Abstract: An oil control ring comprises: an oil ring having a pair of land parts arranged in a sliding direction and connected to each other by a web part; and a coil expander that biases the oil ring toward the outer circumferential side in the radial direction. The web part of the oil ring is provided with a plurality of window holes. In the axial cross-sectional view of the largest opening portion of the window hole in the axial direction of the oil ring, a width H1 in the sliding direction of the oil ring and a length L1 of a combustion chamber-side non-window hole part, which excludes the window hole, in the outer circumferential surface of the web part, satisfy the condition of 0.15>L1/H1?0.

Abstract: A system including an airbag assembly for a vehicle is disclosed. The airbag assembly includes a housing supporting the airbag, an inflation device (“inflator”) in fluid communication with the airbag for inflating the airbag from an uninflated position to an inflated position, a tether fixed to the airbag that helps control the deployment and inflation of the airbag, and a tether lid configured to open in order to release the tether during deployment. The tether lid is installed in a pillar garnish of the vehicle, and is opened in response to the force of the tether as it is pulled by the deploying airbag.

Abstract: A triple containment tank includes: a tank foundation; a triple shell including an outer tank, an intermediate tank, and an inner tank; a first anchor strap extending through a first inter-tank region and a second inter-tank region and coupling an inner tank side plate and the tank foundation; and a second anchor strap extending through the second inter-tank region and coupling an intermediate tank side plate and the tank foundation. The first anchor strap includes: a first end portion coupled to the inner tank side plate; a second end portion coupled to the tank foundation; a first intermediate portion located between the first end portion and the second end portion and coupled to an inner wall-side portion of the intermediate tank; and a second intermediate portion located between the first end portion and the second end portion and coupled to an outer wall-side portion of the intermediate tank.

Abstract: A device for measuring the dynamic matrix sensitivity of an inertia sensor is provided with a motion generating machine or a vibrating table for inducing a translational or rotary motion, an acceleration measuring unit, an angular velocity measuring unit or angular acceleration measuring unit, an output device for fetching an output from the unit, one or, pre light reflectors, a displacement measuring device for seizing a multidimensional motion by using a laser interferometer radiating light from a plurality of directions to the light reflectors, a data processing unit for processing a data indicating the state of motion and obtained from the displacement measuring unit, and a displaying device to display or a transmitting device to transmit the output of the data processing unit and the output of the acceleration measuring unit, angular velocity measuring unit or angular acceleration measuring unit.

Abstract: A sensor obtains transverse sensitivity in a sensitivity matrix of an acceleration sensor with a uniaxial vibration generator. The acceleration is measured by vibrating the table 12. As the measurement of the main axis sensitivity, transverse sensitivity Szx associated with the X-axis is obtained from measured results of the acceleration sensor 5 and measured results of a measuring instrument for measuring the surface motion of the table 12 independently. Likewise, transverse sensitivity Szy associated with the Y-axis is obtained by fixing on the table 12 the cubical block on which the acceleration sensor 5 is mounted in such a manner that the Y-axis direction defined with respect to the acceleration sensor 5 aligns with the vibration direction of the table 12.

Abstract: An elastic wave pulse is generated in a metal rod (1) by impacting an end surface (2) of the metal rod with each of two round, concentric projectiles (8, 10) from a double launch tube (4, 5) independently, and by impacting both projectiles simultaneously or at a prescribed time interval. An acceleration sensor (23) is provided on another end surface (22) of the metal rod to measure an acceleration of the other end surface arising when the elastic wave pulse generated by the impact of the projectiles reflects at the other end surface. The motion of the end surface is measured by a laser interferometer (24) or by a strain gauge (25) provided on a side surface of the metal rod, and the measured signals are calculated and corrected as appropriate. The dynamic linearity of the acceleration sensor is obtained by comparing in time domain and frequency domain the calculated results with the measured values of the acceleration sensor.

Abstract: A metal rod guide (30) supports a metal rod (1) that can be inclined at an arbitrary angle, the support is instantaneously released to produce a free fall state, and during the release period, a first end surface (2) of the metal rod is impacted by a projectile (3) at the same angle as the metal rod, generating an elastic wave pulse in the metal rod. A direct current acceleration sensor (23) detects an acceleration arising when the elastic wave pulse reflects at the other end surface (22) of the metal rod. A strain gauge (25) provided on a side surface of the metal rod and/or a laser interferometer (24) measure strain and end surface motion and the measured values are processed to obtain a frequency response of the direct current acceleration sensor and measure frequency characteristics of the direct current acceleration sensor.

