41results about How to "Improve launch accuracy" patented technology

The invention discloses a ballistic correction method for multi-bullet shooting. The ballistic correction method is realized through a detector, a command and control unit, a multi-bullet shooting assembly frame, a turret system, an integrated scheduling module, an angle calculating module and a data compensation module. By the method, left and right position deviation, upper and lower position deviation, heading error angles and pitching deviation angle of frame positions of the multi-bullet shooting assembly frame and an optical axis of the detector, error in ballistic resolving can be eliminated, and shooting precision can be improved.

The invention provides a method and system for calibrating radio frequency transmitting power. The method comprises the following steps: step S100: when the radio frequency transmitting power of a to-be-tested product is tested by using a plurality of theoretical power values, obtaining a plurality of measured power values corresponding to the theoretical power values, and a power-transmitting signal strength indication voltage curve; step S200: when the deviation between at least one measured power value and the corresponding theoretical power value is greater than a preset deviation threshold, dividing the power-transmitting signal strength indication voltage curve into a plurality of continuous areas, and selecting a to-be-calibrated area; step S300: calibrating each to-be-calibrated area to obtain a functional relationship between a transmitting signal strength indication voltage and the power of each calibrated area; and step S400: configuring the functional relationship between the transmitting signal strength indication voltage and the power of each calibrated area to the to-be-tested product. By adoption of the method and system provided by the invention, the transmitting precision of small power can be improved, thereby ensuring that the high power and the small power transmitted by a Wi-Fi product are relatively accurate.

The invention discloses a delayed expansion mechanism for folding rudder sheets of a small missile, and belongs to the field of missile attitude controlling. Each delayed expansion unit which is composed of a first adapter plate, a second adapter plate and a rudder sheet lock pushing rod is arranged corresponding to each rudder sheet, and the rudder sheets are stably locked in a rudder cabin segment by the delayed expansion units to ensure that the rudder sheets are still in a locking state after the small missile is launched; and in the process of the flight of the small missile, the lockingof the rudder sheets can be released and the expansion of the rudder sheets can be completed quickly by driving the rudder sheet lock pushing rods to move at any time so as to realize the locking anddelayed expansion of the rudder sheets. According to the delayed expansion mechanism, the structure is simple, the controlling is easy, the response is quick, the reliability is high, the working requirements of the folding rudder sheets can be fully met, the stable locking of the rudder sheets can be ensured, and the delayed expansion of the rudder sheets can be realized effectively, so that theflexibility and accuracy of the rudder sheet controlling are effectively improved, then the flight accuracy and controlling flexibility of the small missile are ensured, and good application and popularization value is achieved.

The invention relates to a vehicle-mounted six-degree-of-freedom platform. The vehicle-mounted six-degree-of-freedom platform comprises a base, a vertical vibration layer, a horizontal vibration layer, a pitching layer, a direction adjusting layer and an acceleration sensor, wherein the base is fixedly arranged on a simulated vehicle; the vertical vibration layer is arranged on the base and is used for simulating vibration of the simulated vehicle in the vertical direction; the horizontal vibration layer is arranged on the vertical vibration layer and is used for simulating the vibration of the simulated vehicle in the horizontal direction; the pitching layer is arranged on the horizontal vibration layer and is used for simulating a rotating direction of the simulated vehicle in the horizontal direction; the direction adjusting layer is connected with the pitching layer and is used for simulating a rotating direction of the simulated vehicle in the vertical direction; and the acceleration sensor is fixedly arranged on the base, is in circuit connection with the vertical vibration layer and the horizontal vibration layer, and is used for measuring the vibration of a vehicle body of the simulated vehicle and transmitting driving state direction parameters to the vertical vibration layer and the horizontal vibration layer. The vehicle-mounted six-degree-of-freedom platform has a simple structure, a small size, light weight and low cost; and by stimulating a vehicle driving state, researches on the influences on a vehicle-mounted aircraft positioning system are realized, and the launching precision of the vehicle-mounted aircraft under the vehicle driving state is improved.

