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EP0860355A1 Expired / Lapsed EP ⏱️ 0.0 years remaining

Aerodynamic structure with variable camber such as landing flaps, airfoil, horizontal and vertical stabilizer

Assignee: Deutsches Zentrum für Luft- und Raumfahrt eV
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Filing: 1998-02-21
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Granted: —
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Expires: 2018-02-21
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Abstract

Abstract The component (9) has a distorting outer skin (11) extending in the air-flow direction (12). Ribs (1) of adjustable shape extend in this direction, and have a closed flexible outer belt (2) running along the skin. Numerous constant-length stiffening struts (3) engage with the belt at each of their ends. One or more actuators can engage with the struts and/or belt, so as to vary the angle included by them. The aerodynamic component can be moved so as to distort the ribs, which can be fixed to the skin while the struts can hinge on the belt at each of their ends.

Inventors

  • 👤 Lucio Flavio Dr.-Ing. Campanile
  • 👤 Holger Hanselka

Bibliographic Details

Application Number —
Jurisdiction EP
Data Source google_patents
Last Synchronized 2026-11-06 02:39
CPC Classifications
B; B64; B64C; B64C3/00; B64C3/38; B64C3/44; B64C3/48

Claims Analysis

Total Claims: 0
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References Cited (Backward Citations)

FR554771A Cited
US2022806A Cited
US3179357A Cited
US3716202A Cited
US3987984A Cited
FR2445267A1 Cited
US4349169A Cited
US4341176A Cited
US4865275A Cited
WO1994026588A1 Cited
US5531407A Cited

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