110 results about "Explosive device" patented technology

The invention belongs to the technical field of aircraft recovery, and provides an aircraft controllable parachute recovery device which comprises a parachute opening motor (1), a motor support (2), a motor rocker arm (3), a connecting rod (4), a recovery parachute cabin (5), a parachute cabin cover (6), a parachute cabin locking block torsional spring (9), a locking block rotating shaft (10), a driving rod (11), an unlocking hook (12), a spring guide rod (13), an initial locking rod (14), a parachute opening shaft (21), a parachute opening compression spring (18), a parachute hanging screw (17), a recovery parachute (19), a tower spring (20) and a tower spring pressing plate (15). According to the technical scheme, the motor drives the connecting rod mechanism to unlock, the tower spring and the pressure spring are combined to open the parachute, and the problems that an initiating explosive device is low in safety, poor in testability, unrepeatable in recovery and the like are solved.

An explosive downhole tool includes a housing having an upper housing part on one side of a window section and a lower housing part on an opposite side of the window section. An explosive charge is provided within the housing for at least one of cutting and expanding the wall of the tubular. The outer surface of at least one of the upper and lower housing part is rounded so as to be devoid of corners. The rounded surface eliminates the presence of sharp corners that may catch on restrictions or protrusions in a wellbore so that the downhole tool is more easily conveyable within a wellbore. Another explosive downhole tool includes fins extending from the housing. The fins have a height that decreases in a direction away from the housing. The shape of the fins enables the downhole tool to be more easily conveyable within the wellbore.

The header of an EED is redesigned to increase stiction forces to better hold the main charge throughout deflagration. The header includes a main charge holder, integrally formed or as a discrete component, that has internal structure that is press fit to a complementary outer surface of the main charge. The contact area between the internal structure and the main charge being greater than the contact area between a cylinder that circumscribes the internal structure (the uniform cylindrical shape of a typical EED contact area of π*D*L) to increase stiction forces between the main charge holder and the main charge. For a given diameter and length, the inclusion of the internal structure will reduce the mass of the main charge.

A system for delivering and activating a two-part explosive may include an unmanned vehicle and / or an elevated structure, and a two-part explosive device. The device may include a container that is attached to, and releasable from, the unmanned vehicle or elevated structure. The container may contain an unsensitized explosive enclosed in a casing and and a sensitizing agent adjacent to the casing. The device may include an opening mechanism positioned at least partially within the container and adjacent to the casing. The opening mechanism may open the casing and expose the unsensitized explosive to the sensitizing agent, forming the two-part explosive in response to the container being released from the unmanned vehicle or elevated structure. The device may include a detonator inside or attached to the container. The detonator may trigger ignition of the two-part explosive after the unsensitized explosive is exposed to the sensitizing agent.

A ballistically-safe wellbore tool may include an explosive device, an initiator including an initiating charge, and a bias member. A relative configuration of the explosive device and the initiator may be switchable between a first configuration, in which the initiating charge is at a ballistically safe distance from the explosive device, and a second configuration, in which the initiating charge is within a ballistically operable distance from the explosive device. The bias member is configured to bias the explosive device and the initiator to the first configuration.

The invention discloses a collision test method and test system for an energy storage element of an electronic detonator, and belongs to the technical field of initiating explosive device test. The method comprises the following steps: blocking an electronic detonator sample with a first rotating speed by adopting a blocking mechanism on a collision test system, so that the electronic detonator sample collides with the blocking mechanism; capturing a voltage curve image at the collision moment T through a voltage curve monitoring and processing unit, and calculating to obtain a first drop amplitude value under the maximum voltage at the collision moment T according to the captured voltage curve image; capturing a voltage curve image from the collision moment T to the first collision duration T + T1 through a voltage curve monitoring processing unit, and calculating to obtain a voltage drop rate from the collision moment T to the first collision duration T + T1 according to the captured voltage curve image; and evaluating the impact resistance of the energy storage element according to the obtained first drop amplitude under the maximum voltage and the voltage drop rate. The collision test method provided by the invention is beneficial to improving the accuracy of a collision test result.

