Low noise aeroengine inlet system
AssigneePratt & Whitney Canada Corp.
InventorsMichel Labrecque, Vincent Couture-Gagnon, Richard Ullyott
Life of this patent
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Abstract
An aeroengine is provided with a splitter apparatus disposed in a section of an inlet duct. The splitter apparatus can be actuated from a stowed position to a deployed position to allow splitter(s) to selectively move from out of the inlet flow to a position extending into the inlet duct to divide the inlet flow into multiple passages.
Claims12
An aeroengine comprising an inlet duct for directing an air flow from an inlet opening to a compressor rotor, and an inlet splitter apparatus disposed within a section of the inlet duct and having at least one splitter plate pivotally mounted to a wall of the inlet duct about an axis substantially parallel to a direction of the air flow, the at least one splitter plate being pivotally moveable between a deployed position in which the at least one splitter plate extends from the wall of the inlet duct into the inlet duct to expose both sides of the plate to the air flow, and a stowed position in which one side of the at least one plate is positioned against the wall of the inlet duct and the other side of the at least one plate is substantially exposed to the air flow, the at least one splitter plate extends from said one of the top and bottom walls across the inlet duct to the other one of the top and bottom walls, thereby forming a partition wall between the top and bottom walls in said section of the inlet duct when the splitter apparatus is in the deployed position.
An aeroengine inlet system, the inlet system comprising an inlet duct for directing an air flow from an inlet opening to a compressor rotor of an aeroengine, the inlet duct having a section including opposed and substantially flat first and second peripheral walls, an inlet splitter apparatus disposed within said section of the inlet duct and including first and third splitter plates pivotally mounted to the first peripheral wall about respective first and third axes substantially parallel to a direction of the air flow, and second and fourth splitter plates pivotally mounted to the second peripheral wall about respective second and fourth axes substantially parallel to the direction of the air flow, the splitter apparatus being operative between a stowed position in which the first and third splitter plates are pivoted to a position parallel to and adjacent the first peripheral wall and the second and fourth splitter plates are pivoted to a position parallel to and adjacent the second peripheral wall, and a deployed position in which the first and second splitter plates are pivoted to extend from the respective first and second peripheral walls into the inlet duct such that the first splitter plate extends to the second splitter plate to in combination form a first partition wall extending through said section between the first and second peripheral walls and the third and fourth splitter plates are pivoted to extend from the respective first and second peripheral walls into the inlet duct such that the third splitter plate extends to the fourth splitter plate to in combination form a second partition wall extending through said section of the inlet duct between the first and second peripheral walls.
Dependencies are inferred from the claim text.