet passageway therebetween,
a splitter located between the outer wall and the inner wall and including an outer splitter surface cooperating with the outer wall to define a scavenge channel therebetween and an inner splitter surface cooperating with the inner wall to define an engine channel therebetween, and
a flow regulator configured to regulate a portion of an inlet flow including particles to cause a size and duration of a separated flow region formed along the outer wall and upstream of a scavenge inlet to the scavenge channel to be minimized so that the particles are collected in the scavenge channel and an amount of the particles entering the engine channel are minimized,
wherein the flow regulator includes a set of movable flow diverters located between the outer wall and the splitter, the set of movable flow diverters configured to separate the inlet flow entering the air-inlet duct into a clean flow substantially free from the particles and a dirty flow containing the particles so that the dirty flow is captured in the scavenge channel, and
wherein the flow regulator further includes a set of movable particle diverters located in spaced-apart relation to the set of movable flow diverters and the set of movable particle diverters is located at an engine inlet which opens into the engine channel, the set of movable particle diverters configured to deflect any of the particles into the scavenge channel.

Assignees

• Rolls Royce Nam Tech Inc
• Univ Virginia Patent Foundation

Inventors

• Snyder Philip H
• Loth Eric
• Barone Dominic L

Classifications

• F05D2300/607

  Monocrystallinity · CPC title

• F05D2240/12

  Fluid guiding means, e.g. vanes · CPC title

• B01D45/06

  by reversal of direction of flow · CPC title

• F05D2260/607

  Preventing clogging or obstruction of flow paths by dirt, dust, or foreign particles · CPC title

• F02C7/052 Primary

  with dust-separation devices · CPC title