The invention discloses a damping fluid outflow coefficient rapid testing device capable of simulating driving force of an initiating explosive device. The air cylinder piston can amplify the airflow pressure and transmit the airflow pressure to the donor piston within millisecond, so that the main characteristics of the driving force on the donor piston are basically consistent with those of the driving force of the initiating explosive device, and the effect of simulating the driving force of the initiating explosive device is achieved; the donor piston pushes the damping liquid to pass through the oil passing sheet to simulate the damping effect process, and the change of the length-diameter ratio of the central oil passing hole can be realized by replacing the oil passing sheet, so that the damping effect of the oil passing holes with different length-diameter ratios can be simulated and tested at the initial stage of development; the movement speed of the acceptor piston is consistent with the flow speed of the damping fluid after passing through the oil passing sheet, and the movement speed of the acceptor piston is indirectly obtained based on a photoelectric target signal. Therefore, the outflow coefficients under different temperatures, different damping fluid types, different overflowing hole structure sizes and different driving forces can be obtained, and the damping effect under different working conditions can be rapidly evaluated.

The invention relates to an underwater platform releasing and cable cutting mechanism which comprises a releasing base, a shell, a push shaft, a releasing hook, an initiating explosive device, a watertight connector and a cable limiting structure. The shell is fixed to underwater equipment through the release base and provided with a closed pneumatic cavity, the push shaft is slidably connected to the pneumatic cavity, and the two ends of the push shaft extend out of the two ends of the shell. One extending end of the push shaft is matched with the release hook so as to limit the underwater platform to the underwater equipment; the other extending end of the push shaft is a cutting knife; the cable limiting structure limits the cable to one end corresponding to the cutting knife, and the position of the cable corresponds to the position of the cutting knife. The initiating explosive device is electrically connected with the underwater equipment through the watertight connector and used for receiving signals of the underwater equipment and releasing high-pressure gas to the pneumatic cavity, the high-pressure gas pushes the push shaft to move towards the cable, the push shaft is made to be disengaged from the release hook to relieve limiting of the underwater platform, and meanwhile the cutting knife moves to cut off the cable. According to the invention, the release of the test platform and the cutting of the cable can be synchronously completed, the full-water-pressure balance is realized, and the adaptability is high.

The invention provides a high-pressure gas membrane rupture pressure measuring device and a measuring method thereof, and belongs to the technical field of pressure measurement. The measuring device comprises a pressure generation system, a gas compression system, a gas injection system, a pressure measuring system and a diaphragm clamping system. The piston divides the cavity into a hydraulic cavity and a gas compression cavity, and the piston is hydraulically driven to compress the pre-filled gas, so that the diaphragm is broken. The pressure measurement system records pressure-time data in real time, and a sliding window average algorithm is adopted to extract a membrane rupture pressure peak value. According to the technical scheme, inert gas is used, initiating explosive devices are not used, membrane rupture energy is only gas expansion, the protection box can absorb fragments, and explosion-proof transformation is not needed in a laboratory. And the smoothed unique membrane rupture pressure value is output through a sliding window averaging algorithm, and manual reading errors are eliminated. According to the technical scheme, the device is compact in structure, safe to operate, rapid in testing and suitable for accurately measuring the diaphragm rupture pressure of the gas gun diaphragm in a conventional laboratory.