Abstract: A sensor obtains transverse sensitivity in a sensitivity matrix of an acceleration sensor with a uniaxial vibration generator. The acceleration is measured by vibrating the table 12. As the measurement of the main axis sensitivity, transverse sensitivity Szx associated with the X-axis is obtained from measured results of the acceleration sensor 5 and measured results of a measuring instrument for measuring the surface motion of the table 12 independently. Likewise, transverse sensitivity Szy associated with the Y-axis is obtained by fixing on the table 12 the cubical block on which the acceleration sensor 5 is mounted in such a manner that the Y-axis direction defined with respect to the acceleration sensor 5 aligns with the vibration direction of the table 12.

Abstract: A device for measuring the dynamic matrix sensitivity of an inertia sensor is provided with a motion generating machine or a vibrating table for inducing a translational or rotary motion, an acceleration measuring unit, an angular velocity measuring unit or angular acceleration measuring unit, an output device for fetching an output from the unit, one or, pre light reflectors, a displacement measuring device for seizing a multidimensional motion by using a laser interferometer radiating light from a plurality of directions to the light reflectors, a data processing unit for processing a data indicating the state of motion and obtained from the displacement measuring unit, and a displaying device to display or a transmitting device to transmit the output of the data processing unit and the output of the acceleration measuring unit, angular velocity measuring unit or angular acceleration measuring unit.

Abstract: A metal rod guide (30) supports a metal rod (1) that can be inclined at an arbitrary angle, the support is instantaneously released to produce a free fall state, and during the release period, a first end surface (2) of the metal rod is impacted by a projectile (3) at the same angle as the metal rod, generating an elastic wave pulse in the metal rod. A direct current acceleration sensor (23) detects an acceleration arising when the elastic wave pulse reflects at the other end surface (22) of the metal rod. A strain gauge (25) provided on a side surface of the metal rod and/or a laser interferometer (24) measure strain and end surface motion and the measured values are processed to obtain a frequency response of the direct current acceleration sensor and measure frequency characteristics of the direct current acceleration sensor.

Abstract: A metal rod guide (30) supports a metal rod (1) that can be inclined at an arbitrary angle, the support is instantaneously released to produce a free fall state, and during the release period, a first end surface (2) of the metal rod is impacted by a projectile (3) at the same angle as the metal rod, generating an elastic wave pulse in the metal rod. A direct current acceleration sensor (23) detects an acceleration arising when the elastic wave pulse reflects at the other end surface (22) of the metal rod. A strain gauge (25) provided on a side surface of the metal rod and/or a laser interferometer (24) measure strain and end surface motion and the measured values are processed to obtain a frequency response of the direct current acceleration sensor and measure frequency characteristics of the direct current acceleration sensor.

Abstract: A metal rod guide (30) supports a metal rod (1) that can be inclined at an arbitrary angle, the support is instantaneously released to produce a free fall state, and during the release period, a first end surface (2) of the metal rod is impacted by a projectile (3) at the same angle as the metal rod, generating an elastic wave pulse in the metal rod. A direct current acceleration sensor (23) detects an acceleration arising when the elastic wave pulse reflects at the other end surface (22) of the metal rod. A strain gauge (25) provided on a side surface of the metal rod and/or a laser interferometer (24) measure strain and end surface motion and the measured values are processed to obtain a frequency response of the direct current acceleration sensor and measure frequency characteristics of the direct current acceleration sensor.

Abstract: An acceleration sensor (22) to be calibrated and evaluated is affixed to one end surface (22) of a metal rod (1), and a plurality of projectiles (3) are made to impact the other end surface (2) of the metal rod at prescribed time intervals, generating an elastic wave pulse in the metal rod. Dynamic displacement, velocity or acceleration in a direction normal to the other end surface arising in a process of the generated elastic wave pulse reaching and being reflected by the one end surface where the acceleration sensor is affixed is measured, and an acceleration measured, processed and corrected by a strain gauge (25) attached to a side surface of the metal rod or by a laser interferometer (24) is obtained, and the corrected acceleration and the output of the acceleration sensor are compared to thereby carry out calibration and evaluation of the acceleration sensor.

