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46 results about "Water rocket" patented technology

A water rocket is a type of model rocket using water as its reaction mass. The water is forced out by a pressurized gas, typically compressed air. Like all rocket engines, it operates on the principle of Newton's third law of motion. Water rocket hobbyists typically use one or more plastic soft drink bottle as the rocket's pressure vessel. A variety of designs are possible including multi-stage rockets. Water rockets are also custom-built from composite materials to achieve world record altitudes.

Two-stage water rocket capable of being separated by air friction

The invention discloses a novel two-stage water rocket capable of being separated by air friction. The two-stage water rocket capable of being separated by the air friction comprises a one-stage rocket body, a two-stage rocket body, a parachute and a launch frame. The two-stage water rocket capable of being separated by the air friction is characterized in that the one-stage rocket body and the two-stage rocket body are connected through a separating controller, a separating control wing is arranged at the bottom of the one-stage rocket body, the separating control wing is fixedly connected with a hanging stack on the separating controller through a steer wire rope. A shackle switch, a barometer and a directional guide rail are arranged additionally on the launch frame. A manner of external force controlling trigger and separation is used, air friction which is impacted on the separating control wing in the accelerated rising process of a first stage water rocket is used skillfully for controlling the separation, and thrust of the one-stage rocket body is used fully, and an air pressure difference between the one-stage rocket body and the two-stage rocket body is small. Controllability and safety can be improved. The shackle switch is used for controlling the water rocket to launch, and a gas tube is prolonged. The barometer, the directional guide rail, the parachute and the like are installed. The controllability and the safety of the water rocket can be improved. The two-stage water rocket capable of being separated by the air friction is simple in structure, convenient to operate, safe, environment-friendly and stable in performance.
Owner:GUANGXI NORMAL UNIV

Fairing separation mechanism, water rocket model with same and teaching aid

The invention discloses a fairing separation mechanism, a water rocket model with the same and a teaching aid, the fairing separation mechanism comprises two groups of fairings, an accommodating cavity is formed between the two groups of fairings, a carrier plate is arranged in the accommodating cavity, and a main plate is arranged below the carrier plate; a plurality of groups of first elastic separation parts are connected between the fairing and the main plate, a plurality of groups of second elastic connection parts are connected between the carrier plate and the main plate, the first elastic separation parts and the second elastic connection parts are connected with breaking parts, and the breaking parts are fixedly connected with the main plate; and the water rocket model comprises a fairing separation mechanism, a rocket body, a parachute, an empennage, a clinker bottle and a tail jet. Separation of the fairing is guaranteed through the first elastic separation part and the second elastic connection part, the parachute is bounced and separated under the action of the second elastic connection part, it is guaranteed that the parachute can be opened in real time, and factors influencing the flight attitude and height of the rocket are explored by changing conditions.
Owner:北京九天微星科技发展有限公司 +1

Water rocket pressure-operated interstage locking-separating device

The invention discloses a water rocket pressure-operated interstage locking-separating device, which comprises an upper base, a lower fixing anchor seat, a supporting stand column, a piston-spring assembly and a locking-separating device. The lower fixing anchor seat is sleeved and fixed at the upper end of the rocket body of a lower-stage water rocket; the piston-spring assembly comprises a cylinder barrel, a piston, tension springs and a tension spring hanging rod, the cylinder barrel is fixedly arranged on the periphery of an upper end opening of a rocket body of the lower-stage water rocket in a sleeving mode, the piston is communicated with the interior of the lower-stage water rocket and keeps consistent pressure, the tension spring hanging rod is fixed to the piston, one end of each tension spring is hung at the two side ends of the tension spring hanging rod respectively, and the other end of each tension spring is fixed on the cylinder barrel; and the locking-separating device is fixed to the upper base, and an upper-stage water rocket body is connected to the locking-separating device. According to the device, locking and separating of all stages of the water rocket are achieved, the overall lift limit of the water rocket is improved, the functions of the water rocket and the load capable of being carried by the water rocket are expanded, the working pressure range is wide, and the pressure adjusting freedom degree is high.
Owner:NAT UNIV OF DEFENSE TECH

Claw-type launcher for water rocket launch and launch method of claw-type launcher

PendingCN111964528AShort release strokeGood release synchronizationRocket launchersRocket launchEngineering
The invention relates to a claw-type launcher for water rocket launching. The claw-type launcher is provided with an integrally formed launcher body and two claws, clamping buckle parts are arranged at the upper ends of the claws; limiting horizontal bars facing the corresponding clamping buckle portions are respectively formed at the ends of the same sides of the two clamping buckle parts; the launcher further includes a limiting mechanism that can limit and release the two limiting horizontal bars; when the limiting mechanism limits the limiting horizontal bars, the claws and the clamping buckle parts cannot move; and when the limiting mechanism releases the limiting horizontal bars, the l limiting horizontal bars, the claws and the clamping buckle parts can be opened. By adopting the structure, the limiting horizontal bars extending on the claws are used to lock and release in a limiting mode, the release stroke of the limiting mechanism is shorter and the release synchronization isbetter, and launching is facilitated; the structure of the limiting mechanism is diversified, a variety of launch methods can be achieved, such as multiple water rocket relay launches, mortar launches, and the like, different launch effects are brought, and the needs of more users can be met.
Owner:梁伟基 +1

