Device for determining the rotation angle of a shaft in an aircraft
AssigneeAirbus Deutschland GmbH
InventorJoern Rennhack
Life of this patent
Estimating the term…
Abstract
A device for determining the rotation angle of a shaft in an aircraft, the device having a shaft and a motor operable to rotate the shaft to operate a component and to detect first rotation data of the shaft. The device also includes a position pickup unit designed to detect second rotation data of the shaft, and a synchronization unit for synchronizing the first rotation data with the second rotation data.
Claims12
An aircraft having a device for determining the rotation angle of a shaft in the aircraft, the device comprising:
- a shaft designed for operating a component, the component selected from the group consisting of a brake flap, a landing flap, a landing slat, a rudder, an aileron and an elevator, the shaft having a first region and a second region,
- a motor which rotates the shaft to detect first rotation data corresponding to a first rotation angle of the first region of the shaft, the motor being designed to carry out said detection in an absolute manner;
- a position pickup unit designed to detect second rotation data corresponding to a second rotation angle of the second region of the shaft;
- a synchronization unit designed to synchronize the first rotation data with the second rotation data;
- and
- a control unit designed to provide a calibration procedure which determines a zero point of the motor on the basis of the second rotation data provided by the position pickup unit.
An aircraft having a device for determining the rotation angle of a shaft in the aircraft, the device comprising:
- a shaft designed for operating a component the component selected from the group consisting of a brake flap, a landing flap, a landing slat, a rudder, an aileron and an elevator, the shaft having a first region and a second region,
- a motor which rotates the shaft to detect first rotation data corresponding to a first rotation angle of the first region of the shaft, the motor being designed to carry out said detection in an absolute manner;
- a position pickup unit designed to detect second rotation data corresponding to a second rotation angle of the second region of the shaft;
- a synchronization unit designed to synchronize the first rotation data with the second rotation data;
- and
- a control unit designed to detect and evaluate an incorrectness of the second rotation data provided by the position pickup unit on the basis of the first rotation data.
A method for determining the rotation angle of a shaft in an aircraft, comprising the steps of:
- rotating the shaft by a motor;
- detecting first rotation data that corresponds to a first rotation angle of a first region of the shaft by the motor in an absolute manner;
- detecting second rotation data that corresponds to a second rotation angle of a second region of the shaft by a position pickup unit;
- transmitting the first rotation data from the motor to a control unit;
- transmitting the second rotation data from the position pickup unit to the control unit;
- determining a zero point of the motor on the basis of the second rotation data provided by the position pickup unit;
- synchronizing the first rotation data with the second rotation data;
- and
- controlling or regulating the rotation of the shaft on the basis of the transmitted first and second rotation data by the control unit.
A method for determining the rotation angle of a shaft in a aircraft, comprising the steps of:
- rotating the shaft by a motor;
- detecting first rotation data that corresponds to a first rotation angle of a first region of the shaft by the motor in an absolute manner;
- detecting second rotation data that corresponds to a second rotation angle of a second region of the shaft by a position pickup unit;
- transmitting the first rotation data from the motor to a control unit;
- transmitting the second rotation data from the position pickup unit to the control unit;
- detecting and evaluating an incorrectness of the second rotation data provided by the position pickup unit on the basis of the first rotation data;
- synchronizing the first rotation data with the second rotation data;
- and
- controlling or regulating the rotation of the shaft on the basis of the transmitted first and second rotation data by the control unit.
Dependencies are inferred from the claim text.