Power transmission system
AssigneeAirbus Helicopters Deutschland GmbH
InventorsMarc Cortes-Fargas, Wouter Beckers, Juergen Fischer, Thomas Kellner
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Abstract
A power transmission system that is adapted to transmit forces from a motor to a component comprises an externally threaded shaft 551 that is rotatably attached to the motor, an internally threaded fastener that is movably attached to the externally threaded shaft, a first element, and a second element that is movably attached to the first element at a second joint and that is rigidly attached to the component at a third joint.
Claims20
A helicopter comprising a fuselage, an external load device that is connected to the fuselage via a component and a power transmission system that is adapted to transmit forces from a motor that generates a first rotational movement to the component, wherein the power transmission system comprises:
- an externally threaded shaft that is configured to be rotatably attached to the motor and performs a second rotational movement;
- an internally threaded fastener that is movably attached to the externally threaded shaft and performs a movement along the externally threaded shaft in response to the second rotational movement;
- a first element that comprises:
- a first end that is movably attached to the internally threaded fastener at a first joint, and
- a second end;
- and
- a second element that comprises:
- a plateau having a first end and a second end, wherein
- the first end is movably attached to the second end of the first element at a second joint, wherein the first element transmits the forces from the first joint to the second joint, and
- the second end is adapted to be rigidly attached to the component at a third joint, wherein the plateau transmits the forces from the second joint to the third joint by transforming a rotational movement of the second joint into a rotation of the component.
A power transmission system adapted to transmit forces from a motor that generates a first rotational movement to a component, the power transmission system comprising:
- an externally threaded shaft that is configured to be rotatably attached to the motor and performs a second rotational movement;
- an internally threaded fastener that is movably attached to the externally threaded shaft and performs a movement along the externally threaded shaft in response to the second rotational movement;
- a first element that comprises:
- a first end that is movably attached to the internally threaded fastener at a first joint, and
- a second end;
- a second element that comprises:
- a plateau having a first end and a second end, wherein
- the first end is movably attached to the second end of the first element at a second joint, wherein the first element transmits the forces from the first joint to the second joint, and
- the second end is adapted to be rigidly attached to the component at a third joint, wherein the plateau transmits the forces from the second joint to the third joint by transforming a rotational movement of the second joint into a rotation of the component;
- a third element that comprises:
- a first end that is movably attached to the internally threaded fastener at a fourth joint that is positioned on the internally threaded fastener at a side that is opposite the first joint, and
- a second end;
- and
- an additional plateau that is movably attached to the second end of the third element at a fifth joint and adapted to be attached to the component, wherein the first and third elements together with the plateau and the additional plateau form a guide bracket that is adapted to guide movement of the internally threaded fastener along the externally threaded shaft.
A helicopter comprising:
- a fuselage;
- an external load device connected to the fuselage via a component;
- and
- a power transmission system adapted to transmit forces from a motor that generates a first rotational movement to the component, the power transmission system comprising:
- an externally threaded shaft rotatably attached to the motor and capable of performing a second rotational movement;
- an internally threaded fastener movably attached to the externally threaded shaft and capable of performing a movement along the externally threaded shaft in response to the second rotational movement;
- a first element comprising:
- a first end movably attached to the internally threaded fastener at a first joint, and
- a second end;
- and
- a second element comprising:
- a plateau having a first end and a second end, the first end movably attached to the second end of the first element at a second joint to enable the first element to transmit the forces from the first joint to the second joint, and
- the second end adapted to be rigidly attached to the component at a third joint to enable the plateau to transmit the forces from the second joint to the third joint by transforming a rotational movement of the second joint into a rotation of the component.
Dependencies are inferred from the claim text.