Variable shape airship
AssigneeKelluu Oy
InventorJouni Lintu
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Abstract
Disclosed is a method for controlling an elongated lighter-than-air aircraft formed of a thin shell. The method includes providing a first stiffener on the outer surface of the shell of the aircraft on a first side of a gas tank, and a second stiffener on the outer surface of the shell of the aircraft on a second side of the gas tank, fitting control members with adjustable length through the shell of the aircraft in a gas tank space defined by the inner surface of the shell so the control members extend between the first and second stiffener, adjusting the distance between the first stiffener and the second stiffener when controlling the aircraft by means of the control members by moving the first stiffener and second stiffener in a first and a second direction opposite to each other. Further, disclosed is an aircraft.
Claims8
An aircraft formed of a shell, an inner surface of the shell defining a space for a gas tank fillable with a lighter-than-air gas, an outer surface of the shell defining an external shape of the aircraft, the external shape of the aircraft being elongated and oval when viewed from the side and round when viewed from the front, the aircraft comprising:
- a control arrangement changing the external shape thereof in order to control the aircraft, the control arrangement consisting essentially of:
- a single elongated upper stiffener provided on the outer surface of the shell on a first side of the gas tank,
- at least one elongated lower stiffener provided on the outer surface of the shell on a second side of the gas tank opposite said single elongated upper stiffener, the single elongated upper stiffener and the at least one elongated lower stiffener being parallel to one another,
- at least two control members with adjustable length each extending directly between the single elongated upper stiffener and the at least one elongated lower stiffener through the shell of the aircraft in a gas tank space defined by the inner surface of the shell, the at least two control members being parallel to one another, the single elongated upper stiffener and the at least one elongated lower stiffener being configured to be movable in a first direction and a second direction opposite to each other via the at least two control members, and
- a plurality of lead-throughs provided between the upper and lower stiffeners on the outer surface of the shell and inside of the shell, the plurality of lead-throughs being configured to lead the at least two control members through the aircraft shell,
- wherein the at least two control members are of equal length, said at least two control members of equal length being provided at a distance from each other in the lengthwise direction of said stiffeners thereby maintaining the distance between the stiffeners constant throughout the length of the stiffeners.
A method for controlling an aircraft made of a shell, an inner surface of the shell defining a space for a gas tank fillable with a lighter-than-air gas, an outer surface of the shell defining an external shape of the aircraft, the external shape of the aircraft being elongated and oval when viewed from the side and round when viewed from the front, the method comprising:
- providing a single elongated upper stiffener of a control arrangement on the outer surface of the shell of the aircraft on a first side of the gas tank, and at least one elongated lower stiffener of the control arrangement on the outer surface of the shell of the aircraft on a second side of the gas tank opposite said single elongated upper stiffener, the single elongated upper stiffener and the at least one elongated lower stiffener being parallel to one another;
- fitting at least two control members, of the control arrangement, with adjustable length through the shell of the aircraft in a gas tank space defined by the inner surface of the shell such that said at least two control members extend directly between the single elongated upper stiffener and the at least one elongated lower stiffener, the at least two control members being parallel to one another;
- adjusting the distance between the single elongated upper stiffener and the at least one elongated lower stiffener by moving said single elongated upper stiffener and the at least one elongated lower stiffener in a first direction and a second direction opposite to each other;
- providing a plurality of lead-throughs between the upper and lower stiffeners on the outer surface of the shell and inside of the shell;
- leading, by the plurality of lead-throughs, at least two control members through the aircraft shell;
- and
- configuring said control arrangement lengthwise in the direction of the longitudinal axis of the aircraft along the length of said stiffeners with at least two control members, of the control members, of equal length between said single elongated upper stiffener and said at least one elongated lower stiffener, said at least two control members being provided at a distance from each other in the lengthwise direction of said stiffeners to maintain the distance between the stiffeners constant throughout the length of the stiffeners.
Dependencies are inferred from the claim text.