The invention provides an air gun launching device with a quick release mechanism. The air gun launching device includes an air compressor, an air inlet valve, an air chamber, a launch valve, a firstpressure sensor, a second pressure sensor, a quick release mechanism, a PLC, a Laval acceleration pipe and a launching tube. The air compressor is connected with an air inlet of the air chamber through the air inlet valve, an air outlet of the air chamber is connected with one end of the quick release mechanism through the launch valve, the other end of the quick release mechanism is connected with the launching tube through the Laval acceleration pipe, the first pressure sensor is disposed at the position of the air chamber and used for monitoring a pressure value in the air chamber, the second pressure sensor is disposed at the position of the launch valve to be used for monitoring a pressure value of gas released at the position of the launch valve, and the PLC is electrically connectedwith the air inlet valve, the launch valve, the first pressure sensor, the second pressure sensor and the quick release mechanism. The device enables launched air flow to flow out quick evenly massively in a short time, and acts on the bottom of a projectile to promote the movement of the projectile.

The invention discloses a firefighting ball launching device of a firefighting unmanned aerial vehicle. The firefighting ball launching device comprises a machine body, wherein a fixed plate is fixedly connected with the inner wall of the machine body; a device cavity is arranged in the middle of the fixed plate; a threaded rod is arranged in the device cavity; two ends of the threaded rod are rotatably connected with the inner walls of the device cavity; a cylinder is arranged on the threaded rod in a sleeving manner and is in threaded connection with the threaded rod; a movable block is connected onto the cylinder in a sleeving manner and is movably connected with the cylinder; limiting discs are fixedly connected with two ends of the cylinder; an elastic device is arranged on a part, between the limiting discs and the movable block, of the cylinder; a worm wheel is fixedly connected onto the threaded rod; and the side walls of the worm wheel and the fixed plate are fixedly connectedwith a first drive motor; and the output of the first drive motor penetrates through the side walls of the fixed plate and extends into the device cavity. The firefighting ball launching device is reasonable in structural design, simple to operate and high in launching precision, can continuously launch firefighting balls and greatly improves the firefighting efficiency.

The invention aims at providing a tennis trainer which comprises a trainer rack, a launching mechanism and a horizontally-rotating mechanism. The tennis trainer is characterized in that the launching mechanism is fixed in the horizontally-rotating mechanism, and the trainer rack is positioned outside the horizontally-rotating mechanism and is connected with the horizontally-rotating mechanism. The tennis trainer has the characteristics of undemanding air pressure for tennis launching and high launching accuracy, and can realize the self rotation of the tennis and vividly simulation on playingtennis by human. Besides, the tennis trainer has the advantages of simple structure, lighter weight, high safety performance and lower overall cost.

The invention relates to an engineering supervision device, in particular to an engineering supervision construction management informationization device which comprises a camera, a carrying assemblyand a fire extinguishing device, wherein the carrying assembly comprises a vertical column and a mounting frame; the camera is connected with the mounting frame; the mounting frame is connected with adriving device for driving the mounting frame to rotate around the vertical column; the fire extinguishing device comprises a fire extinguishing grenade and a grenade launcher; the grenade launcher is rotationally connected with the mounting frame and fills the fire extinguishing grenade; the grenade launcher is connected with an adjusting device for controlling the launching elevation angle thereof; the camera, the driving device, the grenade launcher and the adjusting device are controlled by a monitoring system; the carrying assembly is used for mounting the camera and the fire extinguishing device, and through the rotation of the mounting frame, the monitoring scope of the camera and the acting scope of the fire extinguishing device are widened; during a fire, an operator can controlthe monitoring system to start an alarm and the fire extinguishing device and the grenade launcher launches the fire extinguishing grenade for extinguishing the fire or controlling spreading of the fire, so that the time is gained for subsequent firefighting.

The invention discloses a novel fire-fighting projectile and a launching system thereof. A break bulk fuse, a projectile powder box, a push plate, a projectile body, a fire extinguishing agent box, aprojectile band and a projectile tail assembly, wherein the break bulk fuse is mounted on the front end portion of the projectile body, the projectile powder box is arranged between the break bulk fuse and the push plate, the push plate is arranged at the front end of the fire extinguishing agent box, the fire extinguishing agent box is installed in the projectile body, the projectile band is arranged at the bottom end of the projectile body, the projectile tail assembly is installed at the rear end of the projectile body. The novel fire-fighting projectile launching system mainly consists ofa fire-fighting projectile launcher, a sighting device, sighting point solving software, a fire-fighting projectile firing table, a fire-fighting projectile transport cart and a fire-fighting equipment / material transport cart. By means of the novel fire-fighting projectile and the launching system, fire-fighting materials and life-saving equipment can be quickly and accurately delivered to an inaccessible fire scene within short time, and the characteristics of being long in transmission distance, high in launching speed, high in emission precision, safe, reliable and the like are achieved.

