24 results about "Water rocket" patented technology

The utility model relates to an integrally-formed water rocket launcher base which is provided with a base main plate, a first connecting table protruding upwards is formed on the base main plate, a pair of pivot joint seats opposite to each other in a spaced mode is formed at the upper end of the first connecting table, a pair of coaxial pivot joint holes are formed in the pivot joint seats, and the pivot joint holes are communicated with the first connecting table. The water rocket launcher is assembled through screw and nut connection; second connecting tables protruding upwards are formed at the edges of a set of opposite sides of the base main board respectively, and U-shaped clamping grooves are formed in the two ends of each second connecting table respectively; three hollowed-out parts are further formed in the base main plate, and an assembling accessory of the water rocket launcher is formed in each hollowed-out part. By means of the structure, when the emitter base is integrally formed, another three emitter spare and accessory parts can be formed at the same time, and therefore the number of molds needed by production of the whole emitter is reduced, and production cost is greatly reduced; spare and accessory parts of the emitter and the base can be stacked, so that the occupied space is reduced, and the packaging and transportation cost is reduced.

The utility model relates to a quick connector for a multistage water rocket bottle body capable of being provided with an air separator, which comprises an integrally formed connector body, the connector body is divided into two sections which are communicated in a penetrating manner along the axial direction, one section is a straight-through quick plug connector shell, the other section is a bottle mouth connector, and the air separator is arranged on the bottle mouth connector. A sealing rubber ring, a limiting clamp spring and an annular end cover are installed in the straight-through quick-plug connector shell, and an external thread and a positioning convex ring are formed on the outer portion of the bottle opening connector. The length of the straight-through quick-plug connector shell is equal to that of the bottle opening connector. When the quick connector is used for connecting the spliced water rocket bottle body and the air separator, each stage of rocket body can be connected by only one bottle body, so that the bottle body and the air separator can be quickly assembled, the efficiency is improved, and convenience is brought to a user.

1. The name of the design product: double-head bottle assembly (water rocket). 2. The use of the design product: multi-stage bottle for teaching model water rocket. 3. The design points of the design product: in shape. 4. The picture or photo that best indicates the design points: combined state Figure 1. 5. The assembly 2 pitch view rotated 90 degrees is the same as the assembly 2 left view, omitting the assembly 2 pitch view; the assembly 2 right view is the same as the assembly 2 left view, omitting the assembly 2 right view. 6. Other circumstances that need to be explained Assembly Explanation: Assembly 1 is a double-head bottle, and Assembly 2 is a connecting head. 7. Other circumstances that need to be explained Other Explanation: This product can be connected by N Assembly 2 and N+1 Assembly 1 in turn, and combined state Figure 1 is 1 Assembly 2 and 2 Assembly 1 connected in turn, combined state 2 is 2 Assembly 2 and 3 Assembly 1 connected in turn, and so on.

The utility model relates to an extension spray pipe for a water rocket and the water rocket, the extension spray pipe comprises a hollow spray pipe, one end of the hollow spray pipe is provided with an internal thread interface which is in butt joint with a bottle opening at the bottom of a water rocket body, and the other end of the hollow spray pipe is provided with a clamping flange which is connected with a water rocket launcher. And a parachute device is mounted on the extended spray pipe. After the scheme is adopted, the extension spray pipe is additionally arranged below the bottle opening of the water rocket body, the path is longer when water or gas in the water rocket is sprayed in the linear direction where the axis of the extension spray pipe is located, and therefore the directionality of water rocket launching can be better, and the whole water rocket can obtain a better launching effect; the extension spray pipe provides a better and more convenient installation part for the parachute device, the current situation that a traditional water rocket parachute can only be installed on the head of a water rocket is changed, the installation structure of the parachute and the structure of a water rocket body are simplified, and the flying effect of the water rocket cannot be affected when the parachute is installed on the lower portion.

The utility model relates to the technical field of water rocket experimental equipment, in particular to a water rocket altimeter, which comprises a power supply module, an attitude data acquisition module, a data transmission module, a remote control receiving module and an electromagnetic lock driving module, the power supply module is electrically connected with the attitude data acquisition module, the data transmission module, the remote control receiving module and the electromagnetic lock driving module, the attitude data acquisition module is in communication connection with the data transmission module, and the remote control receiving module is in signal connection with the electromagnetic lock driving module through a signal line. A remote control signal is received through the GLX433RX module, a macro relay HFD / 3 is triggered through an S8050 triode, and an SX1308 boosting chip is matched to drive an electromagnetic lock to achieve 0.1-second top-speed parachute opening. The ten-axis sensor and the full-duplex module form closed-loop control to adjust the parachute opening time in real time; the shunt power supply ensures stable operation of strong current and weak current, the RS485 serial port and 433MHz wireless anti-interference design ensures accurate execution of instructions, and the improvement of high performance and reliability of the water rocket altimeter is realized.

