A bearing diagnostic device senses a failure in a bearing of a machine tool including a rotation shaft device. The bearing diagnostic device includes a rotation counting unit, a temperature measuring unit, a frictional torque calculating unit, a rolling speed calculating unit, a bearing characteristic calculating unit, a storage unit, and a determination unit. The frictional torque calculating unit is configured to calculate a frictional torque of the rotation shaft device. The rolling speed calculating unit is configured to calculate a rolling speed of the bearing from the count of rotations. The bearing characteristic calculating unit is configured to calculate a bearing characteristic from the frictional torque and the rolling speed. The determination unit is configured to compare the bearing characteristic calculated by the bearing characteristic calculating unit with a reference bearing characteristic stored in the storage unit to determine a presence of a failure.

A lubrication detection method includes a first step is a lubricator provides an information to a processor, a second step is to detect temperature information within a predetermined time period and then to create a temperature curve and then to determine whether or not the recess in the temperature curve faces upward, and a third step of detecting a start point temperature value to form Value A, and averaging temperature values within time period in front of the lowest point to form Value B, and average temperature values after time period in back of the lowest point to form Value C, and determining whether or not Value B is smaller than Value A, and then determining whether or not Value B is smaller than Value C, and then generating an information of Normal indicative of normal lubrication.

This grease application device includes: a nozzle body that has a first end portion insertable into an inner spline portion, the inner spline portion being formed at an end portion of a workpiece; a nozzle that is formed on the first end portion of the nozzle body and discharges grease into a groove of the inner spline portion; a nozzle body shift portion that is connected to a second end portion of the nozzle body and that moves the nozzle body in a longitudinal direction, the second end portion being on an opposite side to the first end portion; a grease retention portion that retains the grease discharged from the nozzle; a grease pressure-feed portion that pressure-feeds the grease retained in the grease retention portion to the nozzle; and an operation portion that links an operation of causing the nozzle body shift portion to move the nozzle body from the first end portion toward the second end portion with an operation of causing the grease pressure-feed portion to discharge the grease from the nozzle.

An oil mist management system includes a machine tool, an oil mist concentration measuring apparatus for measuring concentration of oil mist, and a flow meter for detecting the flow rate of coolant, in each of a plurality of areas. A data processing apparatus determines whether distribution of the oil mist in the plurality of areas is normal or abnormal on an area-by-area basis, based on the concentration of the oil mist and the flow rate of coolant in each of the plurality of areas, and identifies an abnormal area. Further, the oil mist management system notifies a user of the abnormal area by an output device.

A method of distributing oil to a component within a gas turbine engine includes directing a first oil flow from an oil source to an engine component and back to the oil source, directing a second oil flow from the oil source to a generator driven by the engine and back to the oil source, monitoring a parameter of the second oil flow downstream of the generator and upstream of the oil source, detecting a contaminant in the second oil flow based on the parameter, and reducing the second oil flow to the generator when the contaminant is detected without reducing the first oil flow to the engine component. A shared oil system for a component of a gas turbine engine and a generator driven by the gas turbine engine is also discussed.

A debris monitoring system has a first sensor configured to generate a first signal indicating a presence of a metallic particle in a lubrication system. A second sensor is configured to generate a second signal indicating the presence of a metallic particle in the lubrication system. A signal processor is configured to determine a presence of a metallic particle in a fluid passage based on a comparison of at least the first signal and the second signal; the second signal being used to verify accuracy of the first signal. A gas turbine engine and a method for monitoring a fluid passage for debris are also disclosed.

There is described herein methods and systems for detecting of metallic chips in a fluid system of an aircraft engine. The method comprises measuring a resistance value across a magnetic chip detector mounted to a fluid system of the aircraft engine and transmitting the resistance value to an engine computer of the aircraft engine. The method further comprises, in the engine computer, comparing the resistance value to a first threshold and issuing a first warning indicative of a chip in the fluid when the resistance value exceeds the first threshold.

A method of detecting debris within a lubricant stream, the method includes generating data indicative of debris and sensor system functionality within a lubricant stream with a sensor system. The data is communicated to a controller. Features calculated from the data are indicative of a debris within the lubricant stream. The calculated features are compiled over time during operation. The compiled features are classified. An oil debris monitoring system for a turbine engine is also disclosed.

A method for monitoring a lubricant throughflow of a centrifuge is monitored involves rotating the drive shaft with the motor and simultaneously operating the lubricant supply to generate a lubricant throughflow through the bearing arrangement and monitoring a temperature of the lubricant throughflow through the bearing arrangement at at least one measurement point at or in the device for supplying lubricant.

A method for monitoring a lubricant throughflow of a centrifuge is monitored involves rotating the drive shaft with the motor and simultaneously operating the lubricant supply to generate a lubricant throughflow through the bearing arrangement and monitoring a temperature of the lubricant throughflow through the bearing arrangement at at least one measurement point at or in the device for supplying lubricant.