The invention provides a multifunctional launching training device based on modular design. According to the multifunctional launching training device based on the modular design, the problem that different ammunition can be launched through the same launching barrel is solved, meanwhile, rapidly filling can be carried out after launching so that next launching can be carried out, the impact force, the explosive force and the acousto-optic effect in the launching process can be truly simulated, the real launching condition of weapons in the real confrontation process can be simulated, and great significance can be achieved for improving the short-distance actual combat ability of soldiers. According to the technical scheme for solving the problem, the multifunctional launching training device is characterized in that the multifunctional launching training device comprises a launching barrel, a guiding module used for performing image transmission on a launching target is connected to the lower portion of the launching barrel in a sliding mode, and the guiding module is connected with the launching barrel in a sliding mode, a rocket projectile bearing block or a signal projectile launching module are connected above launching barrel in sliding manner, and the multifunctional launching training device has the advantages that the multifunctional launching training device is ingenious in structure, simple and practical.

The invention relates to the technical field of launching mechanisms, in particular to a launching mechanism based on a rigid ejector pin. The launching mechanism comprises a top plate, wherein a ball storage bin for storing elastic shots is fixedly connected to the bottom of the top plate, an ejector pin fixing seat is connected to a ball outlet of the ball storage bin, a ball outlet through hole is formed in the ejector pin fixing seat, a launching pipeline is connected into the ejector pin fixing seat, the ball outlet through hole communicates with the launching pipeline, a driving plate is rotationally connected into the ball storage bin and driven by a driving plate motor, a limiting assembly for limiting the elastic shots from passing through the launching pipeline is arranged on the ejector pin fixing seat, openings are symmetrically formed in the left side and the right side of the launching pipeline, launching friction wheels are arranged at the openings in the two sides of the launching pipeline, the launching friction wheels are driven by a brushless motor, and the launching friction wheels is located in front of the limiting assembly. According to the launching mechanism, the elastic shots can be preset, and the uncontrollable multi-shot situation is prevented, so that controllable single shot and multi-ball continuous shot are realized, and the overall shooting precision can be improved.

The invention relates to a mechanical rope throwing device. The mechanical rope throwing device mainly solves the problems that three-level launching is adopted in the prior art, the energy storage difference of a launching box of each level is large before launching, precision is poor, and in addition, the assembling work difficulty is high. The mechanical rope throwing device comprises a shell,and a launching device, an energy storage device and a clutch device are arranged on the shell. A launching channel is arranged in the shell, and the launching device is arranged at the inner end of the launching channel. A launching body is arranged at the position, located in the launching channel, on the shell and is located at the output end of the launching device. The input end of the launching device is connected with the output end of the energy storage device. The input end of the energy storage device is connected with the output end of the clutch device. The input end of the clutchdevice is provided with a driving device. The shell is provided with a locking device used for fastening a launching body in the launching channel.

The invention belongs to the technical field of aviation emergency rescue equipment, and particularly relates to high-rise building emergency rescue bombs launched through an airborne track. The bombinvolves a power module, a loading module and a blasting and dispersing module, wherein the loading module is detachably connected with the power module, and the blasting and dispersing module is detachably located in the loading module. According to the provided high-rise building emergency rescue bombs launched through the airborne track, the matched emergency rescue bombs can be quickly assembled for targeted disposal according to a fire type on site.

The invention discloses fireproof and explosion-proof combined fireworks which comprise a transmitting seat body (1), transmitting holes (2) of the transmitting seat body (1) and a fireproof cover plate (11). The transmitting seat (1) is made of light fireproof materials, a lead wire (3) is embedded in the transmitting seat body (1), the bottoms of the transmitting holes (2) are communicated with one another by the lead wire (3), inner barrels (8) are arranged in the transmitting holes (2), a lead hiding hole (4) is formed in the transmitting seat body (1), an ignition portion of the lead wire (3) is hidden in the lead hiding hole (4), the fireproof cover plate (11) is made of light fireproof materials, fireproof plugs (6) for the transmitting holes and a fireproof plug (5) for the lead hiding hole are formed in the fireproof cover plate (11), the fireproof cover plate (11) covers the transmitting seat body (1), the fireproof plugs (6) for the transmitting holes are inserted into the transmitting holes (2), and the fireproof plug (5) for the lead hiding hole is inserted into the lead hiding hole (4). The fireproof and explosion-proof combined fireworks have the advantages that the fireproof and explosion-proof combined fireworks are high in transmission precision and low in transmission powder usage, the transmitting holes are short, the manufacturing cost can be saved, the safety coefficient can be increased, the fireworks can be prevented from being ignited by external fire sources, and accordingly sympathetic detonation accidents can be completely eradicated during production, transportation and storage.