The application relates to a water rocket structure for vertical autonomous recovery, which comprises a head cone part, an attitude control part coaxially connected with the head cone part, a water storage main body part coaxially connected with the attitude control part, a main nozzle part connected with the water storage main body part, a control unit and an altimeter; the control unit is arranged in the head cone part; the altimeter is arranged at the bottom of the water storage main body part; an electrical circuit pipeline is connected between the head cone part, the attitude control part and the main nozzle part, and the control unit is connected with the attitude control part, the main nozzle part and the altimeter through the electrical circuit pipeline; a water supply pipeline is connected between the attitude control part and the main nozzle part. The water rocket is safe and reliable, the test condition construction is simple, and the test data is reliable.

The invention relates to a lateral inflatable water rocket launcher suitable for a rocket body with a nozzle, which comprises an integrally formed launcher main body, the launcher main body is provided with a transverse platform, and a hollow cylindrical nozzle butt joint part in which the nozzle of the rocket body is internally inserted is upwards formed in the middle of the upper surface of the transverse platform; an air inflation part is further formed on one side wall of the transverse platform in a protruding mode, and an air inflation channel communicated with the interior of the nozzle butt joint part is formed in the air inflation part and the interior of the transverse platform; a pair of vertical side walls are upwards formed on the two sides of the transverse platform, and the vertical side walls are higher than the nozzle butt joint part; the launcher main body can be used for launching a water rocket body with a nozzle, after a common bottle body is connected with the nozzle, butt joint is achieved through sealing of the nozzle and the sealing ring and the nozzle butt joint part, and therefore the launcher is matched with launching of the water rocket with the nozzle; in addition, the nozzles with different nozzle inner diameters can be replaced, and emission effects such as different emission speeds and durations are correspondingly obtained.

A separating device for a water rocket comprises an upper connector, the upper connector is connected with an upper-stage water rocket body, a breather pipe penetrates through the upper connector, extends downwards and penetrates through a lower connector, the lower connector is connected with a lower-stage water rocket body, the breather pipe is sleeved with a separating hose, and a second one-way air valve is arranged at the lower end of the separating hose. The separation hose is sleeved with an air storage pipe, air holes are formed in the pipe wall of the air storage pipe, and a first one-way air valve is arranged at the lower end of the air storage pipe. The gas storage pipe is arranged, the gas holes are formed in the gas storage pipe, the gas storage pipe has a buffering effect on pressure release, so that the effect of delayed separation can be started, and the device is simple in structure, light in weight and high in separation success rate.

This utility model discloses an electrolytic water rocket launching game device, comprising: a steel frame with a waterproof anchor bolt fixing seat at the bottom to support the entire device body; within the device body, the operating console includes: a host computer and a start button and a launch button connected to the host computer respectively; the electrolysis system consists of a hand-cranked generator and a transparent electrolytic cell; the positive and negative terminals of the hand-cranked generator are located in the two tubes of the transparent electrolytic cell respectively; the host computer controls the circuit switching of the hand-cranked generator; the gas drive mechanism consists of a gas collection chamber, a pressure relief valve, and a piezoelectric igniter; the pressure relief valve is installed on one side wall of the gas collection chamber and connected to the host computer; the piezoelectric igniter is installed on the other side wall of the gas collection chamber and connected to the host computer; the top of the gas collection chamber abuts against the bottom of the rocket model; the rocket model is located in a vertical glass pipe. This device integrates the complex electrolysis, gas collection, and ignition processes into a single operating console, simplifying operation, enhancing interaction, and providing structural stability and high durability.

