Device for improving the field of view of aircrafts having...

G - Physics – 02 – B

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G02B 23/12 (2006.01) G01S 13/89 (2006.01) G02B 27/01 (2006.01) G02B 27/18 (2006.01) H04N 7/18 (2006.01) G02B 27/00 (2006.01)

Patent

CA 2150182

L'invention concerne un dispositif d'amélioration du champ de vision d'aéronefs ne présentant pas une surface vitrée suffisante. Le dispositif est constitué au moins d'un collimateur (31, 32) relié à un capteur d'imagerie de l'espace extérieur. Le collimateur projette une image (34) dans le champ de vision du pilote, cette image chevauchant la surface vitrée (6) et le tableau de bord (5) du cockpit. L'image du cockpit coïncide avec l'image réelle dans le champ de vision directe produit par la surface vitrée (6). Application: sécurisation de la phase d'atterrissage.

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