Inflatable float assembly for aircraft

Details Inflatable float assembly for aircraft Inflatable float assembly for aircraft

B - Operations, Transporting

64

C

244/83

B64C 25/56 (2006.01)

Patent

CA 1239136

INFLATABLE FLOAT ASSEMBLY FOR AIRCRAFT ABSTRACT OF THE DISCLOSURE Inflatable or pneumatic float assembly has tough outer fabric tubular shell with an upper wall having a first elongated sleeve extending therealong to receive an elongated stiffening member. The float has a plurality old generally transverse webs extending between at least one pair of oppositely spaced apart walls, so as to form a plurality of compartments within the interior of the float. A plurality of air tight bladders having valve means to pass gas are fitted within respective compartments of the float, so that when the bladders are fully inflated with gas, the floats assume an essentially rigid form. The elongated stiffening member extending through the first sleeve has exposed portions to provide access for attachment means which cooperate with the exposed portions to permit the stiffening member to cooperate with an aircraft undercarriage. Means are provided to permit the float to be moved from a lowered position, for the aircraft to land on water, to a raised position, in which wheels are exposed below the float, to permit the aircraft to land on land.

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