The application belongs to the field of water rocket testing, and particularly relates to a water rocket testing system and method, which comprises a power source assembly, a thrust device, a support and a connecting pipe. The power source assembly comprises a sealed cylinder and an inflator connected with each other, and the sealed cylinder is provided with a water injection mechanism. The thrust device is arranged on the support, and the support is further provided with a sensor for monitoring the state of the thrust device. One end of the connecting pipe is connected in a cavity of the thrust device, and the other end extends into the bottom of the sealed cylinder. The testing system provided by the application can realize long-time stable pressure or variable pressure thrust experiment of the thrust device, and the pressure and water quantity in the cavity will not sharply decrease when the nozzle is opened as in the conventional thrust device, thereby the power parameters of the thrust device can be observed and studied for a long time, the influence of the flowmeter on the thrust is excluded during the thrust experiment of the thrust device, the mass flow and other related parameters can be measured with high precision, and data support is provided for scientific research, so that the related model can be better corrected.

The utility model relates to a time-adjustable air separator for a multi-stage water rocket, which comprises a first pipe body and a hose, and the inner diameter of the hose is smaller than the outer diameter of the first pipe body so as to form expanded connection when the first pipe body is inserted into the hose; the upper end opening of the hose is provided with a radial flange which is arranged outwards, and the lower surface of the radial flange of the hose is further provided with a sealing groove and a connecting convex ring and is connected with a second pipe body; a pressure relief hole is formed in the pipe wall of the second pipe body; the bottom of the hose is provided with a connecting through hole and a first one-way valve; and the bottom of the second pipe body is provided with a mounting hole communicated with the interior and a second one-way valve. The time-adjustable air separator can be used for quickly inflating a multi-stage rocket body and adjusting the separation time of the rocket body, so that the launching operation efficiency can be improved, a self-provided sealing structure and a simplified product structure are realized through the radial flange, the sealing groove and the like which are formed by the hose, and the assembling time and the material cost are saved.

The utility model relates to a water rocket launcher capable of being inflated laterally, which comprises an integrally formed launcher main body, the launcher main body is provided with a hollow rocket body inserting pipe, and a radial platform protruding in the radial direction is formed at the bottom of the rocket body inserting pipe; an air inflation part is further formed on one side of the radial platform in a protruding mode, and an air inflation channel communicated with the inside of the arrow body inserting pipe is formed in the air inflation part and the radial platform. The transmitter further comprises a transmitter base, the transmitter base is provided with a base main board, three hollowed-out parts are further formed in the base main board, and lock catch releasing parts, first inserting strips and second inserting strips are formed in the hollowed-out parts respectively. According to the utility model, the emitter main body is integrally provided with the lateral inflation part and the built-in inflation channel, so that inflation operation can be carried out from the lateral direction; when the emitter base is integrally formed, another three emitter spare and accessory parts, namely the first inserting strip, the second inserting strip and the lock catch releasing part, can be formed at the same time, so that the number of molds required by production of the whole emitter is reduced.

The invention discloses an anti-unmanned aerial vehicle water rocket and a guidance method, and relates to the technical field of guidance, and the anti-unmanned aerial vehicle water rocket is characterized by comprising an unmanned aerial vehicle defense station and an anti-unmanned aerial vehicle water rocket; the unmanned aerial vehicle defense station comprises a base, the base is fixedly connected with a dry ice pill storage tank, the dry ice pill storage tank is fixedly connected with a group of dry ice conveying channels, each dry ice conveying channel is fixedly communicated with a water rocket launching cylinder, and an anti-unmanned aerial vehicle water rocket is matched with the water rocket launching cylinder; the dry ice pill storage tank is fixedly connected with the laser designator, and the laser designator is fixedly connected with the multispectral comprehensive photoelectric unmanned aerial vehicle detection system; the anti-unmanned aerial vehicle water rocket comprises a water rocket cavity, the water rocket cavity is fixedly connected with an LED beacon and a net gun device, a dry ice chamber is fixedly connected into the water rocket cavity, a fragile film is arranged on the lower side of the dry ice chamber, and saturated salt water is contained in the water rocket cavity. The technical problem to be solved by the invention is to provide the anti-unmanned-aerial-vehicle water rocket and the guidance method, so that anti-unmanned-aerial-vehicle water rocket guidance is facilitated.

This utility model relates to the field of water rocket landing chamber technology and discloses a water rocket parachute chamber, including a water rocket body. A disc is provided on the top of the water rocket body, and a through mounting hole is opened on the disc. The disc is fitted onto the top of the water rocket body through the mounting hole. A through threading hole is opened on the disc. A ring is fixedly connected to the disc. Solid cylinders A and B are symmetrically fixedly connected to the outer circumference of the disc ring. Through the design of the blocking column, the tilting driving force can be strengthened and the separation efficiency can be improved. That is, when the elastic band A is released and a rapid rebound occurs, the rebound force acts on the blocking column to generate an impact force. This impact force directly exacerbates the tilting of the parachute chamber towards the solid cylinder A. The above-mentioned actively enhanced tilting trend allows the parachute chamber cover to detach from the main body more quickly and thoroughly, avoiding separation jamming caused by insufficient tilting force, and greatly improving the overall separation efficiency of the cover.