The utility model discloses a single foot twist break type transducing element. Including electrode plug, shell, fixed glue, solder and bridge silk. The utility model has designed single foot twist break type initiating explosive device structure in the country first, is a novel structure's transducing element for missile gyro, has higher firing reliability, twist break reliability and security, can be applicable to various gyro ignition, provides new train of thought for gyro design and structure optimization. Product adopts single foot structure electrode plug, double bridge parallel firing design, constitutes firing unit after filling detonating agent, integrates firing and working function, realizes product 700ma firing, 35MPa output pressure bearing, foot line 3.92N the twist break of cm, 59kPa vacuum ignition, damp heat, medium withstand voltage, electromagnetic compatibility, firing reliability 0.999 etc. technical index requirement. The utility model product reliability, security, versatility are high, and environmental adaptability is strong, and the technology reaches the leading level in the country, and the application prospect is wide, and military, economic benefit is remarkable.

Safe addressable firing controls positioned within a reusable housing that only allows voltage and current from the shooting panel to reach the explosive device by addressing the switch to open allowing electricity to pass through it and setting off the chain reaction during detonation, wherein the safe addressable firing controls positioned within a cartridge that creates a safety barrier between the surface equipment and a downhole tool, such as an explosive device.

The utility model relates to the technical field of army teacher training auxiliary tools, and discloses a weapon launching bidirectional acousto-optic smoke effect simulation device, which comprises a device main body, and a bidirectional initiating explosive device is fixedly connected in the device main body. According to the weapon launching bidirectional acousto-optic smoke effect simulation device, through cooperative arrangement of the device main body, a limiting groove, a reset spring and a fixed suction cup, the device main body is rotationally clamped into a 40mm rocket barrel during training use, and then the reset spring is driven to be compressed; when the device main body is rotated and clamped to a proper position, the fixed sucking disc stops moving and is adsorbed on the inner wall of a 40mm rocket barrel for anti-skid fixation, and when the device main body needs to be separated, the device main body can be pulled out by rotating and loosening the fixed sucking disc, so that the anti-skid adsorption and fixation effects on the weapon launching two-way acousto-optic smoke effect simulation device and the 40mm rocket barrel are achieved; the operation is simple, and the possibility of loosening and falling off is low.

The utility model discloses a circuit substrate structure as well as an electronic detonator control module and an electronic detonator comprising the circuit substrate structure, and belongs to the technical field of initiating explosive devices. The circuit substrate structure comprises a body, the body is of a long-plate-shaped structure, the body is provided with a containing through groove used for containing an energy storage capacitor, the containing through groove extends in the length direction of the body, the body forms a wide-edge bridge on one side of the containing through groove in the width direction, and the body forms a narrow-edge bridge on the other side of the containing through groove in the width direction. The narrow-side bridge is arranged right opposite to the wide-side bridge, the width size of the wide-side bridge is larger than that of the narrow-side bridge, and when the energy storage capacitor is placed in the placing through groove, the energy storage capacitor is located on the inner side of the placing through groove in the horizontal direction; and the narrow-side strength enhancing structure is arranged on the narrow-side bridge and is used for enhancing the strength of the narrow-side bridge. The circuit substrate structure provided by the utility model is beneficial to reducing the size of the protruding body of the energy storage capacitor and improving the reliability and stability of the energy storage capacitor.

The invention relates to the technical field of initiating explosive device production, and discloses an explosive charging device for initiating explosive device production, which comprises a base, a conveying belt is arranged in the base, a support frame is fixedly connected to the front side of the base, a fixed plate is fixedly connected to one side of the support frame, a stock bin is fixedly connected to one side of the top of the support frame, and the fixed plate is fixedly connected to the other side of the top of the stock bin. And one side of the fixing plate is fixedly connected with a discharging port, the top of the fixing plate is provided with a charging assembly and an adjusting assembly, and the bottom of the fixing plate is provided with a rotating assembly. A motor is started to drive a half gear to rotate, the half gear rotates to drive a rotating disc to intermittently rotate through cooperation of a full gear and a rotating shaft, the rotating period is a half circle, the two first feeding pipes are arranged at the bottom of a stock bin and the top of a discharging port correspondingly, one feeding pipe feeds the other feeding pipe, and the two feeding pipes alternately operate and move; in the moving process, the cover plate is in a sealed state, raw material leakage is avoided, and the charging continuity and the production efficiency are improved.

