G01N2203/0228

SYSTEM AND METHOD FOR TESTING ROCK FRACTURE UNDER VACUUM AND EXTREME-TEMPERATURE CONDITION
20250198894 · 2025-06-19 ·

A system for testing rock fracture under a vacuum and extreme-temperature condition includes a vacuum extreme-temperature loading structure, an overall loading frame structure and a mobile cart. The vacuum extreme-temperature loading structure includes a vacuum transparent shield, a vacuum base and an extreme-temperature loading module. A bottom end of the vacuum transparent shield is covered on the vacuum base and is hermetically connected with the vacuum base to form a vacuum structure. The extreme-temperature loading module is provided inside the vacuum structure. The overall loading frame structure includes an overall frame and a loading cylinder. A middle of the overall frame is provided with a loading space, and the vacuum extreme-temperature loading structure is located in the loading space. The mobile cart is located in the loading space and is slidably connected with the overall frame, and the vacuum base is arranged on the mobile cart.

RIG FOR TESTING THERMOMECHANICAL LOADS

A rig for testing thermomechanical loads comprises grip portions for gripping a test specimen, and a frame that join the grip portions to each other, the thermal expansion coefficient of the grip portions being greater than the thermal expansion coefficient of the frame. The frame may be made from metal.

System and method for testing rock fracture under vacuum and extreme-temperature condition

A system for testing rock fracture under a vacuum and extreme-temperature condition includes a vacuum extreme-temperature loading structure, an overall loading frame structure and a mobile cart. The vacuum extreme-temperature loading structure includes a vacuum transparent shield, a vacuum base and an extreme-temperature loading module. A bottom end of the vacuum transparent shield is covered on the vacuum base and is hermetically connected with the vacuum base to form a vacuum structure. The extreme-temperature loading module is provided inside the vacuum structure. The overall loading frame structure includes an overall frame and a loading cylinder. A middle of the overall frame is provided with a loading space, and the vacuum extreme-temperature loading structure is located in the loading space. The mobile cart is located in the loading space and is slidably connected with the overall frame, and the vacuum base is arranged on the mobile cart.

THERMAL SHOCK TESTING APPARATUS AND THERMAL SHOCK TESTING METHOD
20250271489 · 2025-08-28 · ·

A thermal shock testing apparatus includes a test chamber in which a test sample is placed, and which is sealed; a chiller which cools the test chamber to a predetermined temperature with coolant; a lamp heater which heats the test sample to a target temperature; a temperature sensor which detects a temperature of the test sample; a control device which controls the operation of the chiller, and the energization and shut-off of the lamp heater. The test sample is heated to a target temperature with the lamp heater, after the test chamber is cooled to a predetermined temperature. Thereafter, the energization of the lamp heater is shut off, and a thermal shock is added to the test sample. Thereby, a thermal shock test can be conducted in a short time.

IN-SITU MICRO-NANO IMPACT INDENTATION TESTING INSTRUMENT

The present invention relates to an in-situ micro-nano impact indentation testing instrument, falling within the technical field of material micromechanical testing. The instrument comprises a nitrogen generation module, an environmental chamber, a high/low temperature loading module, an optical-infrared in-situ monitoring module, an electromagnetic-piezoelectric coupling impact module, etc. After the nitrogen is introduced into the environmental chamber and the test area is determined by microscopic imaging, the electromagnetic-piezoelectric coupling impact module can drive an indenter to indent a specimen. An acoustic emission sensor embedded in the high/low temperature loading module can monitor the surface crack propagation of the specimen. The optical-infrared in-situ monitoring module can perform real-time high-speed optical imaging and infrared imaging on the impact indentation process. The present invention can perform micro-nano impact indentation testing on the material at high or low temperatures.

Micro-nano impact indentation testing device and method based on cyclic refrigeration

The present invention provides a micro-nano impact indentation testing device and method based on cyclic refrigeration, and relates to the technical field of material property testing. The testing device comprises a pressure rod and a stage for low-temperature micro-nano impact indentation testing, and a refrigeration device for refrigerating and cooling the pressure rod and the stage, wherein the refrigeration device refrigerates the pressure rod and the stage by adopting an embedded channel, a cold conduction wire connected to the pressure rod and the stage and a refrigeration balancer in contact with the cold conduction wire are arranged between the pressure rod and the stage, and the temperature of the pressure rod and the temperature of the stage are stabilized at a common temperature point by the cold conduction wire and the refrigeration balancer together.

DEVICE FOR TESTING THE LOW-TEMPERATURE CAVITATION OF INDUCER AND TEST METHOD

A device for testing a low-temperature cavitation of an inducer and a test method are provided. The device includes an inducer cavitation test assembly, a first liquid storage tank configured for storing a liquid medium therein and having an outlet connected with an inlet of the temperature control assembly, and a temperature control assembly having an outlet connected with an inlet of the inducer cavitation test assembly. An outlet of the inducer cavitation test assembly is connected with an inlet of the first liquid storage tank. The temperature control assembly is configured for controlling the temperature of the liquid medium from the first liquid storage tank into the inducer cavitation test assembly. The inlet of the inducer cavitation test assembly is connected with a gas storage tank for conveying gas. The inducer cavitation test assembly is configured for testing an inducer.

Adjustable Tilt Angle Compression Device for Mechanical Abuse Testing of Lithium-Ion Batteries and Test Method Thereof
20260043723 · 2026-02-12 ·

The present invention relates to the field of batteries, and particularly to a device and method for mechanical abuse testing of batteries. Existing devices apply compression vertically to the battery's force-bearing surface, which does not adequately simulate complex mechanical abuse during tilted scenarios. Specifically, they cannot compress the battery at multiple angles or collect compressive force values from different orientations. The invention provides an adjustable-tilt compression device for mechanical abuse testing of lithium-ion batteries. By tilting the battery support plate of the fixture, the device enables multi-angle compression and collection of force data from various angles, allowing for comprehensive testing of mechanical stresses encountered in real-world tilted abuse conditions. Additionally, the device supports testing at multiple points and under varying temperatures, enhancing the reliability and coverage of mechanical abuse assessments for battery safety evaluation.

SYSTEMS AND METHODS FOR PERFORMING RESPONSE TESTING AT LOW TEMPERATURES

Systems and methods are directed toward low temperature testing of motion, vibration, or force responses of test fixtures. For cryogenic shock testing, a test object can be secured on a test apparatus, such as a test fixture of a shock table. An elongated enclosure, such as a flexible tube, can be connected between the test fixture and a laser vibrometer, positioned orthogonal to a surface normal at a test region of the test fixture to enable light emitted by the vibrometer to be reflected from the test region back to the vibrometer. A flow of purge gas can be introduced into the tube, proximate the test fixture, to direct moisture away from the test fixture. The flow can prevent condensation or ice from forming on the surface of the test fixture at the cryogenic temperature. A shock event can be simulated, and the response of the test region measured by the laser vibrometer. The impact of the shock event on the test object can then be observed.