G01B17/00

System and method for hitch angle detection

A hitch angle detection system is provided herein. Ultrasonic transducers are disposed on a rear vehicle structure and are configured to transmit ultrasonic waves in a rearward vehicle direction. An ultrasonic reflector is disposed on a trailer and is configured to reflect incident ultrasonic waves back toward the corresponding ultrasonic transducers. A processor is configured to derive distance measurements between the ultrasonic transducers and the ultrasonic reflector and determine a hitch angle based on the derived distance measurements.

System and method for hitch angle detection

A hitch angle detection system is provided herein. Ultrasonic transducers are disposed on a rear vehicle structure and are configured to transmit ultrasonic waves in a rearward vehicle direction. An ultrasonic reflector is disposed on a trailer and is configured to reflect incident ultrasonic waves back toward the corresponding ultrasonic transducers. A processor is configured to derive distance measurements between the ultrasonic transducers and the ultrasonic reflector and determine a hitch angle based on the derived distance measurements.

METHOD FOR DETERMINING ANGULAR POSITIONS OF MULTIPLE COMPRESSOR GUIDE VANES
20170306789 · 2017-10-26 · ·

A method is for determining the angular positions of multiple compressor guide vanes. The method includes measuring the positions of at least two points on the circumference of the actuating ring, via at least two linear position sensors fixed on the compressor casing, and pointing at the actuating ring vertically at a time when the actuating ring deviates from its original position where the ring center coincides with the casing center; calculating the ring center offset based on the measured positions of the at least two points and the radius of the actuating ring; measuring the angle of one of the multiple guide vanes at the same time when measuring the positions of the at least two points; and calculating the angles of the multiple guide vanes based on the ring center offset and the angle of the guide vane. An actuation apparatus for multiple compressor guide vanes is included.

METHOD FOR DETERMINING ANGULAR POSITIONS OF MULTIPLE COMPRESSOR GUIDE VANES
20170306789 · 2017-10-26 · ·

A method is for determining the angular positions of multiple compressor guide vanes. The method includes measuring the positions of at least two points on the circumference of the actuating ring, via at least two linear position sensors fixed on the compressor casing, and pointing at the actuating ring vertically at a time when the actuating ring deviates from its original position where the ring center coincides with the casing center; calculating the ring center offset based on the measured positions of the at least two points and the radius of the actuating ring; measuring the angle of one of the multiple guide vanes at the same time when measuring the positions of the at least two points; and calculating the angles of the multiple guide vanes based on the ring center offset and the angle of the guide vane. An actuation apparatus for multiple compressor guide vanes is included.

Ultrasonic Inspection of Wrinkles in Composite Objects
20170299381 · 2017-10-19 ·

A method and apparatus for evaluating an object having a wrinkle are provided. An array of receiving elements is configured such that only two receiving apertures are configured to receive at a given point in time. Energy is sent into the object using an array of transmitting elements. Reflected energy is received at the only two receiving apertures of the array of receiving elements in response to a portion of the energy being reflected off a plurality of layers in the object. A number of dimensions of a wrinkle in the object is determined based on the reflected energy received at the only two receiving apertures of the array of receiving elements.

Ultrasonic Inspection of Wrinkles in Composite Objects
20170299381 · 2017-10-19 ·

A method and apparatus for evaluating an object having a wrinkle are provided. An array of receiving elements is configured such that only two receiving apertures are configured to receive at a given point in time. Energy is sent into the object using an array of transmitting elements. Reflected energy is received at the only two receiving apertures of the array of receiving elements in response to a portion of the energy being reflected off a plurality of layers in the object. A number of dimensions of a wrinkle in the object is determined based on the reflected energy received at the only two receiving apertures of the array of receiving elements.

DEVICE AND METHOD FOR TESTING IMPEDANCE CHARACTERISTIC AND EXPANSION PERFORMANCE OF SOUND ABSORPTION MATERIAL
20170276540 · 2017-09-28 · ·

Disclosed are a device and a method for testing impedance characteristic and expansion performance of a sound absorption material. The device includes a first cavity and a second cavity which are both sealed. The first cavity is communicated with the second cavity through a slit channel. The second cavity is used for placing a sound absorption material therein. The device further includes a sound excitation source whose sounding face is located in the first cavity and used to provide a testing sound pressure. The device further includes two sound pickup sensors whose sound pickup surfaces are respectively arranged in the first cavity and the second cavity and respectively used to detect sound pressure in the first cavity and the second cavity. The device further includes a material for enclosing the first cavity and the second cavity is a hard sound insulation material.

DEVICE AND METHOD FOR TESTING IMPEDANCE CHARACTERISTIC AND EXPANSION PERFORMANCE OF SOUND ABSORPTION MATERIAL
20170276540 · 2017-09-28 · ·

Disclosed are a device and a method for testing impedance characteristic and expansion performance of a sound absorption material. The device includes a first cavity and a second cavity which are both sealed. The first cavity is communicated with the second cavity through a slit channel. The second cavity is used for placing a sound absorption material therein. The device further includes a sound excitation source whose sounding face is located in the first cavity and used to provide a testing sound pressure. The device further includes two sound pickup sensors whose sound pickup surfaces are respectively arranged in the first cavity and the second cavity and respectively used to detect sound pressure in the first cavity and the second cavity. The device further includes a material for enclosing the first cavity and the second cavity is a hard sound insulation material.

Round bale weighing method and system

Yield monitoring systems for round baling machines and methods that can provide weight estimations for round bales at the time of formation are described. Balers can include those that incorporate hydraulically actuated bale kicking or pushing assemblies as well as those that incorporate spring-loaded off ramps. Farm implements including baling machines and cotton module builders are encompassed. The system includes a sensor that can ascertain a physical parameter associated with ejection of a round bale from the farm implement. Physical parameters as may be ascertained can include pressures, velocities, accelerations, etc. associated with bale ejection.

DEVICE AND METHOD FOR CONTROLLED EMISSION OF RADIATION
20220034649 · 2022-02-03 ·

Embodiments of present disclosure relates to method and device for controlled emission of radiation. Device comprises probe unit, sensor unit and switch unit. Probe unit is configured to emit radiation on surface of object. Probe unit is supported, via an elastic, to supporting structure of device. Sensor unit is placed at predefined distance from probe unit, along supporting structure, to establish contact with surface. Sensor unit comprises flexible material, mounted to supporting structure, with cavity and first force sensing unit placed in cavity of flexible material. First force sensing unit is configured to detect first force transferred from surface sensor unit. Switch unit is configured to control emission of radiation on surface, based on first force detected by first force sensing unit, upon contact of sensor unit with surface and identification of probe unit to be one of in contact with surface or at minimal distance from surface.