Method and device for external de-icing of aircraft

B - Operations – Transporting – 64 – F

Patent

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Details

B64F 5/00 (2006.01)

Patent

CA 2748903

The invention relates to a method for exterior de-icing of an aircraft before takeoff, wherein a region of the aircraft (2) to be de-iced has hot air applied thereto and is heated, said air exiting a de-icing nozzle (10) that can be disposed in the vicinity of the region to be de-iced, wherein hot air exiting a hot air outlet opening (4) of the aircraft is collected and fed to the de-icing nozzle (10). The invention further relates to a device (7) for externally de-icing aircraft, having a flexible hot air channel (9) and a de-icing nozzle (10) disposed at a first end of the hot air channel (9), comprising a collector device (8) for hot air exiting the aircraft (2) and connected to a second end of the hot air channel (9).

L'invention concerne un procédé de dégivrage extérieur d'aéronefs avant un décollage, procédé selon lequel une zone à dégivrer de l'aéronef (2) est exposée à un courant d'air chaud et est réchauffée, ledit courant sortant d'une buse de dégivrage (10) disposée à proximité de la zone à dégivrer, l'air chaud sortant d'une ouverture de sortie d'air chaud (4) de l'aéronef (2) étant collecté et alimentant la buse de dégivrage (10). Un dispositif (7) de dégivrage extérieur d'aéronefs, comprenant un conduit d'air chaud souple (9) et une buse de dégivrage (10) montée à une première extrémité dudit conduit d'air chaud (9), présente un dispositif collecteur (8) de l'air chaud sortant de l'aéronef (2), qui est relié avec une seconde extrémité du conduit d'air chaud (9).

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