A window (7) with an emergency exit function for a helicopter (1) is described that comprises: a frame shaped as a framework (8) that can be coupled to a door (6) of said helicopter provided with an opening (9); and a transparent element (10) designed to engage the opening (9) and held in position by the frame (8); the frame (8) comprises a first side (25) arranged abutting against the transparent element (10) when a first force (F) below a threshold value is exerted on the latter in a direction transversal to a first plane (P) of a main portion (11) of the transparent element (10), and which can be elastically moved away from the transparent element (10) when the first force (F) exerted on the latter exceeds the threshold value; and a second side (30) having greater flexural rigidity than the first side (25) in a second plane transversal to first plane (P) and arranged abutting against the transparent element (10) even when the force (F) is greater than said threshold value.
WINDOW WITH AN EMERGENCY EXIT FUNCTION FOR A HELICOPTER AND METHOD FOR REMOVING A TRANSPARENT ELEMENT FROM THIS WINDOW
FENSTER MIT EINER NOTAUSGANGSFUNKTION FÜR EINEN HUBSCHRAUBER UND VERFAHREN ZUM ENTFERNEN EINES TRANSPARENTEN ELEMENTS VON DIESEM FENSTER
FENÊTRE PRÉSENTANT UNE FONCTION DE SORTIE D'URGENCE POUR UN HÉLICOPTÈRE ET PROCÉDÉ DE RETRAIT D'UN ÉLÉMENT TRANSPARENT À PARTIR DE LADITE FENÊTRE
2018-11-14
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
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