Airship and method for controlling its flight

B - Operations – Transporting – 64 – B

Patent

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Details

B64B 1/24 (2006.01) B64B 1/12 (2006.01)

Patent

CA 2113989

A non-rigid airship is provided which includes a gas envelope having propulsion units mounted on either side thereof Thrust emanating from the propulsion units is deflectable to control at least the vertical positioning of the airship. Horizontal positioning of the airship may be controlled by varying the relative thrust of the propulsion units. A method is also provided for controlling the flight path of an airship. The method includes providing propulsion units on opposite sides of the airship and deflecting the thrust of the propulsion units to control vertical placement of the airship. Horizontal placement of the airship and may be carried out by varying the relative thrust of the propulsion units.

Dirigeable non rigide comprenant une enveloppe de gaz ayant des unités de propulsion montées sur chaque côté. La poussée émanant des unités de propulsion peut être déviée de façon à contrôler au moins le positionnement vertical du dirigeable. Son positionnement horizontal peut être contrôlé en changeant la poussée relative des unités de propulsion. On peut également contrôler la trajectoire de vol du dirigeable. La méthode comprend la présence d'unités de propulsion montées sur les côtés opposés du dirigeable et la déviation de la poussée de ces unités de façon à contrôler le placement vertical du dirigeable. Le placement horizontal du dirigeable peut être effectué en changeant la poussée relative des unités de propulsion.

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