Abstract: An acceleration sensor (22) to be calibrated and evaluated is affixed to one end surface (22) of a metal rod (1), and a plurality of projectiles (3) are made to impact the other end surface (2) of the metal rod at prescribed time intervals, generating an elastic wave pulse in the metal rod. Dynamic displacement, velocity or acceleration in a direction normal to the other end surface arising in a process of the generated elastic wave pulse reaching and being reflected by the one end surface where the acceleration sensor is affixed is measured, and an acceleration measured, processed and corrected by a strain gauge (25) attached to a side surface of the metal rod or by a laser interferometer (24) is obtained, and the corrected acceleration and the output of the acceleration sensor are compared to thereby carry out calibration and evaluation of the acceleration sensor.

Abstract: An elastic wave pulse is generated in a metal rod (1) by impacting an end surface (2) of the metal rod with each of two round, concentric projectiles (8, 10) from a double launch tube (4, 5) independently, and by impacting both projectiles simultaneously or at a prescribed time interval. An acceleration sensor (23) is provided on another end surface (22) of the metal rod to measure an acceleration of the other end surface arising when the elastic wave pulse generated by the impact of the projectiles reflects at the other end surface. The motion of the end surface is measured by a laser interferometer (24) or by a strain gauge (25) provided on a side surface of the metal rod, and the measured signals are calculated and corrected as appropriate. The dynamic linearity of the acceleration sensor is obtained by comparing in time domain and frequency domain the calculated results with the measured values of the acceleration sensor.

Abstract: A method of testing frequency characteristics of a laser displacement/vibration meter by the use of a novel which can cope with a broader frequency range and finer micro-level displacements to enhance the reliability of the displacement/vibration meter. Upon applying impact on one end face of a round metal rod, an elastic wave pulse which propagates through the metal rod generates a stepwise dynamic displacement of the other end face of the rod when reflected there. This dynamic displacement is measured simultaneously by a reference laser interferometer with a reference laser beam and a laser displacement/vibration meter with unknown frequency response characteristics, followed by comparison of measurement data over a frequency range to determine the frequency response characteristics of the unknown laser displacement/vibration meter.

Abstract: A method of testing frequency characteristics of a laser displacement/vibration meter by the use of a novel method which can cope with a broader frequency range and finer micro-level displacements to enhance the reliability of the displacement/vibration meter. Upon applying impact on one end face of a round metal rod, an elastic wave pulse which propagates through the metal rod generates a stepwise dynamic displacement of the other end face of the rod when reflected there. This dynamic displacement is measured simultaneously by a reference laser interferometer with a reference laser beam and a laser displacement/vibration meter with unknown frequency response characteristics, followed by comparison of measurement data over a frequency range to determine the frequency response characteristics of the unknown laser displacement/vibration meter.

Abstract: A CPU interprets and executes a command in accordance with a program. A DMA channel selector is controlled by the CPU. The DMA channel selector determines whether a DMA transfer control signal from each of the independent DMA transfer control lines of a plurality of expansion slots is a common DMA transfer control signal or an independent DMA transfer control signal for each slot, thus connecting each of the independent DMA transfer control lines to a first or second DMAC. With this operation, an independent DMA transfer control line is assigned to each expansion slot while the compatibility with each expansion slot of an existing apparatus is maintained.

Abstract: When a data read timing of a DMAC is not matched with an output timing of data read out from a DRAM, the readout data is held in a register until a subsequent data read timing of the DMAC comes to the front. When data is read out from the DRAM, and if a processor clock of the DMAC has a phase matched with that of an operation clock of the DRAM, then a direct read operation is performed. If the phases of the two clocks are not matched with each other, the readout data from the DRAM is temporarily stored in the register and then fetched in the DMAC.

Abstract: A method for measuring the dynamic response characteristics of a shock accelerometer comprises the steps of attaching an accelerometer to be tested and a strain gage to one end of a rod supported to be axially slidable, imparting an impact to the other end of the rod, inputting the acceleration arising when the elastic wave reflect from the end surface of the rod to the accelerometer and the strain gage, subjecting the outputs of the accelerometer and the strain gage to data processing and error compensation to obtain the gain and phase characteristics of the accelerometer.