G01G19/12

System and method for handling lost item in autonomous vehicle

A system for handling a lost item in an autonomous vehicle and a server. The vehicle includes a vision sensor configured to respectively capture a first vehicle interior image and a second vehicle interior image when a passenger boards and alights from the vehicle. The vehicle is configured to transmit the captured first vehicle interior image and second vehicle interior image to the server. The server is configured to compare the first vehicle interior image with the second vehicle interior image and transmit lost item information to the passenger when the lost item in the vehicle is sensed.

WEIGHT MEASURING HITCH BALL ASSEMBLY INCLUDING LOW PROFILE HITCH BALL ASSEMBLIES FOR MEASURING WEIGHT OF A TRAILER SUPPORTED BY A TOW VEHICLE
20220363096 · 2022-11-17 · ·

A weight measuring hitch ball assembly is described. The assembly can include a hitch ball having a ball and a lower portion. The assembly can also include a body portion defining a hitch ball opening that slidably receives the lower portion of the hitch ball. The assembly can further include a load measurement device operably associated with the body portion and the hitch ball to determine a magnitude of a force acting on the hitch ball. Additionally, the assembly can include a hitch mount interface configured to interface with an attachment structure that facilitates coupling the weight measuring hitch ball assembly to a tow vehicle.

WEIGHT MEASURING HITCH BALL ASSEMBLY INCLUDING LOW PROFILE HITCH BALL ASSEMBLIES FOR MEASURING WEIGHT OF A TRAILER SUPPORTED BY A TOW VEHICLE
20220363096 · 2022-11-17 · ·

A weight measuring hitch ball assembly is described. The assembly can include a hitch ball having a ball and a lower portion. The assembly can also include a body portion defining a hitch ball opening that slidably receives the lower portion of the hitch ball. The assembly can further include a load measurement device operably associated with the body portion and the hitch ball to determine a magnitude of a force acting on the hitch ball. Additionally, the assembly can include a hitch mount interface configured to interface with an attachment structure that facilitates coupling the weight measuring hitch ball assembly to a tow vehicle.

Load sensor system with improved assembly connection
11614372 · 2023-03-28 · ·

A load sensor having a centrally disposed aperture element through which a fastening element of a vehicle air suspension assembly passes to affix the load sensor between the vehicle air suspension assembly and the vehicle suspension, wherein the load sensor has a force measurement sensor disposed proximate an elongate slot to generate a load signal which varies based on an amount of strain in the load sensor, wherein the load signal received by a load calculator allows calculation of the load exerted from the vehicle frame to the vehicle suspension.

Load sensor system with improved assembly connection
11614372 · 2023-03-28 · ·

A load sensor having a centrally disposed aperture element through which a fastening element of a vehicle air suspension assembly passes to affix the load sensor between the vehicle air suspension assembly and the vehicle suspension, wherein the load sensor has a force measurement sensor disposed proximate an elongate slot to generate a load signal which varies based on an amount of strain in the load sensor, wherein the load signal received by a load calculator allows calculation of the load exerted from the vehicle frame to the vehicle suspension.

System for Monitoring a Payload, Aircraft and Method
20220340297 · 2022-10-27 ·

The invention relates to a payload monitoring system of an aircraft, wherein the system comprises at least one storage area (26, 28, 30, 32, 36, 38, 42) for a payload and at least one pressure sensor (10), wherein the at least one sensor (10) is configured to detect a weight force and its center of gravity of payload resting on the storage area (26, 28, 30, 32, 36, 38, 42). Furthermore, the invention relates to an aircraft and a method for operating an aircraft.

System for Monitoring a Payload, Aircraft and Method
20220340297 · 2022-10-27 ·

The invention relates to a payload monitoring system of an aircraft, wherein the system comprises at least one storage area (26, 28, 30, 32, 36, 38, 42) for a payload and at least one pressure sensor (10), wherein the at least one sensor (10) is configured to detect a weight force and its center of gravity of payload resting on the storage area (26, 28, 30, 32, 36, 38, 42). Furthermore, the invention relates to an aircraft and a method for operating an aircraft.

TELESCOPING/WEIGHING FORK COMBINATION
20230085508 · 2023-03-16 · ·

A telescoping weigh fork unit where a base fork has an integrated hydraulic cylinder and a slideable outer shoe on which are supported at least two load cells. Optionally the unit may include an outside telescopic fork shoe to which the load cells are mounted and which supports the outer shoe. Unit may further include a system to alert if distance or weight thresholds are exceeded or if a load cell is inoperable.

TELESCOPING/WEIGHING FORK COMBINATION
20230085508 · 2023-03-16 · ·

A telescoping weigh fork unit where a base fork has an integrated hydraulic cylinder and a slideable outer shoe on which are supported at least two load cells. Optionally the unit may include an outside telescopic fork shoe to which the load cells are mounted and which supports the outer shoe. Unit may further include a system to alert if distance or weight thresholds are exceeded or if a load cell is inoperable.

Elevator car load measurement system and method for determining a load of an elevator car
11603285 · 2023-03-14 · ·

An elevator car load measurement system for determining a load of an elevator car includes a plurality of at least two force sensors that are daisy-chained and connected to a controller for determining the load. Each force sensor measures a force exerted by the elevator car on the respective force sensor and generates a frequency signal with a square-wave form, wherein the frequency signal is proportional to the respective measured force. At least one of the force sensors adds a first frequency signal received from the previous force sensor along the daisy chain a second frequency signal generated by the at least one force sensor to generate a frequency sum signal, the last of the force sensors in the daisy chain forwards the frequency sum signal to the controller.