The application provides a chute blocking blasting charge structure and a blasting method, and relates to the technical field of blasting, and comprises an explosion device and an ignition device.The explosion device comprises an umbrella-shaped explosion assembly and a columnar explosion assembly, and the columnar explosion assembly is located between the umbrella-shaped explosion assembly and the ignition device.The umbrella-shaped explosion assembly comprises a plurality of limiting frameworks and first explosives fixed on the surfaces of the limiting frameworks, adjacent two limiting frameworks have a predetermined angle, and a plurality of the limiting frameworks form an umbrella-shaped structure at the lower end of a blocking body.The application greatly improves the effect of blasting construction, ensures the safety of blasting, improves the efficiency of underground blasting construction, is convenient for on-site construction, can effectively deal with long-distance blocking of a main chute shaft, and is well applied in mines.

The application provides a kind of automatic detection switching device for wire device, including support assembly and wire carrier assembly, the support assembly is opened in two holes on main support, one hole is installed with switching connector, for interfacing wire carrier assembly, another hole is used to install leaded explosive device;The wire carrier assembly includes switching socket, wire carrier body and switching connector, the wire carrier body is slotted at one end for installing switching socket, switching socket is used to interface the lead of leaded explosive device, the other end is installed with switching connector, the switching socket and switching connector are electrically connected;The slotted end of the wire carrier body is closed with switching socket cover plate.The application can ensure the safety of short circuit during the switching process of connector, while reducing the interfacing accuracy requirement of micro plug and automatic detection equipment, greatly reducing the automatic production and detection cost of such products.

The utility model provides a light long-distance non-contact dangerous initiating explosive device laser destruction vehicle, which comprises an optical system, a holder, a mounting seat, an air-cooled laser, a large connecting platform, an intelligent crawler, a small connecting platform, a battery and a remote control terminal, the holder is connected with the optical system and the mounting seat through screws; the mounting seat is connected with the holder and the intelligent crawler through screws; the air-cooled laser is fixed on the large connecting platform through a screw; the large connecting platform is connected with the air-cooled laser through screws; the intelligent crawler is respectively connected with the large connecting platform, the mounting seat and the small connecting platform through screws; the small connecting platform is connected with the battery and the intelligent crawler through screws; the remote control terminal is configured to output signals to the intelligent crawler, the holder and the laser. The laser destroying device is compact in structure and light in weight, dangerous initiating explosive devices can be destroyed in a long-distance non-contact laser mode, and the safety of operators is greatly guaranteed.

The invention discloses an aircraft attitude control execution system, which is characterized in that an actuator controls pitching and overturning of an aircraft through four groups of attitude control engines, each group of engines is controlled through an independent control circuit, and the control delay time of each path does not exceed 50us; each control circuit is connected with a safety protection circuit, a state function checking circuit, an execution control circuit and an execution state voltage recovery circuit, the control circuits control an external ignition wire F1, an external ignition wire F2, an external ignition wire G1 and an external ignition wire G2, and execution control is completed through an ignition module. Through the safety protection circuit, the safety of storage and transportation of the initiating explosive devices of the aircraft can be ensured; the state inspection circuit can inspect the state of the initiating explosive device of the aircraft timely and inspect the safety state of the initiating explosive device of the aircraft in real time; an execution control circuit responds to output signals of the aircraft in a low-delay mode, and attitude control is conducted on the aircraft in time; the advantages of optical coupler isolation collection are utilized in state recovery collection, and false alarm caused by interference is avoided.

