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614results about How to "Large locking force" patented technology

Powerful and mechanical automatic-locking hydraulic cylinder

The invention discloses a powerful and mechanical automatic-locking hydraulic cylinder, and belongs to the technical field of hydraulic cylinders. The two ends of a cylinder barrel are sealed by a cylinder cover and a cylinder bottom respectively. A guiding column of the cylinder cover is sleeved with a spring. The spring is sleeved with a brake block. The two ends of the spring abut against the cylinder cover and the brake block respectively. The outer circumferential face of the large diameter of the brake block is in sealing fit with the inner circumferential face of the cylinder cover. The end face of the end, with a large-diameter hole, of a locking block abuts against the end face of the step of an inner hole of the cylinder barrel, and the other end face of the locking block abuts against the end face, located at the portion of the cylinder barrel, of the cylinder cover. After a steel ball is put into a steel ball installation hole of a piston, the steel ball installation hole of the piston is matched with an inner hole of the cylinder barrel, and an annular groove of the piston corresponds to a rodless cavity oil port in the cylinder barrel. One end of a piston rod is fixed to a piston rod installation hole of the piston, and the other end of the piston rod penetrates through the cylinder bottom to be located outside the cylinder barrel. According to the powerful and mechanical automatic-locking hydraulic cylinder, the requirement for automatic locking after the piston rod is completely retracted can be met, and the locking state can be kept for a long time under the situation that pressure relief of a hydraulic system is completed or leakage happens until unlocking is actively achieved.
Owner:CSIC ZHONGNAN EQUIP

On-orbit repeated locking and releasing mechanism for space

The invention relates to a repeated locking and releasing mechanism, in particular to an on-orbit repeated locking and releasing mechanism for space, and aims to solve the problem of repeated on-orbit locking and releasing of a large-scale actual load in a spacecraft. The on-orbit repeated locking and releasing mechanism comprises a trunnion locking mechanism, a lock hook compacting mechanism, a base locking mechanism, a crank and rocker mechanism and a driving gear mechanism, wherein the trunnion locking mechanism is arranged at the upper end of the base locking mechanism; and the driving gear mechanism is connected with the lock hook compacting mechanism and the crank and rocker mechanism. According to the on-orbit repeated locking and releasing mechanism disclosed by the invention, the trunnion locking mechanism, the lock hook compacting mechanism, the base locking mechanism, the crank and rocker mechanism and the driving gear mechanism are arranged in a crossed manner, so that the on-orbit repeated locking and releasing mechanism is simple and compact in structure; all the freedom degrees of a fixed object can be completely limited, and repeated locking can be realized; the maneuverability is good, so that the using requirement of on-orbit locking-releasing-relocking can be met. The on-orbit repeated locking and releasing mechanism disclosed by the invention is suitable for the technical field of aerospace and the technical field of electromechanical integration.
Owner:赵士野

Gas-driving jumping device

The invention provides a gas-driving jumping device which comprises a cylinder body, a piston and at least one elastic element, wherein the top end of the cylinder body is sealed by an upper cylinder cover; an opening is formed on the bottom of the cylinder body; the cylinder body is fixedly connected with the upper cylinder cover; a pressure detection port, an exhaust port and an ignition device are arranged on the upper cylinder cover; the ignition device is located on the inner side of the upper cylinder cover; a first level step, a second level step and a third level step are respectively formed in a top-wide bottom-narrow form on an inner side wall of the cylinder body; the exhaust port is controlled by an exhaust solenoid valve; the piston is located in the cylinder body in a drawing form; the piston is hollow; the top of the piston is opening; the bottom of the piston is fixedly connected with a base; a gas inlet is formed on the side wall of the lower part of the base; the gas inlet is controlled by an inlet solenoid valve; a lug boss is arranged at the top end of the piston; the lug boss is connected with the top end of the elastic element; the bottom end of the elastic element is connected with the second level step. The gas-driving jumping device has the advantages that the locking force is large, the gas purity can be effectively ensured, the structure is compact, the mounting and dismounting are convenient, and the gas-driving jumping device has high-efficient ignition device and higher space use rate so that the robot has higher extreme obstacle-crossing ability and higher flexibility and maneuverability.
Owner:HARBIN INST OF TECH SHENZHEN GRADUATE SCHOOL

