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US 2023/0407788 A1Published application
Turbine engine inertial particle separator with particle rebound suppression
AssigneesRolls-Royce North American Technologies Inc., University of Virginia Patent Foundation
InventorsBrian J. Connolly, Eric Loth, Crawford F. Smith, III
Life of this patent
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Abstract
An inlet duct for a gas turbine engine includes a particle separator, a scavenge duct, and a layer of material having a low coefficient of restitution. The particle separator including an outer wall spaced, an inner wall, and a splitter located radially between the outer wall and the inner wall. The scavenge duct is coupled with particle separator. The layer of material is located on at least one of the outer wall, the splitter, and the scavenge duct.
Claims20
An air-inlet duct for a gas turbine engine, the air-inlet duct comprising
- a particle separator formed to include an inlet passageway for receiving a stream of air, a compressor passageway that extends downstream from the inlet passageway, and a scavenge passageway that extends downstream from the inlet passageway, the particle separator configured to receive atmospheric air laden with particles and to direct the particles into the scavenge passageway while allowing the atmospheric air to move into the compressor passageway thereby reducing a number of particles that enter the compressor passageway, the particle separator including:
- an outer wall spaced apart from an engine rotation axis,
- an inner wall located radially between the outer wall and the engine rotation axis to define the inlet passageway between the inner wall and the outer wall, and
- a splitter located radially between the outer wall and the inner wall, the splitter including an outer splitter surface that cooperates with the outer wall to define the scavenge passageway and an inner splitter surface cooperating with the inner wall to define the compressor passageway;
- and
- means for reducing the coefficient of restitution on the outer wall of the particle separator to reduce a velocity of the particles colliding with the outer wall to prevent the particles from bouncing off of the outer wall and flowing into the compressor passageway,
- wherein the scavenge passageway defines a channel cross-sectional area between the outer wall and the outer splitter surface, the compressor passageway defines a channel cross-sectional area between the inner wall and the inner splitter surface, a sum of the channel cross-sectional area of the scavenge passageway and the channel cross-sectional area of the compressor passageway defines a total channel area, and the channel cross-sectional area of the scavenge passageway is a percent of the total channel area equal to about one half of the percent of a mass flow rate of air in the scavenge passageway compared to a total mass flow rate of air in the scavenge passageway and the compressor passageway.
4 more elements
(canceled)
An air-inlet duct for a gas turbine engine, the air-inlet duct comprising
- a particle separator having an inner wall, an outer wall arranged circumferentially around the inner wall relative to an axis, and a splitter located radially between the inner wall and the outer wall, the inner wall and the outer wall defining an inlet passageway for receiving a stream of air laden with particles, the inner wall and splitter defining a compressor passageway that extends downstream from the inlet passageway, and the outer wall and the splitter defining a scavenge passageway that extends downstream from the inlet passageway, and
- a fluid injection system configured to direct a stream of liquid along the outer wall and into the scavenge passageway to entrain the particles in the liquid to prevent the particles from flowing into the compressor passageway,
- wherein the fluid injection conduit is located in the inlet passageway and coupled with the outer wall.
(canceled)
(canceled)
A method of reducing particle ingestion in a gas turbine engine, the method comprising
- receiving a flow of atmospheric air laden with particles in an inlet passageway of an air-inlet duct of the gas turbine engine,
- directing, with a splitter, a first portion of the flow with the particles into a scavenge passageway of the air-inlet duct defined between the splitter and an outer wall of the air-inlet duct,
- directing, with the splitter, a second portion of the flow without the particles into a compressor passageway of the air-inlet duct defined between the splitter and an inner wall of the air-inlet duct, and
- injecting a fluid into the inlet passageway and along the outer wall so that the fluid travels along the outer wall and into the scavenge passageway such that the fluid collects the particles that collide with the outer wall and transports the particles into the scavenge passageway,
- wherein the scavenge passageway defines a channel cross-sectional area between the outer wall and an outer splitter surface of the splitter, the compressor passageway defines a channel cross-sectional area between the inner wall and an inner splitter surface of the splitter, a sum of the channel cross-sectional area of the scavenge passageway and the channel cross-sectional area of the compressor passageway defines a total channel area, and the channel cross-sectional area of the scavenge passageway is a percent of the total channel area equal to about one half of the percent of a mass flow rate of air in the scavenge passageway compared to a total mass flow rate of air in the scavenge passageway and the compressor passageway.
2 more elements
(canceled)
Dependencies are inferred from the claim text.