A hydrostatic test device for a turbine may include a plurality of feeding holes having a groove part formed with a greater diameter. Sealing members may be fitted into feeding holes in upper or lower casings of a turbine to seal the feeding holes.

A method for measuring load performance of a positive displacement motor (PDM) test coupon. The test coupon comprises a partial length of a PDM stage and is received inside a sealable test chamber. In some embodiments, the test coupon may be cut from a failed PDM stage. The test chamber is filled with test fluid. In some embodiments, the test fluid may be drilling fluid sampled from a live well. Rotation of the rotor on the test coupon actuates rotation of the stator. A braking torque is applied to the stator rotation, enabling evaluation of, for example, fatigue load performance of test coupon. Additional embodiments comprise the rotor axis and the stator axis being offset in order to simulate rotor/stator eccentricity in a full size PDM stage.

The invention pertains to a method for respectively determining the neutral temperature or the stressfree state in a rail section (1), wherein an ultrasonic signal is coupled into a representative volume of the rail profile perpendicular to its longitudinal direction, wherein the volume is subjected to stresses in the longitudinal direction of the rail section (1), wherein the stresses are measured, wherein an ultrasonic signal influenced by these stresses is decoupled, wherein a function describing the functional dependence of the decoupled ultrasonic signal on the introduced stress is determined, and wherein the stressfree state is determined based on the course of this function.

A device to test a contact of a connector includes a frame and a connector adaptor coupled to the frame. The connector adaptor is configured to retain the connector. The device also includes one or more alignment actuators coupled to the frame and a piston assembly movable relative to the connector by the one or more alignment actuators. The piston assembly is configured to apply a compressive force to the contact to test a locking mechanism of the contact.

The invention provides a structural fatigue strength design method based on an intensity field, aiming at the phenomenon that the stress field is mismatched with the overall strength in the existing structural fatigue strength design process according to the overall strength viewpoint. The invention takes the fatigue strength of mechanical structures and parts as field treatment, and organically matches a structural stress field and a fatigue intensity field, wherein an ideal fatigue intensity field distribution of a dangerous section of the structure is determined according to the maximum stress amplitude distribution of the dangerous section of the structure; the actual fatigue intensity field of the dangerous section of the structure is designed by combining materials and heat treatment with cold working strengthening-residual stress field; and by using the full-field stress-strength interference model, the fatigue strength design level of the dangerous section of the structure can be quantitatively evaluated.

A fatigue test assessment method for assessing a suspension point of a cylinder block by means of a fatigue test includes: fixing a suspension point of a cylinder block test piece by using a power assembly installation approach; applying a load to the suspension point of the cylinder block test piece in a preset direction; and determining whether the suspension point of the cylinder block fails. The method can ascertain, by means of assessment during a stage of parts testing, whether the structural strength of a suspension point of a cylinder block meets user requirements, so as to predict and prevent breakage of and faults in the suspension point of the cylinder block, thereby enhancing overall test validity.

A simulated payload apparatus (SPA) for testing in a flight motion system (FMS), which has a body for mounting in the FMS, and which simulates an actual payload during the FMS test. The SPA may include a plurality of adjustable weights that are mountable on and/or removable from the body to vary the mass and/or center of gravity of the SPA. The SPA may include an adjustable bracket for interfacing with a motion drive of the FMS, in which the bracket is positionable along the body to vary the moment of inertia of the SPA. The SPA may include an onboard electronic measurement device that is configured to measure a motion characteristic of the SPA and/or communicate information about the measured motion characteristic in real-time during the FMS test. The SPA may include a laser alignment for aligning the SPA relative to test equipment of the FMS.

A test apparatus for verifying plugging force of an electrical component having sockets for receiving one or more corresponding plugs in a push fit arrangement. The test apparatus includes a load plate with a support surface orthogonal to first and a second axes. A holder retains the first electrical component on the load plate. A plurality of load cells supports the load plate at spaced locations. A plugging force applied to the first electrical component via the second electrical component is transferred to the plurality of load cells. A processor is provided for receiving load cell data corresponding to the force applied to each load cell respectively. The processor determines the magnitude of the plugging force and the location at which the plugging force is applied to the first electrical component relative to the first and second axes of the load plate.

A testing device for simulating frictional wear behaviors of threaded joints of a drill pipe under turbid seafloor environment, including a support, an oil cylinder, upper and lower specimens, a first motor, several second motors, stirring rods, a turbidity sensor, and a test tank. The oil cylinder and test tank are arranged on the support. A piston rod of the oil cylinder is connected to the first motor. A rotating-speed sensor is arranged on a bottom surface of the first motor, facing toward an output shaft of the first motor. The output shaft of the first motor is connected to an upper end of a torque limiter. A lower end of the upper specimen fits an upper end of the lower specimen under loading of a main shaft of the first motor. The stirring rods are provided at two sides of the test tank.

An apparatus for testing a flexible screen. The apparatus for testing a flexible screen includes a slide rail, a reel, a clamping module and a drive module. The reel is fixed to one end of the slide rail. The axial direction of the reel is perpendicular to the extension direction of the slide rail. The flexible screen includes a first end and a second end which are disposed opposite to each other. The reel is configured to fix the first end of the flexible screen and rotate to drive the flexible screen to fit to the reel and coil around the reel. The clamping module is configured to clamp the second end of the flexible screen. The reel is further configured to rotate to drive, through the flexible screen, the clamping module to slide along the slide rail towards the reel.