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US 10,370,087 B2Granted
Propeller device for aircraft, spacecraft or watercraft
AssigneeAirbus Defence and Space GmbH
InventorsJesús López Ferrer, Eugenio Garrido Corralejo
Life of this patent
Estimating the term…
Abstract
A propeller device for aircraft, spacecraft or watercraft comprising two or more blades and a spinner. The blades are arranged on a hub so that they can be in a deployed or a retracted position. The spinner comprises first, second and third movable portions configured for allowing deploying or retracting the blades and for keeping the blades deployed or retracted.
Claims7
A propeller device comprising:
- two or more blades mounted on a hub connected to a motor or to a generator by a shaft and
- a forward spinner with an outer surface having the shape of a surface of revolution around a longitudinal axis in the direction of said shaft, wherein
- the blades are mounted on the hub by a mounting arrangement configured to arrange the blades in a deployed position or in a retracted position inside the forward spinner;
- the forward spinner comprising:
- a first movable portion movable in the direction of the longitudinal axis and a second rotatory portion rotatable around the longitudinal axis from a closed position to an open position and vice versa wherein the first movable and second rotary portions are configured for allowing deploying or retracting the blades and for keeping the blades deployed or retracted;
- an outer surface of the first movable portion comprising slots suitably dimensioned for allowing passage of the blades through them;
- an outer surface of the second rotatory portion being formed by first slot covers for covering said slots, less the spaces allocated to the blades in their deployed position, when the second rotatory portion is in the closed position;
- a third rotatory portion rotatable around the longitudinal axis from a closed position to an open position and vice versa wherein the third rotatory portion is configured to allow deployment or retraction of the blades and to keep the blades deployed or retracted;
- an outer surface of the third rotatory portion being formed by second slot covers to cover said spaces.
6 more elements
An aircraft or spacecraft comprising a propeller device comprising:
- two or more blades mounted on a hub connected to a motor or to a generator by a shaft and
- a forward spinner with an outer surface having the shape of a surface of revolution around a longitudinal axis in the direction of said shaft, wherein
- the blades are mounted on the hub by a mounting arrangement configured to arrange the blades in a deployed position or in a retracted position inside the forward spinner;
- the forward spinner comprising:
- a first movable portion movable in the direction of the longitudinal axis and a second rotatory portion rotatable around the longitudinal axis from a closed position to an open position and vice versa wherein the first movable and second rotary portions are configured for allowing deploying or retracting the blades and for keeping the blades deployed or retracted;
- an outer surface of the first movable portion comprising slots suitably dimensioned for allowing passage of the blades through them;
- an outer surface of the second rotatory portion being formed by first slot covers for covering said slots, less the spaces allocated to the blades in their deployed position, when the second rotatory portion is in the closed position;
- a third rotatory portion rotatable around the longitudinal axis from a closed position to an open position and vice versa wherein the third rotatory portion is configured to allow deployment or retraction of the blades and to keep the blades deployed or retracted;
- an outer surface of the third rotatory portion being formed by second slot covers to cover said spaces.
6 more elements
A watercraft comprising a propeller device comprising:
- two or more blades mounted on a hub connected to a motor or to a generator by a shaft and
- a forward spinner with an outer surface having the shape of a surface of revolution around a longitudinal axis in the direction of said shaft, wherein
- the blades are mounted on the hub by a mounting arrangement configured to arrange the blades in a deployed position or in a retracted position inside the forward spinner;
- the forward spinner comprising:
- a first movable portion movable in the direction of the longitudinal axis and a second rotatory portion rotatable around the longitudinal axis from a closed position to an open position and vice versa wherein the first movable and second rotary portions are configured for allowing deploying or retracting the blades and for keeping the blades deployed or retracted;
- an outer surface of the first movable portion comprising slots suitably dimensioned for allowing passage of the blades through them;
- an outer surface of the second rotatory portion being formed by first slot covers for covering said slots, less the spaces allocated to the blades in their deployed position, when the second rotatory portion is in the closed position;
- a third rotatory portion rotatable around the longitudinal axis from a closed position to an open position and vice versa wherein the third rotatory portion is configured to allow deployment or retraction of the blades and to keep the blades deployed or retracted;
- an outer surface of the third rotatory portion being formed by second slot covers to cover said spaces.
6 more elements
Dependencies are inferred from the claim text.