The invention discloses a lead-embedded firework launching base which comprises a launching base body (1) made of light materials and launching holes (2) of the launching base body (1). Leads (3) are embedded in the launching base body (1), the bottoms of the launching holes (2) are communicated through the leads (3), different connection modes are adopted by the leads (3) in the launching base body (1) according to different rules of firework launching, and the inner space of each launching hole (2) is an inverted cone with a small bottom and a large top. The lead-embedded firework launching base improves launching accuracy, reduces propellant dosage, lowers the height of the launching holes, saves manufacturing cost, improves a safety system, is rapid in setting-off rhythm, high in production efficiency, free of blaze phenomenon, environmentally friendly and various in launching form and saves energy.

The invention relates to a novel welding line detection device. The novel welding line detection device comprises a shell; a handle is arranged on the top of the shell; the handle is connected to a bracket; a probe is arranged on the bracket; the bottom of the probe is connected to a hand lever through a connecting part; the hand lever can be folded in 90 DEG; a cable is inserted into the handle lever; a protective cover is arranged outside the cable; one end of the cable is connected to a laser transmitter; the other end of the cable is connected to a processor in the shell; the processor isconnected to an ultrasound scanner; the ultrasound scanner is connected to a small hole on the shell through a reinforcement pipe; the ultrasound scanner is connected to a memory; the memory is connected to an adjusting button on a control panel embedded in the shell; and a display screen is arranged on the control panel. According to the novel welding line detection device in the invention, the detection precision and the working efficiency are increased; the stability is improved; the service life is prolonged; the bracket structure is steady and firm; the intuition is high; data is convenient to check; the device is convenient to use; and thus, the comprehensive economic benefits are increased.

The invention relates to the technical field of launching mechanisms, in particular to a launching mechanism based on an elastic ejector pin. The launching mechanism comprises a top plate, a ball storage bin for storing shots is fixedly connected to the bottom of the top plate, an ejector pin fixing seat is connected to a ball outlet of the ball storage bin, a ball outlet through hole is formed in the ejector pin fixing seat, a launching pipeline is connected in the ejector pin fixing seat, and the ball outlet through hole communicates with the launching pipeline; a shifting plate is rotationally connected into the ball storage bin and driven by a shifting plate motor, a limiting clamp used for clamping or loosening the shots entering the launching pipeline is arranged on the ejector pin fixing seat, openings are symmetrically formed in the left side and the right side of the launching pipeline, launching friction wheels are arranged at the openings in the two sides of the launching pipeline, the launching friction wheels are driven by a brushless motor, and the launching friction wheels are located in front of the ejector pin fixing seat. According to the launching mechanism, the shots can be preset, and uncontrollable multi-shot conditions are prevented, so that controllable single shot and multi-ball continuous shot are realized, and the overall launching precision can be improved.

The invention discloses a cartridge type automatic repeating crossbow. According to the cartridge type automatic repeating crossbow, a linear motor is mounted above a crossbow arm, a runner sliding block of the linear motor is provided with a string pulling mechanism of automatic string buckling and releasing, an arrow box for automatically supplying arrows is mounted at the bottom of the crossbowarm, and automatic winding of the crossbow and automatic launching of the arrows are achieved through combination of the linear motor and the arrow box. The cartridge type automatic repeating crossbow uses the reciprocating linear motor to drive the string pulling mechanism to automatically complete tension and release of a bowstring, so that automatic continuous launching of the arrows can be achieved by being matched with the arrow box, the launching speed of the crossbow is improved effectively, the cartridge type automatic repeating crossbow has the characteristics that the structure is simple, operation is convenient, labor saving is achieved in using, the launching precision is high, and problems of the prior art are solved.

