A high-pressure liquid delivery system under a high centrifugal acceleration condition on an arm-centrifuge, comprising a centrifuge main engine, a ground liquid source, a ground delivery conduit, a centrifuge bottom rotary joint, a centrifuge rotary arm delivery conduit, a rotary arm-basket pin roll, a basket rotary joint, a basket delivery conduit and a basket conduit outlet. According to the present disclosure, the basket rotary joint is introduced to adapt to the change of the basket-rotary arm angle before and after the arm-type basket centrifuge works, so that the demand for water, electricity, oil and gas transportation of the centrifuge is met. Therefore, the design for the conduit of the centrifuge-basket part is solidified, and compared with the traditional solution that a high-pressure hose is connected to the basket, the centrifugal acceleration load of the load can be increased to more than 500 g.

Described herein are examples of improved material (and/or universal) testing machines having a lower crossbeam that may be moved via a drive system of the material testing machine. In some examples, this may be accomplished via drive shafts with different threading in upper and lower portions, and/or independent drive systems for upper and lower crossbeams. The ability to dynamically adjust (e.g., raise) the lower crossbeam may allow an operator to interact with test samples at a more comfortable height, and reduce the need for an operator to repeatedly bend and/or kneel.

A shear testing system and method of thermo-seepage-mechanical field and engineering disturbance coupling under deep and complex condition are provided. The shear testing system can be used in conjunction with an axial pressure application device to simplify the structure, save costs, and facilitate a triaxial confining pressuretemperatureaxial pressuretorsional shear coupled test on a rock specimen. The shear testing system can achieve the following three purposes. First, the shear testing system can convert an axial pressure into a torsional shear force through a transmission mechanism of a power conversion assembly. Second, the shear testing system can apply an axial pressure to the rock specimen fixed between two specimen fixing heads, through a pressure shaft of an axial pressure mechanism. Third, the shear testing system can apply a triaxial confining pressure and a temperature field to the rock specimen.

A test fixture is provided for containing a pair of test samples (i.e., sample pair) that contact each other along an interface. The fixture receives exposure to laser emission for radiative heating while providing compression to the sample pair. The text fixture includes a housing, an isolation container, and a compressor. The housing has an axial cavity with annular cross-sections including an internal helical thread portion and a window for receiving the laser emission. The isolation container receives the sample pair. The container inserts into the axial cavity and including an opening for disposition adjacent to the window. The compressor has circular cross-sections for insertion into the axial cavity and includes an external helical thread portion for engaging the internal helical thread portion of the housing. Axial pressure applies to the isolation container by turning the compressor inside the axial cavity. The isolation container provides thermal insulation from the housing and the compressor. In additional embodiments, the isolation container comprises a cup with the opening to isolate the sample pair from the housing, and a washer to isolate the sample pair from the compressor.

A device for testing a rotor blade of an aircraft. The device is configured to receive and secure a shaft of the rotor blade. Once secured, the device is configured to allow for inputting combined loads and bending moments into the rotor blade to simulate the rotor blade behavior in flight. A testing assembly is also disclosed that includes the device and the rotor blade and methods of use that provide for testing the rotor blade.

The present disclosure includes a method for determining a melt strength includes extruding one or more polymers to form the polymer film, passing the polymer film at least partially around a measurement roll coupled to a force measuring device, at least partially around a chill roll downstream of the measurement roll, and through a nip defined between two nip rolls, and measuring a force exerted on the measurement roll by the polymer film using the force measuring device. The polymer film is at least partially molten when contacting the measurement roll. A system includes an extruder, a measurement roll couple to one or more load cells, a chill roll coupled to a drive motor, at least two nip rolls downstream of the chill roll, and a take-up roll downstream of the nip rolls. The load cells measure a force exerted by the molten polymer film on the measurement roll.

A detecting machine for a yield rate of bristles of a toothbrush and a detecting method for the bristles are provided. The detecting machine includes a power device and two rotating units, and the two rotating units are rotatably mounted on a side surface of the power unit. The two rotating units are disposed parallel to each other. When in a rotating condition, the two rotating units rotate in opposite rotating directions. When a manufacturer horizontally disposes a toothbrush between the two rotating units, the surfaces of the two rotating units may compress the bristles and pull the bristles toward a direction away from the toothbrush. Therefore the manufacturer can inspect whether the bristles are firmly mounted on the toothbrush.

A system for testing a device under a high gravitational force including a centrifuge with a rotating member and method of operation thereof. An operating power can be applied to a device, which can be coupled to the rotating member. The system can include a rotational control that can be coupled to the centrifuge. This rotational control can be configured to rotate the rotating member in response to a controlled number of revolutions per time period. The system can also include an analysis device for monitoring one or more signals from the device with respect to the controlled number of revolutions per time period. The analysis device can be configured to determine a stiction force associated with the DUT (Device Under Test) in response to the time-varying gravitational forces and to the one or more signals from the DUTs.

A specimen testing system has holders that hold a specimen for testing. The holders brace the specimen so that a load may be applied. A load applicator applies a load to the specimen at a location that is between the holders bracing the specimen. A user may adjust the load applicator until it applies the desired load to the specimen. If desired, a user may apply rotation to a specimen while it is experiencing a load by using a specimen rotation system. The user may continue to adjust the load applied to the specimen or continue to rotate the specimen during loading until the specimen fails.

An example flexible substrate testing system includes: a first substrate support structure configured to hold a first portion of a flexible substrate under test; a second substrate support structure configured to hold a second portion of the flexible substrate; one or more actuators configured to move the first and second substrate support structures at respective angles to fold the flexible substrate; and load cells configured to measure loads on the first substrate support structure and the second substrate support structure while the actuator moves the first substrate support structure and the second substrate support structure.