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766results about How to "Reduce shock load" patented technology

Method for controlling temporary flush type supersonic velocity wind tunnel with ejector function

The invention provides a method for controlling a temporary flush type supersonic velocity wind tunnel with an ejector function. The method includes that when the wind tunnel is started, firstly, the total pressure of a gas collection chamber of an ejector is adjusted to be working total pressure, then the total pressure of a stable section is adjusted to be a running total pressure value of a wind tunnel test, and then the ejector is closed for carrying out the wind tunnel test; and after specified testing items are finished, the total pressure value of the stable section maintains the same, the ejector is started to adjust the total pressure of the gas collection chamber to be a working total pressure value in a closed-loop mode, then gas flow is cut off, after the total pressure of the stable section is reduced to a preset cutoff total pressure value, the ejector is closed, and then a whole air-blowing testing process is finished. Through the method for controlling the temporary flush type supersonic velocity wind tunnel with the ejector function, the impact load in a start-up process of the wind tunnel and the impact load in a cutoff process of the wind tunnel can be reduced effectively, safety of models, a balance and a wind tunnel system can be guaranteed, requirements of the balance on strength and rigidity in a designing process of the balance can be effectively reduced, sensitivity of the balance can be improved, and the accuracy of the measurement of the balance and the quality of testing data can be improved.
Owner:INST OF HIGH SPEED AERODYNAMICS OF CHINA AERODYNAMICS RES & DEV CENT

Charging control method for energy-storage charging station

The invention relates to a charging control method for an energy-storage charging station. The method comprises the following steps: receiving a charging request from a vehicle; calculating current total power demand of the energy-storage charging station; judging whether the total power demand is higher than current load capacity of a power distribution network or not; controlling the energy-storage charging station to enter a pure-power-grid power supplying mode if the total power demand is not higher than the current load capacity of the power distribution network, and supplying power to a charging terminal and an energy storage system in the energy-storage charging station by the power distribution network; judging whether the current load capacity of the power distribution network is higher than a minimum load threshold or not if the total power demand is higher than the current load capacity of the power distribution network; judging whether the electric quantity of the energy storage system in the energy-storage charging station is greater than a first electric quantity or not if the current load capacity of the power distribution network is higher than the minimum load threshold; controlling the energy-storage charging station to enter a partial-dependency power supplying mode if the electric quantity of the energy storage system is greater than the first electric quantity, and supplying power to the charging terminal in the energy-storage charging station jointly by the energy storage system and the power distribution network. The charging control method for the energy-storage charging station has the advantage that the load impact on the power grid during charging can be effectively lowered.
Owner:SHENZHEN CLOU ELECTRONICS

Self-adaption claw mechanism of spatial on-orbit service robot

Disclosed is a self-adaption claw mechanism of a spatial on-orbit service robot. The self-adaption claw mechanism is composed of a self-adaption claw, a motor, a transmission mechanism of the motor and a base part. The self-adaption claw is used for achieving the function of on-orbit target object capturing. The motor and the transmission mechanism of the motor are used for transmitting torque, and the motor provides active torque. The base part is used for maintaining the relative positions of all the parts of a system. The self-adaption claw mechanism has adaptivity, so that grabbing modes can be selected in a self-adaption mode according to the shapes of target objects, and the universality is strong. The claw mechanism has auto-stability, and after the claw mechanism makes contact with the target objects, the post grabbing process is prone to self-stabilization due to the fact that a torsion spring which has the effect of adjusting the torque in a passive mode is adopted. The active and passive composite driving design with the single motor and the torsion spring combined is adopted in the mechanism, so that control strategies are simplified, and impulsive loads can be effectively buffered. The self-adaption claw mechanism is applied to the on-orbit robot, and greatly improves the task executing efficiency.
Owner:BEIHANG UNIV

First-child-stage parachuting-recovery carrier rocket

The invention relates to a first-child-stage parachuting-recovery carrier rocket. The first-child-stage parachuting-recovery carrier rocket is combined by two stages of rockets and comprises a recovery system arranged in a shell of a first-child-stage rocket, wherein the recovery system comprises a speed reducing device and a buffering device; the speed reducing device is arranged at the position close to the interstage section of the shell and comprises a supporting frame connected with the inner wall of the shell; a parachuting device is arranged on the supporting frame and is used for reducing the speed of the separated first-child-stage rocket in the falling process; the buffering device comprises two buffering airbags, one buffering air bag is arranged at the position close to the interstage section, the other buffering airbag is arranged at the position close to the tail section, and the two buffering airbags are used for buffering the first-child-stage rocket in the landing process. The first-child-stage parachuting-recovery carrier rocket has the advantages that the first-child-stage rocket can land smoothly without damage under the common action of the buffering device and the speed reducing device, so that non-damage recovery of the first-child-stage rocket can be realized, and the first-child-stage rocket can be secondarily utilized, so that the launching cost can be reduced.
Owner:CHINA ACAD OF LAUNCH VEHICLE TECH

Independent suspension system and crane with same

The invention discloses an independent suspension system. Two suspension oil cylinders are arranged between wheel edges of wheels on two sides and a frame respectively, and a steering mechanism drives the wheels on the two sides to perform steering. Two upper V-shaped swing rods and two lower V-shaped swing rods are arranged corresponding to the wheels on the two sides. Rod connection end portions of the two upper V-shaped swing rods are hinged to the upper portions of the wheel edges of the wheels on corresponding sides through spherical hinges respectively, and rod separation end portions of the two upper V-shaped swing rods are hinged to fixing members fixed below the frame along the lateral direction. Rod connection end portions of the two lower V-shaped swing rods are hinged to the lower portions of the wheel edges of the wheels on corresponding sides through spherical hinges respectively, and rod separation end portions of the two lower V-shaped swing rods are hinged to the fixing members fixed below the frame along the lateral direction. By means of the independent suspension system, possible frustrating effects caused by the suspension oil cylinders can be avoided, mutual independent motion of the wheel on the left side and the wheel on the right side can be achieved reliably, adhesion conditions of the ground are fully utilized, and control stability of the complete machine is improved. On the basis, the invention further comprises a crane with the independent suspension system.
Owner:XUZHOU HEAVY MASCH CO LTD

Compound bit formed by PDC (polycrystalline diamond compact) bits and rotary cutting bit

The invention discloses a compound bit formed by PDC (polycrystalline diamond compact) bits and a rotary cutting bit. The compound bit comprises a main body (1), rotary cutting bit cones (2), rotary cutting bit cutting teeth (3), PDC blades (4), PDC cutting teeth (5), oil storage sacs (6) and nozzles (7), wherein the main body (1) comprises a cone journal, centralizing blocks, high-pressure slurry channels and a connection screw thread. The compound bit is characterized in that a compound bit cutting unit comprises the rotary cutting bit and a PDC bit cutting unit. The compound bit has the following beneficial effects: the PDC bits complete drilling the central part of the borehole in the drilling process; the linear velocity of the periphery of the borehole is high in the drilling process and the rotary cutting bit and the PDC bit cutting unit complete drilling the periphery of the borehole; and the rotary cutting bit in the compound bit shocks, crushes and cuts the rocks by way of rotary cutting, has high central rock breaking efficiency, high rate of penetration and better dynamic performance, is uniform in wear, simultaneously improves the bit bearing structure, ensures to prolong the service life of the bit while improving the rock breaking efficiency, improves the cutting capability of the compound bit and ensures good gauge protection effect.
Owner:SICHUAN DEEP & FAST OIL DRILLING TOOLS CO LTD
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