Systems and methods for determining a throttle position of an aircraft are described herein. A first throttle position is obtained from a first sensor, a second throttle position is obtained from a second sensor, and a third throttle position is obtained from a third sensor. The first, second, and third sensors are separately coupled to a throttle of the aircraft for obtaining independent throttle position measurements therefrom. A difference between the first throttle position and the second throttle position is determined. A mismatch is detected when the difference between the first throttle position and the second throttle position exceeds a threshold. A valid one of the first throttle position and the second throttle position is selected based on the third throttle position, in response to detecting the mismatch. A signal indicative of the throttle position is outputted based on the valid one of the first throttle position and the second throttle position.

The invention relates to a method for identifying a fault (96) in an angle sensor (24) which is designed to determine the angular position (18) of a shaft (14) based on an angular position difference (56) between a first output gear (32), which is driven by the shaft (14), and a second output gear (34), which is driven by the shaft (14), the output gears differing in respect of their diameter (34, 36), said method comprising: determining a reference value (18, 52) for the angular position (18) of the shaft (14) based on the angular position (42) of the first output gear (32), determining a comparison value (18′, 52′) for the angular position (18) of the shaft (14) based on the angular position (46) of the second output gear (34) and a transmission ratio (90) between the first output gear (32) and the second output gear (34), and identifying the fault (96) when a comparison (93, 94) of the reference value (18, 52) and the comparison value (18′, 52′) satisfies a predetermined condition (95).

The invention relates to a method for identifying a fault (96) in an angle sensor (24) which is designed to determine the angular position (18) of a shaft (14) based on an angular position difference (56) between a first output gear (32), which is driven by the shaft (14), and a second output gear (34), which is driven by the shaft (14), the output gears differing in respect of their diameter (34, 36), said method comprising: determining a reference value (18, 52) for the angular position (18) of the shaft (14) based on the angular position (42) of the first output gear (32), determining a comparison value (18′, 52′) for the angular position (18) of the shaft (14) based on the angular position (46) of the second output gear (34) and a transmission ratio (90) between the first output gear (32) and the second output gear (34), and identifying the fault (96) when a comparison (93, 94) of the reference value (18, 52) and the comparison value (18′, 52′) satisfies a predetermined condition (95).

Positioner assemblies may be configured to sense at least one position of at least a portion of a valve assembly that is moved along a first axis of movement. A movable element of the positioner assembly is configured to rotate about a second axis of movement, where the first axis of movement is substantially parallel to the second axis of movement. Valve systems and methods of sensing a position of a component of a valve system may include such a positioner assembly.

Positioner assemblies may be configured to sense at least one position of at least a portion of a valve assembly that is moved along a first axis of movement. A movable element of the positioner assembly is configured to rotate about a second axis of movement, where the first axis of movement is substantially parallel to the second axis of movement. Valve systems and methods of sensing a position of a component of a valve system may include such a positioner assembly.

The system of the present disclosure replaces the reduction gearbox of a conventional system with a screw shaft and nut system wherein the position of the nut feeds into a linear sensor that determines the stabilizer position based on the nut position. The screw shaft and nut system in the position sensor train is reflective of the screw shaft and nut system and the stabilizer movement end of the assembly whereby rotation of the shaft causes axial movement of the nut along the shaft.

The system of the present disclosure replaces the reduction gearbox of a conventional system with a screw shaft and nut system wherein the position of the nut feeds into a linear sensor that determines the stabilizer position based on the nut position. The screw shaft and nut system in the position sensor train is reflective of the screw shaft and nut system and the stabilizer movement end of the assembly whereby rotation of the shaft causes axial movement of the nut along the shaft.

The present disclosure relates to a magnetic sensor arrangement comprising a first rotatable body having a first magnetic quadrupole attached thereto, a first magnetic sensor configured to generate, in response to a rotational angular position of the first magnetic quadrupole, a first sensor signal indicative of a first rotational angle of the first rotatable body, a second rotatable body having a second magnetic quadrupole attached thereto, and a second magnetic sensor configured to generate, in response to a rotational angular position of the second magnetic quadrupole, a second sensor signal indicative of a second rotational angle of the second rotatable body.

The present disclosure relates to a magnetic sensor arrangement comprising a first rotatable body having a first magnetic quadrupole attached thereto, a first magnetic sensor configured to generate, in response to a rotational angular position of the first magnetic quadrupole, a first sensor signal indicative of a first rotational angle of the first rotatable body, a second rotatable body having a second magnetic quadrupole attached thereto, and a second magnetic sensor configured to generate, in response to a rotational angular position of the second magnetic quadrupole, a second sensor signal indicative of a second rotational angle of the second rotatable body.

Locating apparatus for machine tool including supporting portion for placing at fixed point on object's machining surface, detector including cable to connect apparatus with machine, and locating portion to release or receive cable to measure distance between machine and apparatus and including frame, first device, second device and third device. First device attached to the frame and for receiving or releasing cable in opposition to or pushed by elastic element. Second device attached to frame and includes transmission member to allow the cable passage. Third device attached to frame and allows cable release or reception by apparatus towards machine. First device includes discoidal element rotating around axis of rotation respective to frame to wind or release cable on winding surface. Second device includes guiding slider for conveying cable along conveying direction and moving along translation direction parallel to axis of rotation in proportion to discoidal element rotation.