Actuator cylinder position locking and unlocking mechanism

The invention relates to an actuator cylinder position locking and unlocking mechanism, which comprises a cylinder body (4), a piston (5) and an ejector rod (6). The ejector rod (6) is mounted in the piston (5), a cavity is arranged at one end of the ejector rod (6), a spring (1) is mounted in the cavity, a hole is arranged at the other end of the ejector rod (6), the other end of the ejector rod is connected with a first connecting rod (7) with a cylindrical boss, the first connecting rod (7), a second connecting rod (8) and a third connecting rod (9) are hinged sequentially, and the other end of the third connecting rod (9) is fixed relatively. Radial holes (51) used for mounting an upper lock pin (2) and a lower lock pin (3) are arranged at one end of the piston (5) close to the cavity of the ejector rod (6) and are distributed circumferentially, and grooves are arranged in the radial holes (51). An annular groove (10) is arranged in the cylinder body (4) and the lower lock pin (3) can be clamped into the annular groove (10). The upper position and the lower position of a hydraulic/pneumatic actuator cylinder can be locked by the aid of the actuator cylinder position locking and unlocking mechanism which is high in locking force, low in unlocking force and high in reliability.
Owner:JINCHENG NANJING ELECTROMECHANICAL HYDRAULIC PRESSURE ENG RES CENT AVIATION IND OF CHINA

Dumper tail structure with hydraulic locking device

The invention discloses a dumper tail structure with a hydraulic locking device. The upper part of a back door body is a hinge plate which is hinged with a hinge seat, the hinge seat is arranged at the upper end of a dumper box body, an oblong hole is formed in a connection part between the hinge plate and the hinge seat and is matched with a connecting shaft on the hinge seat, and the connecting shaft and the oblong hole can generate relative movement; a latch hook clamping shaft is arranged at the lower part of the back door body, and a hook clamping shaft is arranged between the hinge plate and the latch hook clamping shaft on the back door body and is clamped with a hook on the side wall of the dumper box body. According to the dumper tail structure with the hydraulic locking device, a back door and the hydraulic locking device use cooperatively, the locking effect is excellent, the fitting degree of the back door and the box body can be improved, and material leakage can be effectively prevented; the hydraulic locking device can further prevent the back door from jumping up, and ensure the safety and the reliability of a vehicle during using; the hydraulic locking device can further increase the pushing force of a hydraulic cylinder, and provides a larger locking force; the dumper tail structure with the hydraulic locking device has the advantages of being simple in operation, safe, reliable and high in controllability.
Owner:SINO TRUK JINAN POWER

Self-oriented large-fault-tolerance isomorphic interface for spacecraft and using method thereof

The invention provides a self-oriented large-fault-tolerance isomorphic interface for a spacecraft and a using method thereof. A gear wheel is driven to rotate by a motor by means of a worm, a supporting sleeve is driven to rotate by the gear wheel by means of a gear wheel key, the supporting sleeve rotates to drive an inner rotating cylinder to rotate firstly, for the movement of the inner rotating cylinder, a guide plate is pushed out through a meshed guide plate driving rod, a guide plate pushing rod and a rotating pin, meanwhile, a locking positioning pin is pushed out by the supporting sleeve, after the locking positioning pin and the supporting sleeve reach a limit station, the motor stops, after the interface is aligned, the motor is started again, the supporting sleeve drives a meshed telescopic sleeve to move through the driving rod, and a connecting key is used for clamping a concave part of the locking sleeve so as to complete locking. According to the interface and the method in the invention, self-oriented fault-tolerant butt joint with large butt joint initial deviation between spacecrafts can be achieved, multi-angle butt joint under the condition of multi-face connection is achieved, the interface structure is simple, the locking force is large, the size is compact, and high-reliability and large-fault-tolerance butt joint of the spacecraft can be met; meanwhile, the control is simple, the energy consumption is low, and the task cost of actual spacecraft butt joint can be saved.
Owner:NORTHWESTERN POLYTECHNICAL UNIV

Mold locking device of hollow plastic product forming machine

ActiveCN102848558BLarge locking forceAffect the clamping forceMolding machineMechanical engineering
The invention relates to a mold locking device of a hollow plastic product forming machine, belonging to the field of a plastic product forming machine. The hollow plastic product forming machine comprises a left mold frame and a right mold frame, the mold locking device comprises a mold-locking actuating cylinder, a mold locking box and a mold-locking actuating cylinder grabbing mechanism, wherein the mold locking box comprises a mold locking box body, a cover plate, a first guide plate and a second guide plate; the mold-locking actuating cylinder grabbing mechanism comprises an upper actuating cylinder, an upper actuating cylinder seat plate, an upper engagement clamp block, a lower actuating cylinder, a lower actuating cylinder seat plate and a lower engagement clamp block; and the mold-locking actuating cylinder is horizontally arranged on the left mold frame, and cylinder column engagement teeth are formed at the surface of a mold-locking actuating cylinder column of the mold-locking actuating cylinder, at one end facing the mold locking box body. The mold locking device has the advantages that the closing effect of one pair of semi-molds can be ensured; the upper engagement clamp block and the lower engagement clamp block can be prevented from deflection to affect clamping forces on the mold-locking actuating cylinder column; the stability of vertical movement of the upper engagement clamp block and the lower engagement clamp block can be maintained in a long time; and the structure can be simplified, large locking forces for the mold-locking actuating cylinder column can be obtained with small mold locking forces, and electric energy can be saved.
Owner:SUZHOU TONGDA MACHINERY