Large-volume split-type water rocket parachute umbrella bin and water rocket

PendingCN110379283AThere will be no situation where it cannot be openedOpen smoothlyToy aircraftsEducational modelsInterior spaceEngineering
The present invention relates to a large-volume split-type water rocket parachute umbrella bin. The umbrella bin has a bullet-shaped bin body, and the bin body is formed by connecting and combining afirst and second shells that can be opened and closed; a connecting portion connected with the top of the water rocket body is formed at the center of the bottom surface of the bin body; a surroundingrubber band is connected with the bottom of the side wall of the first shell; a mounting recess hollow toward the inner portion of the second shell is formed at the middle of the second shell; and arubber band connection and release device is arranged in the mounting recess, and the rubber band connection and release device can be connected with the movable end of the surrounding rubber band andcan release the movable end of the surrounding rubber band in due course. According to the large-volume split-type water rocket parachute umbrella bin provided by the present invention, by using thestructure, the opening manner of the bin body becomes a side opening or split type, the opening area after opening is maximized, the internal space of the bin body is completely exposed, the load in the bin body including the parachute can be opened smoothly, and the situation that the parachute cannot be opened cannot occur.
Owner:梁伟基

Parallel type water rocket launcher

InactiveCN102867455AIncrease thrustSuccessful launchEducational modelsRocketWater rocket
The invention relates to the field of model rockets, in particular to a parallel type water rocket launcher. The launcher solves the problems of the existing model rockets that the environment is polluted, and a parent of a plurality of parallelly-connected subrockets does not have a matched launching device. A lateral wall of an inflation pipeline is respectively communicated with a pressure adjusting valve, a pressure meter, a gas needle and two first ball valves. One end of the inflation pipeline is communicated with a plurality of gas inlet pipes of the water rocket launcher, a water injection device is respectively communicated with a first connecting pipe, the first connecting pipe is respectively communicated with a plurality of second connecting pipes, each second connecting pipe is communicated with a plurality of gas inlet pipe lateral walls of the launcher, each second connecting pipe is provided with a second ball valve, the water rocket launcher is fixed on a launching platform, a launching plate is arranged on the launching platform parallelly, the launching plate is provided with a plurality of launching sleeves of the water rocket launcher, a lead screw is fixedly connected onto the launching plate, and the lead screw is in transmission connection with a guiding rod of an air cylinder. The parallel type water rocket launcher is applicable to the model rockets.
Owner:施胜南

High-position automatic water spraying noise reduction system following rocket exhaust plume

ActiveCN113606990ASprinkler start time earlyProlong the action timeRocket launchersRocket launchControl system
The invention discloses a high-position automatic water spraying noise reduction system following rocket exhaust flame, and belongs to the technical field of rocket launching noise protection. The system comprises nozzles, a quick valve control system, an air supply system, a water supply system and a drainage system; the nozzles are connected to the water supply system through water spraying pipelines, and evenly arranged on the front side and the rear side of a launching station; and the water spraying range can cover a launching pad after stable water spraying of the nozzles. The rapid valve control system is arranged on a water supply pipeline, and short-range water spraying of the system is achieved before ignition of a rocket engine; long-range water spraying of the system is achieved at a certain moment after a rocket is ignited to take off, and the time interval between the working conditions of short-range water spraying and long-range water spraying is about 1 s; the air supply system is used for providing compressed air for the quick valve control system as a control air source; and large-flow sprayed water is timely collected and discharged to a low-lying position outside a launching site through the drainage system. According to the system, the working conditions of water spraying are switched according to the rocket launching conditions, the safety of a rocket body can be guaranteed, and meanwhile noise radiation and propagation are restrained.
Owner:NO 63921 UNIT OF PLA +1

Pressure-operated glider connecting-separating device of water rocket boosting glider

The invention provides a pressure-operated glider connecting-separating device of a water rocket boosting glider. The pressure-operated glider connecting-separating device comprises a connecting base, a connecting sliding block and a piston-spring mechanism. The connecting base is provided with a connecting sliding groove matched with the connecting sliding block in the vertical direction. The piston-spring mechanism comprises a soft gas circuit connector, a cylinder-piston assembly, a tension spring, a tension spring fixed hanging rod, a tension spring movable hanging rod, a tension spring movable hanging rod limiter and a carbon fiber bolt; the soft gas path joint is connected to the soft gas path; the cylinder-piston assembly is composed of a cylinder barrel and a piston, the tension spring fixed hanging rod is fixedly arranged on the upper portion of the outer wall of the cylinder barrel, and the tension spring movable hanging rod is connected to the working tail end of the piston; the tension spring is hung between the tension spring fixed hanging rod and the tension spring movable hanging rod; the tension spring movable hanging rod limiter is arranged at the lower part of the cylinder barrel; and the upper end of the carbon fiber bolt is fixed on the tension spring movable hanging rod. The device provided by the invention can work independently; the reliability and the action triggering precision are high; and the design requirements of moisture resistance and water pressure impact resistance are met.
Owner:NAT UNIV OF DEFENSE TECH
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