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1.发明申请公开(公告)号：US20200340426A1
公开(公告)日：2020-10-29
申请号：US16855298
申请日：2020-04-22
Applicant: Airbus Operations SAS
Inventor： Frédéric CHELIN , Guillaume CLAIRET , Gabriel GALINDO FERNANDEZ
IPC: F02K1/62
Abstract: A thrust reverser door for an aircraft propulsion unit, including a seal positioned at an upstream edge of the door. This seal includes a part that projects with respect to the upstream edge of the door and a rigid core to stiffen the projecting part. This configuration serves to reduce aerodynamic disturbances.
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