Invention Grant
- Patent Title: Aircraft propulsion assembly comprising an air flow valve with a variable flow rate
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Application No.: US14634212Application Date: 2015-02-27
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Publication No.: US09835050B2Publication Date: 2017-12-05
- Inventor: Jacques Hervé Marche
- Applicant: Airbus Operations (S.A.S.)
- Applicant Address: FR Toulouse
- Assignee: AIRBUS OPERATIONS (S.A.S.)
- Current Assignee: AIRBUS OPERATIONS (S.A.S.)
- Current Assignee Address: FR Toulouse
- Agency: Jenkins, Wilson, Taylor & Hunt, P.A.
- Priority: FR1453325 20140414
- Main IPC: F01D25/12
- IPC: F01D25/12 ; F01D1/02 ; F01D9/02 ; F01D15/02 ; F01D17/00 ; B64D33/08 ; F01D17/14 ; F02K3/06 ; F02K3/115 ; F02C6/08 ; F02C7/143 ; F02C7/18

Abstract:
A propulsion assembly having a heat exchanger and a system for supplying cold air including an air inlet in a stream of air, an air duct connecting the air inlet fluidly to the exchanger, and an air flow valve with a variable flow rate inside the duct, the valve including a hub having blades projecting radially from the hub forming a helix, each blade having a root mounted rotatably on the hub, the valve comprising an electric motor to drive the hub by a motor shaft, and structure for varying pitch angle of the blades, the extremity of each blade being flush with a wall of the duct, the valve controllable to a closed configuration where pitch angle of the blades is 0° and the valve prevents passage of air, an open configuration where pitch angle is 90°, and/or a charge configuration where pitch angle is between 0° and 90°.
Public/Granted literature
- US20150292352A1 AIRCRAFT PROPULSION ASSEMBLY COMPRISING AN AIR FLOW VALVE WITH A VARIABLE FLOW RATE Public/Granted day:2015-10-15
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