The invention relates to a metal wire tension adjusting device and method, and belongs to the field of spaceflight initiating explosive devices, and the metal wire tension adjusting device comprises an alignment assembly and an adjusting assembly. The annular bottom plate, the annular guide rail, the annular sliding block, the linear bottom plate, the linear guide rail, the linear sliding block and the support base form an alignment assembly of the tension adjusting device. The square tube bearing seat, the deep groove ball bearing, the adjusting nut, the screw rod, the tension meter seat, the locking nut and the tension meter form an adjusting assembly of the tension adjusting device. Before adjustment, the tension meter is moved to the position over the metal wire through the alignment assembly to be connected with the metal wire; during adjustment, the adjusting nut is rotated to adjust the tensile force of the metal wire; and after the tensile force is adjusted in place, a locking nut on the metal wire is fixed, so that the metal wire with certain tensile force can be obtained. The device is suitable for adjusting the tension of the metal wire in the metal wire embedded composite solid propellant grain.

The invention relates to the technical field of initiating explosive device detonation control, and provides an initiating explosive device detonation control device with an output state acquisition function, which comprises a power supply circuit, a detonation control circuit, a triggering and driving circuit, an ignition output circuit and an output state isolation acquisition circuit, the power supply circuit converts ignition output power supply + 28V into + 5V and + 3.3 V to supply power to a peripheral circuit of a single-chip microcomputer in the detonation control circuit, an ignition instruction of an upper computer is processed by the detonation control circuit and then outputs an ignition control signal through two IO ports of the single-chip microcomputer, and the ignition control signal is sent to the ignition output circuit after passing through the trigger and drive circuit. Meanwhile, ignition output is enabled by load release and physical separation signals, the ignition output is output to the initiating explosive device, and the initiating explosive device is detonated; and in the detonation process, the output state isolation acquisition circuit acquires the state of the output voltage and reports the state regularly. The reliability of ignition output in the initiating explosive device detonation process can be effectively improved.

The invention relates to an initiating explosive device ignition circuit, in particular to a comprehensive electronic equipment initiating explosive device ignition circuit capable of suppressing power-on peak voltage, and aims to solve the problems that when an existing initiating explosive device ignition circuit works, microsecond-level power-on peak voltage can be generated at the output end, mistaken activation of an initiating explosive device is easily caused, and the power-on peak voltage cannot be suppressed. And therefore, the problem of harm to products and personnel is solved. A power-on peak voltage suppression module is added between PMOS transistors and a VCC power supply, the power-on peak voltage suppression module comprises two PMOS transistors, and the source electrodes of the two PMOS transistors are connected with the VCC power supply; the grid electrode of the PMOS tube V3 is connected to the ground through a resistor R5 and a resistor R108, and the grid electrode of the PMOS tube V4 is connected to the ground through a resistor R6 and a resistor R108; a soft start time control resistor is connected in series between the resistor R5, the resistor R6 and the resistor R108. And a first delay capacitor bank is connected in parallel between the source electrodes of the PMOS tubes V3 and V4 and the resistor R5 and the resistor R6, so that the conduction time of the PMOS tube V1 is delayed after the VCC power supply is powered on, and the power-on peak voltage is suppressed.

The invention discloses an integrated multi-mode electric baking explosion testing device for an electric initiating explosive device, which belongs to the technical field of initiating explosive device testing and comprises a measurement and control cabinet, a multi-mode testing module integrated in the measurement and control cabinet, an industrial control data acquisition system and a human-computer interaction interface. The multi-mode test module integrates four functional modules of alternating current baking explosion, direct current baking explosion, 10A1S safety current test and 12V dry battery baking explosion, and can meet various test working conditions required by national military standards. The industrial control data acquisition system serves as a core, uniformly controls all test processes, and realizes real-time and high-precision acquisition and dynamic analysis of key parameters such as voltage and current in an experiment process. The problems that a traditional testing method is single in function and insufficient in data collection are solved, and an efficient, accurate and safe integrated testing solution is provided for research, development, production and reliability evaluation of initiating explosive devices.