Combined machining hydraulic locking power tool table

ActiveCN104190973AAdapt to functional requirementsVersatileTool holdersPositioning apparatusDrive shaftControl engineering
The invention discloses a combined machining hydraulic locking power tool table, and belongs to machine tool parts. A plurality of power tool bases are arranged on a tool disc at intervals in the circumferential direction, the tool disc is fixedly connected with a transposition tooth disc and is supported through a bearing, and a gear shaft is meshed with a gear on the outer peripheral face of the transposition tooth disc for transmitting power of a tool changing drive motor. A lock oil cylinder piston is connected with a locking tooth disc through a connection piece to drive a tooth groove in the rear end face of the locking tooth disc to be correspondingly meshed with a tooth groove in the front end face of the transposition tooth disc and a tooth groove in the front end face of a fixing tooth disc fixed to a tool table base so as to achieve locking. A power drive motor transmits the rotating power to the power tool base through a drive shaft and a driven shaft which are connected in a transmission mode, the driven shaft and the power tool base are matched through a clamping groove and a clamping tenon, a driven shaft angle sensing mechanism feeds back signals to control the rotating angle of the driven shaft, the driven shaft is arranged in a radial driven shaft hole in a flange base through a bearing in a supported mode, and the tool table base is provided with a front transmission cavity and a rear transmission cavity which are used for passing of a transmission mechanism. The combined machining hydraulic locking power tool table is simple in structure and solves the problem that a traditional power tool table is complex in structure.
Owner:ZHEJIANG RIFA PRECISION MACHINERY

Intelligent production line for part manufacturing and working method thereof

The invention discloses an intelligent production line for part manufacturing and a working method thereof. The intelligent production line comprises a loading and unloading mechanism, a conveying mechanism, a production mechanism and a tray mechanism, wherein the conveying mechanism comprises a fixing frame and a truss rail which is fixed to the upper side of the fixing frame; the surface of thetruss rail is slidably connected with a mechanical arm assembly; and an inner cavity of the mechanical arm assembly is slidably connected with a lifting mechanical arm. The invention relates to the technical field of part machining. According to the intelligent production line for part manufacturing and the working method thereof, it is achieved that different parts are machined on a same device on the premise that a clamping way and cutting tools are not changed; by using a zero-point positioning module, the machined workpiece is fixed to a clamping tray; a truss robot grabs the clamping trayto place the clamping tray on a clamping base well fixed on a CNC machine; it is achieved that loading and unloading of the CNC machine are automatic; an operator clamps the workpiece on a loading table without occupying a machine tool; and it is achieved that one truss robot can be responsible for loading and unloading of multiple CNC machines.
Owner:AVIC POWER SCI & TECH ENG

Deployable hood device for stationary orbit remote sensing camera

A deployable hood device for a stationary orbit remote sensing camera belongs to the spaceflight field. The device comprises an optical-mechanical structure body, a multistage hood cylinder, a lockingmechanism and a cord sleeve driving mechanism. The multistage hood cylinder is fixed with the optical-mechanical structure body and achieves the compressed state by the locking mechanism; the stagesof the core sleeve driving mechanism is the same as that of the multistage hood cylinder; the sleeve of each stage of the cord sleeve driving mechanism is in rigid connection with the corresponding stage of the hood cylinder of the multistage hood cylinder, and the multistage hood cylinder achieves multistage sleeve unfolding through the cord sleeve driving mechanism; a main mirror is arranged inthe first stage sleeve of the cord sleeve driving mechanism; and the circumference of each stage of the locking mechanism is uniformly distributed on the corresponding stage of the multi-stage hood cylinder. The compression ratio of the deployable hood device is high; the driving force of the cord sleeve driving mechanism is large and the synchronism is high; the structural rigidity of the whole device in the compressed state is high, and the whole device can bear the vibration impact load during the launching; and the reliability of the locking / unlocking is high, and the locking force is large.
Owner:CHANGCHUN INST OF OPTICS FINE MECHANICS & PHYSICS CHINESE ACAD OF SCI
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