An aircraft with a detachable passenger escape cabin and an...

B - Operations – Transporting – 64 – C

Patent

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B64C 1/32 (2006.01) B64D 17/80 (2006.01) B64D 25/12 (2006.01)

Patent

CA 2403158

An aircraft with a detachable cabin (1) that serves to rescue its passengers as a result of the aircraft's sudden fall either due to its malfunction or fire. The cabin escapes either smoothly or by means of fast ejection and descends slowly to the Earth with the aid of a parachute (13; 14); during a crash on the ground or in the sea external airbags (38a-38f) with which it is equipped and which are located in its lower part are inflated thus absorbing the loads that are developed during the crash. In addition a conventional aircraft (70) of the type being already in use is also described and in which the parachute equipment (71) has already been applied; however, the proposed equipment of the airbag boxes (72a-72c) is adapted to it for the absorption of the energy produced due to its crash on Earth in case of its sudden fall.

L'invention concerne un aéronef pourvu d'une capsule amovible (1) permettant de sauver des passagers à la suite d'une chute soudaine de cet aéronef causée par une défaillance ou un incendie. Ladite capsule peut se détacher de manière graduelle ou par éjection rapide, et descend lentement vers le sol à l'aide d'un parachute (13, 14). Avant un choc contre la surface du sol ou de la mer, des coussins gonflables extérieurs (38a-38f) intégrés dans cet aéronef et situés sur la partie inférieure dudit appareil se gonflent, d'où l'absorption de l'énergie produite par ce choc. Par ailleurs, l'invention concerne un aéronef classique (70) en cours d'exploitation avec lequel cet équipement de parachute (71) a déjà été utilisé, l'équipement supplémentaire proposé de coussins gonflables (72a-72c) étant destiné à absorber l'énergie produite par un choc contre la surface du sol en cas de chute soudaine.

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