The utility model belongs to the technical field of initiating explosive devices, and discloses a metal flyer transduction element for a slapper detonator, which comprises a substrate (1), an adhesion layer (2), a bridge foil (3), an insulating layer (4), a metal flyer (5), an acceleration chamber (6), an electrode I (7) and an electrode II (8), the adhesion layer (2) is attached to the substrate (1) in a magnetron sputtering manner; the bridge foil (3) is attached to the adhesion layer (2) in an electroplating or magnetron sputtering mode and is in a bridge shape. The first electrode (7) and the second electrode (8) are made of the same material as the bridge foil (3) and are arranged at the two ends of the bridge shape of the bridge foil (3); the metal flyer (5) is attached to the insulating layer (4) in an electroplating or magnetron sputtering manner and is circular; and the accelerating chamber (6) is arranged on the outer surface of the metal flyer (5). According to the utility model, excessive loading and neglected loading of flyers and entry of foreign matters in the transduction element assembly process are effectively avoided, and the production quality control of the transduction element is improved.

The utility model belongs to the technical field of initiating explosive devices, and discloses an embedded high-overload-resistant slapper detonator which comprises a shell (1), an output grain (2) is embedded and clamped on one side of the shell (1), a fastening compression ring (3) is clamped on one side of the output grain (2), and a starting grain (4) is clamped on one side, far away from the output grain (2), of the fastening compression ring (3). And an acceleration chamber (5) and a flyer (6) are arranged on one side, far away from the fastening compression ring (3), of the starting grain (4). According to the technical scheme provided by the utility model, the problem of energy transmission interruption or detonation failure caused by assembly looseness is avoided, the structural stability and reliability of the detonator in a high overload environment are greatly improved, and normal detonation under various extreme conditions is ensured.

The utility model discloses an anti-knock door bucket structure used in an initiating explosive device production building. The anti-knock door bucket structure comprises a plurality of layers of anti-knock door bucket wall bodies and anti-knock door bucket floor systems. The anti-explosion door hopper wall bodies are connected with anti-explosion wall bodies of a general assembly workshop and a packaging workshop respectively, fireproof outlets are formed in the anti-explosion door hopper wall bodies, and channels formed by the fireproof outlets in the adjacent anti-explosion door hopper wall bodies are arranged in a staggered mode. Compared with the prior art, the explosion-proof door is omitted, and the connecting channel of the general assembly workshop and the packaging workshop is arranged to be of the multi-layer explosion-proof door bucket structure, so that production workers can directly convey the assembled initiating explosive devices from the assembly workshop to the packaging workshop, and the explosion-proof door does not need to be repeatedly opened and closed in the conveying process. And the situation that an assembly workshop or a packaging workshop explodes, and shock waves of explosion affect workers and equipment working in the adjacent workshops is avoided, and the safety and production efficiency of initiating explosive device production are improved.

The invention discloses a mechanical arm system for grabbing small initiating explosive devices for assembly and a control method of the mechanical arm system. The executing mechanism is composed of a Baxter double-arm collaborative robot and an improved two-finger parallel clamping jaw; the feedback mechanism comprises a depth camera, a color camera and a thin film type pressure sensor; the control mechanism is a cross-platform architecture formed by a Windows upper computer and a Linux lower computer; the system collects image information and grabbing force information of the small initiating explosive device in a working area through the feedback mechanism, grabbing parameters are output after the image information and the grabbing force information are processed by the control mechanism, and high-precision recognition, lossless grabbing and flexible assembly of the small initiating explosive device are achieved through the execution mechanism according to the grabbing parameters. According to the invention, the improved clamping jaw can realize lossless grabbing of the small initiating explosive device based on the grabbing information obtained by the neural network; the end-to-end grabbed information generation method of the deep learning neural network is utilized, the algorithm operation speed is greatly improved, the overall architecture potential does not need to be reconstructed during expansion, and maintainability is enhanced.