This invention belongs to the field of educational demonstration products, specifically relating to a water rocket, a launch system, and a launch method. The water rocket includes a rocket body and a piston. The rocket body has a hollow cavity, and the piston is slidably and sealed within the cavity, dividing the cavity into a secondary cavity and a main cavity. The rocket body is equipped with an inflation nozzle I communicating with the secondary cavity and an inflation nozzle II communicating with the main cavity. A nozzle is also provided at the end of the rocket body away from the secondary cavity. During flight, as the pressure in the main cavity gradually decreases, the pressure in the secondary cavity becomes higher than that in the main cavity, pushing the piston towards the main cavity. This maintains the pressure balance in the main cavity, ensuring stable thrust during flight and partially compensating for the pressure loss in the main cavity, guaranteeing the thrust provided by the main cavity, and further improving the kinetic energy and speed of the water rocket.

The application belongs to the field of teaching demonstration supplies, and particularly relates to a horizontal flight water fire arrow, a launching system and a launching method, wherein the horizontal flight water fire arrow comprises an arrow body and a bend pipe; the arrow body is internally provided with a cavity, and the arrow body is further provided with a gas filling nozzle II and a nozzle which are in communication with the cavity; the bend pipe is arranged in the cavity, one end of the bend pipe is in communication with the nozzle, and the other end is arranged in abutment with the inner side wall of the cavity after being bent. The application can realize small-inclination or horizontal launching and flight of the water fire arrow by arranging the bend pipe, and provides a launching and flight mode which is different from conventional water fire arrows.

The utility model discloses a water rocket parachute opening device which comprises a connecting sleeve head and an outer cover which are arranged between two rocket bodies, the two rocket bodies are connected through a butt joint, the connecting sleeve head is arranged on the butt joint in a sleeved mode, a support used for installing a parachute opening control piece is arranged on the side face of the connecting sleeve head, and the outer cover can surround the rocket bodies to form a parachute containing area. An elastic pull rope is connected to one side of the outer cover, and a mounting hole matched with the parachute opening control piece is formed in the outer cover; the side opening type parachute opening structure is adopted, the parachute bin body is constructed on the basis of an original water rocket, it can be guaranteed that the parachute is smoothly opened, device components are greatly simplified, manufacturing cost is reduced, operation is convenient and fast, and the side opening type parachute opening device is more suitable for being widely used in teaching demonstration.

This utility model relates to a delayed-release air-separation lower-stage rocket assembly connector for water rockets, used to connect two rocket bodies to form a single lower-stage rocket body. The assembly connector has a hollow screw body and a one-way valve body that is hollowly connected to the interior of the hollow screw body. The assembly connector also has a micro-hole communicating with an internal airflow channel of the hollow screw body. When the lower-stage rocket body is assembled, the micro-hole and the one-way valve body are located within the same rocket body, and the hollow screw body extends into the other rocket body. During water rocket launch, after the lower rocket body loses pressure, the air pressure in the upper rocket body can only be slowly released to the lower rocket body through the micro-hole. This significantly prolongs the depressurization time in the upper rocket body, thereby extending the time for triggering the air-separator assembly to achieve release and separation. This extends the separation time between the upper and lower rocket bodies, allowing for an interval of 1-2 seconds between launch and separation, which is more than 10 times longer than existing technologies.

The utility model relates to the technical field of water rockets, in particular to a jet orifice of a water rocket, which comprises a water outlet pipe connected to an outlet of a water storage tank of the water rocket, spiral threads for assisting in water storage are arranged on the inner wall of the water outlet pipe to increase the rotating speed of water flow, and a detachable water outlet disc is arranged at an outlet of the water outlet pipe. A plurality of jet holes are formed in the water outlet disc; a mounting ring is arranged on the outer side edge of the water outlet pipe, butt joint columns are arranged on the periphery of the water outlet disc, and the butt joint columns are connected with the mounting ring through screws. The water rocket is reasonable in structure, the performance and flexibility of the water rocket are improved through the design of the threads, the detachable water outlet disc and the jet holes, and the water rocket is suitable for various scenes such as education, entertainment and scientific research.

