• Patent Title: Aerodynamic element, in particular for aircraft, comprising two aerodynamic parts forming an ascending profile junction
  • Application No.: US17776373
    Application Date: 2020-11-03
  • Publication No.: US11873077B2
    Publication Date: 2024-01-16
  • Inventor: Mathias Farouz-Fouquet
  • Applicant: Airbus SAS
  • Applicant Address: FR Blagnac
  • Assignee: Airbus SAS
  • Current Assignee: Airbus SAS
  • Current Assignee Address: FR Blagnac
  • Agency: Greer, Burns & Crain, Ltd.
  • Priority: FR 12845 2019.11.18
  • International Application: PCT/FR2020/051982 2020.11.03
  • International Announcement: WO2021/099710A 2021.05.27
  • Date entered country: 2022-05-12
  • Main IPC: B64C21/02
  • IPC: B64C21/02
Aerodynamic element, in particular for aircraft, comprising two aerodynamic parts forming an ascending profile junction
Abstract:
An aerodynamic element includes at least one first, fixed aerodynamic part including a box section that is covered at least partly by a plate with an extreme part, and one second aerodynamic part including a peripheral surface with an end and at least one holding element provided with a shoulder which forms, with the extreme part of the plate, a groove in which the end of the peripheral surface can be housed, such that the peripheral surface and the plate form a junction having an ascending profile. The presence of the groove makes it possible to obtain a continuous ascending junction with favors a laminar airstream on the upper surface of the aerodynamic element.
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