The utility model discloses an initiating explosive device transportation detection electromagnetic protection box, which relates to the technical field of initiating explosive device transportation and comprises a box body, a box cover arranged at the top of the box body, a waterproof edge formed by bending a metal plate at the edge of an upper side port of the box body, a water vapor sealing ring fixed on a platform at the bottom of the waterproof edge, and a conductive sealing ring fixed on the inner side of the bottom of the box cover. An observation window is installed on the box cover and is made of flexible shielding glass, grooves are formed in the left side and the right side of the box body, electromagnetic shielding sleeves extending into the box body are arranged on the grooves, side opening covers installed on the box body are correspondingly arranged on the outer sides of the electromagnetic shielding sleeves, and initiating explosive device detection work can be conveniently carried out through the observation window before use; the conductive sealing ring can abut against the waterproof edge of the upper port of the box body in a contact mode, reliable electric connection is formed, the electromagnetic protection effect is achieved, the performance stability of the initiating explosive device is improved, the probability of accidents is reduced, protection detection is conducted through the electromagnetic shielding sleeve before the initiating explosive device is used, and the quality performance of the initiating explosive device is ensured.

The invention discloses a volume-variable initiating explosive device weighing and charging system, and relates to the technical field of initiating explosive device weighing, a high-precision servo motor is used for automatically carrying out online adjustment on the volume of a metering plate, the adjustment process is controlled, the output torque is detected, the adjustment process is safe and accurate, and the workload of workers is greatly reduced. During production, the control system automatically adjusts the volume of the metering plate online in real time according to the matching condition of the current constant-volume explosive quantity and the target explosive quantity, the explosive loading precision is high, meanwhile, the problem of continuous rejecting caused by density change due to explosive batch changing or explosive layering is solved, the production efficiency is improved, operation of workers on the metering plate and the explosive is reduced, and the labor intensity of workers is reduced. The production safety is improved. The volume of the metering plate can be adjusted with high precision within a certain range, and the metering plate is large in adjustable dose interval and can adapt to flexible production of various products.

The invention relates to a three-axis cooperative assembly system, in particular to an automatic three-axis cooperative assembly system for slapper type initiating explosive devices. The device comprises a bottom plate; the at least one group of Z-axis turntable module is fixedly arranged on the bottom plate, and the Z-axis turntable module is used for bearing, rotating and positioning the initiating explosive device part; the double-axis motion platform is erected above the bottom plate and above the Z-axis rotary table module, and the double-axis motion platform is used for providing micron-sized positioning in an XY plane; the integrated interface is mounted at the output end of the double-shaft motion platform; the portal frame is used for supporting the double-shaft motion platform; the closed-loop servo control unit is used for receiving feedback signals of the encoder, driving the double-axis motion platform to perform X-axis and Y-axis motion and driving the Z-axis rotary table module to perform Z-axis motion. The repeated positioning precision is high, manual operation is replaced with a high-precision servo motor, the repeated positioning precision of products in the same batch in the assembling process is improved to a great extent, and the consistency of the products in the same batch is improved.

This invention discloses a blade separation device for containment testing. A guide groove for placing the blade separation device is formed on the cross-section of the blade's flow channel. The blade separation device for containment testing includes a shell, a partition, an explosive body, and a shear-hardening colloid. A receiving cavity is formed inside the shell; the partition divides the receiving cavity into an explosive cavity and an energy confinement cavity; the explosive body is placed in the explosive cavity; the shear-hardening colloid fills the energy confinement cavity, causing the blade to break and separate along the flow channel cross-section to meet the requirements of the containment test. The shear-hardening colloid, in conjunction with the partition, provides explosive energy confinement, replacing the metal materials contained in traditional explosive devices. This avoids the generation of high-temperature, high-speed molten metal debris after the explosion, resulting in low risk. It also has the advantage of being lightweight, reducing the impact on the overall rotor dynamic balance, and is simple and convenient to install.