The present application relates to a kind of adjustable time delay air separation and water rocket with the separator.The separator includes: a first pipe body, through the first pipe body to the upper level rocket body inside inflation;A first sealing joint, the lower end of first sealing joint is sealed and connected with a hose, the lower end of hose is connected with a one-way valve, the first pipe body is inserted from the first channel upper end of first sealing joint and extends to the inside of hose to form expansion joint;A second pipe body is connected with first sealing joint and the sleeve of the hose and one-way valve in it, the lower end of the second pipe body is connected with inlet and outlet air regulating valve.The separator and water rocket of the present application, through the sealing space of a second pipe body component and its inlet and outlet air regulating valve, realize the pressure relief speed controllable in the sealing space, and then can control the time of two-stage rocket body separation, so that two-stage rocket body can be delayed separation, control in better flight height and time opportunity separation, realize better simulation experiment effect.

This invention relates to a claw-type launcher for water rockets, comprising an integrally formed launcher body and two claws, each claw having a latching portion at its upper end; limiting crossbars facing each other are formed on the same side of the two latching portions; the launcher also includes a limiting mechanism for restricting and releasing the two limiting crossbars. When the limiting mechanism restricts the limiting crossbars, the claws and latching portions cannot move; when the limiting mechanism releases the limiting crossbars, the limiting crossbars, claws, and latching portions can open; with the above structure, the invention utilizes the limiting crossbars extending from the claws for limiting locking and releasing, resulting in a shorter release stroke and better release synchronization of the limiting mechanism, facilitating launch; the limiting mechanism structure is versatile, enabling various launch methods, such as relay launch of multiple water rockets, mortar-style launch, etc., bringing different launch effects and meeting the needs of more users.

This utility model discloses a multifunctional base for making water rockets, relating to the field of water rocket manufacturing technology. It includes a cola bottle and a cylindrical base. The cylindrical base is snapped into the cola bottle. A threaded through hole is formed at the center of the bottom of the cylindrical base. Four sets of strip-shaped grooves are evenly spaced on the cylindrical base. The top of the cylindrical base abuts against a semi-circular card. Two sets of semi-circular cards are provided, with their inner walls abutting against the outer wall of the cola bottle. A trapezoidal placement block is provided on the outer wall of the cylindrical base. The threaded through hole is threadedly connected to a threaded collar, which is connected to a bottom blocking plate. The bottom blocking plate abuts against the cylindrical base. Through the snapping of the cylindrical base with the cola bottle and the abutting action of the semi-circular cards, the cola bottle is stably fixed, effectively preventing the bottle from shaking during drilling and ensuring that the drilled hole is centered on the cola bottle. The strip-shaped grooves on the cylindrical base reduce the weight of the base while limiting the position of the tail fin attachment, ensuring the symmetry of the tail fin attachment.

The application provides a device, method, equipment and storage medium for automatically launching a water rocket, which comprises a power gas pump module, a gas-liquid control unit, a water storage tank, a release assembly and a pressure sensor. The power gas pump module comprises a plurality of gas output sides, the plurality of gas output sides are connected with a first electromagnetic valve and a second electromagnetic valve in the gas-liquid control unit, and the second electromagnetic valve is connected with the release assembly. The water storage tank comprises an input side, an output side and a bidirectional transmission side, the input side is connected with the first electromagnetic valve, the output side is connected with a fourth electromagnetic valve in the gas-liquid control unit, and the bidirectional transmission side is connected with a third electromagnetic valve in the gas-liquid control unit, and the third electromagnetic valve is connected with the release assembly. The pressure sensor is connected with the release assembly. The release assembly comprises a rudder and a release element. Through the device, the effect of fully automatically launching the water rocket can be achieved.

The application discloses a water rocket assembling and launching system matched with a VR simulation, which comprises a supporting table, a part placing platform and a launching platform are arranged on the supporting table, the part placing platform is provided with a part placing area and a finished product placing area, the part placing area is used for placing water rocket parts which have not been assembled, and the finished product placing area is used for placing a launching device; the part placing platform comprises a first groove and a sliding plate, the first groove is communicated with the right side wall of the part placing platform, the sliding plate is slidingly arranged on the first groove, the finished product placing area is arranged on the sliding plate, a second groove which is located on the same horizontal line with the first groove is arranged on the launching platform, and the second groove is communicated with the left side wall of the launching platform; and the application aims at solving the problem that the existing VR system cannot connect virtuality with reality, thereby resulting in poor practicability.