The invention provides a launch module of a table tennis ball picking device, which includes a launch unit and a visual recognition unit; the launch unit is connected to the base and connected to the control unit for signals; The recognition part is installed at the launch end of the launch part; the control part controls the movement of the base based on the recognition information of the visual recognition part, and the control part controls the movement of the base to a preset distance position according to the recognition result, and adjusts the posture direction of the base; the control part Calculate the distance between the preset distance position and the target position according to the recognition information of the visual recognition part, adjust the initial launch speed of the launch part, control the launch part to adopt a circular rotation method, and launch towards the target launch direction at the initial launch speed, so as to realize Launch the ping pong ball to the target location. The invention can realize the adjustment of the launching speed according to the actual launching situation or the launching scene, not only improves the work efficiency of delivering the table tennis balls, but also can improve the launching accuracy of the table tennis balls.

The invention provides an electrothermal chemical firework launching device and method. The launching device comprises an electrothermal chemical firework bomb, a launcher and a discharging loop; the electrothermal chemical firework bomb is composed of a cartridge case, a plasma generator, an ablation material and firework projectiles, the launcher is composed of a body tube, a supporting system and a cartridge chamber, and the discharging loop is composed of a pulse power supply, a primary energy source and a high-voltage cable. Through adjustment of the waveform and amplitude of the pulse current generated by the pulse power supply, the temperature and pressure of the plasma generated by the plasma generator are controlled, so that different doing capacities are obtained, different launching initial speeds of the firework projectiles can be accurately obtained, the firework projectiles can reach the preset launching height needed by fireworks, the controllability of the firework launching height and launching direction can be enhanced, meanwhile, impact damage to firework projectiles in the launching process can be reduced, the firework launching precision and the mechanical rigidity of the firework launching device can be improved, and it is guaranteed that fireworks with specific characters or patterns are achieved according to the design effect.

The invention discloses an ecological treatment system for river surface water. The system comprises an information acquisition unit, a management server and an instruction transmission unit, the instruction transmission unit comprises an isolation filter circuit, an instruction amplification adjusting circuit and a power amplifier transmitting circuit. The isolation filter circuit carries out isolation output on a scheduling instruction signal by using a voltage follower principle, ensures the stability of instruction issuing, improves the current driving capability of the signal, eliminatesexternal high-frequency clutter interference by using a band-pass filter principle, and improves the precision of the scheduling instruction signal. The instruction amplification adjusting circuit performs two-stage amplification on the scheduling instruction signal, and a composite stable amplifier tube is designed, so that the stability effect of the amplification output of the scheduling instruction signal is well improved; the power amplifier transmitting circuit improves the transmitting precision of the scheduling instruction and maintains good transmitting power intensity, and finally the processed scheduling instruction is remotely transmitted by a signal transmitter E1 so as to realize efficient scheduling and effective control of the river surface water ecological management system.

The invention provides a recoil-free firework launching device adopting an electromagnetic counter-recoil mechanism and a firework bullet launching method. The launching device comprises a barrel, a movable powder chamber, a breech mechanism and an electromagnetic brake. According to the invention, rapid opening of a nozzle under different pressures is implemented by adjusting the electromagnetic resistance, the latch opening time and the closing time of pressure relief of a chamber pressure are controlled to adjust the tail jet flow pressure to implement initial speed control, and the launching height and the launching speed are controlled by controlling the bullet chamber exiting speed. According to the invention, the launching height and the launching speed can be controlled only by adjusting the current and the voltage which are input into the electromagnetic brake, impact damage to firework bullets in the launching process is reduced, the firework launching precision and the mechanical rigidity of the firework launching device are improved, and specific character or pattern fireworks are guaranteed to be implemented according to the design effect.

The invention provides an air gun launching device with a quick release mechanism. The air gun launching device includes an air compressor, an air inlet valve, an air chamber, a launch valve, a firstpressure sensor, a second pressure sensor, a quick release mechanism, a PLC, a Laval acceleration pipe and a launching tube. The air compressor is connected with an air inlet of the air chamber through the air inlet valve, an air outlet of the air chamber is connected with one end of the quick release mechanism through the launch valve, the other end of the quick release mechanism is connected with the launching tube through the Laval acceleration pipe, the first pressure sensor is disposed at the position of the air chamber and used for monitoring a pressure value in the air chamber, the second pressure sensor is disposed at the position of the launch valve to be used for monitoring a pressure value of gas released at the position of the launch valve, and the PLC is electrically connectedwith the air inlet valve, the launch valve, the first pressure sensor, the second pressure sensor and the quick release mechanism. The device enables launched air flow to flow out quick evenly massively in a short time, and acts on the bottom of a projectile to promote the movement of the projectile.