Described herein is a weight or pressure measuring shovel. The shoveling apparatus has a broad blade assembly or scoop assembly including an elongate handle member. A coupler assembly is designed to couple the curved plate assembly to allow angular orientation or movement of the curved plate assembly to be adjusted relative to the handle member. A force transducer converts the weight or pressure of a material on the curved plate assembly into an electrical signal designed to communicate the weight or pressure of a material such as snow, sand, dirt, or ice. A control module in a housing mounted on the elongate handle is designed to receive electrical signals from the force transducer assembly or a load cell assembly. A display assembly is coupled to the electrical scale assembly and control module.

The present invention relates to the technical field of systems for measurement of weight load and other physical variables in vehicles and/or containers, comprising a system of sensing and monitoring of their conditions, instantaneous or not. Consists of an external data collection subsystem (SSI) with module with sensing network (1), signal transduction module (2) and connection module (3); of a data processing and reading subsystem (SSII) with energizing module (4); reading and data acquisition module (5); processing and memory module (6); and data transmission subsystem (SSIII) with data communication module (7). The system has advantages, does not present false sensor measurements, that allow wide multiplexing, no electricity, high signal and there is no electromagnetic interference, they are robust, do not suffer corrosion and do not fail due to vibration and mechanical impacts.

A weight measuring apparatus for vehicles includes a measuring plate on which an object to be measured is placed; a plurality of entry members installed on the measuring plate; and a load cell having one side fixed to the entry member and the other side fixed to the measuring plate, wherein the entry members are installed apart from each other at the edge of the measuring plate. A weight measuring apparatus for vehicles with which a vehicle is easy to enter thereby measuring the weight of the vehicle conveniently, of which structure is simple and light thereby improving the usability and handling thereof, of which cost for manufacturing can be reduced, of which supporting structure is stable and reinforced with structural strength thereby improving durability and safety, and that can measure load weight accurately.

A method for controlling an electronic scale in disclosed in this disclosure, which is applied to measure and indicate a state of an external force, comprises the following steps. A weight sensor detects the external force, and a controller drives a prompting device to emit a first light with a first optical characteristic when the external force detected by the weight sensor reaches a first weight. The controller drives the prompting device to emit a second light with a second optical characteristic when the prompting device emits the first light for a predetermined period, wherein the prompting device continuously emits the second light until the external force reaches a second weight.

A method for controlling an electronic scale in disclosed in this disclosure, which is applied to measure and indicate a state of an external force, comprises the following steps. A weight sensor detects the external force, and a controller drives a prompting device to emit a first light with a first optical characteristic when the external force detected by the weight sensor reaches a first weight. The controller drives the prompting device to emit a second light with a second optical characteristic when the prompting device emits the first light for a predetermined period, wherein the prompting device continuously emits the second light until the external force reaches a second weight.

The invention relates to a kitchen scale comprising a carrying plate (1), a substructure (2) supporting the carrying plate, weighing cells (6) comprising at least one strain gauge (10), an electronics unit (4), which is capable of computing the weight of the load, and comprising a display device for displaying the ascertained weight and a battery compartment for accommodating a voltage source which supplies the electronics unit (4) with power. The weighing cell (6) has at least one strain gauge, which is at least partially provided with a parylene coating.

A system includes a signal generator that is configured to generate a first electrical signal. The system also includes a light source configured to generate a light beam based on the first electrical signal. The light source is also configured to direct the light beam towards a structural member of an aircraft. The system also includes a photoelectric sensor configured to receive a reflected light beam and convert the reflected light beam to a second electrical signal. The reflected light beam corresponds to a portion of the light beam that is reflected from one or more optical reflectors coupled to the structural member. The system also includes circuitry configured to estimate a location of a center-of-gravity of the aircraft based on a timing difference between the first electrical signal and the second electrical signal.

The present invention relates to the technical field of systems for measurement of weight load and other physical variables in vehicles and/or containers, comprising a system of sensing and monitoring of their conditions, instantaneous or not. Consists of an external data collection subsystem (SSI) with module with sensing network (1), signal transduction module (2) and connection module (3); of a data processing and reading subsystem (SSII) with energizing module (4); reading and data acquisition module (5); processing and memory module (6); and data transmission subsystem (SSIII) with data communication module (7). The system has advantages, does not present false sensor measurements, that allow wide multiplexing, no electricity, high signal and there is no electromagnetic interference, they are robust, do not suffer corrosion and do not fail due to vibration and mechanical impacts.

A method for controlling an electronic scale in disclosed in this disclosure, which is applied to measure and indicate a state of an external force, comprises the following steps. A weight sensor detects the external force, and a controller drives a prompting device to emit a first light with a first optical characteristic when the external force detected by the weight sensor reaches a first weight. The controller drives the prompting device to emit a second light with a second optical characteristic when the prompting device emits the first light for a predetermined period, wherein the prompting device continuously emits the second light until the external force reaches a second weight.

A system includes a signal generator that is configured to generate a first electrical signal. The system also includes a light source configured to generate a light beam based on the first electrical signal. The light source is also configured to direct the light beam towards a structural member of an aircraft. The system also includes a photoelectric sensor configured to receive a reflected light beam and convert the reflected light beam to a second electrical signal. The reflected light beam corresponds to a portion of the light beam that is reflected from one or more optical reflectors coupled to the structural member. The system also includes circuitry configured to estimate a location of a center-of-gravity of the aircraft based on a timing difference between the first electrical signal and the second electrical signal.