Deployable apparatus to prevent helicopter rollover
AssigneeTextron Innovations Inc.
InventorsScott David Poster, Martin Peryea
Life of this patent
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AssigneeTextron Innovations Inc.
InventorsScott David Poster, Martin Peryea
Estimating the term…
The present invention includes an apparatus for preventing aircraft rollover upon a water landing comprising: a deployable first and/or second boom affixed by a first end to the aircraft and capable of deployment substantially perpendicular to a longitudinal axis of the aircraft; and a first and/or second air bladder attached to a second end of the first and/or second boom, wherein the first and/or second air bladders are configured to inflate when an aircraft lands in the water, wherein deployment of the first and second boom and air bladder prevents aircraft rollover upon water landing; or a deployable keel affixed by a first end to the aircraft and capable of deployment substantially perpendicular to a longitudinal axis and opposite a rotor of the aircraft upon a water landing, wherein the keel is sized to prevent aircraft rollover upon deployment; or both.
An apparatus for preventing aircraft rollover upon a water landing of an aircraft that is supported by a plurality of float kits of the aircraft, the apparatus comprising:
An aircraft comprising:
A method of preventing aircraft rollover upon a water landing of an aircraft that is supported by a plurality of float kits of the aircraft, the method comprising:
Dependencies are inferred from the claim text.