532results about "Compressed gas guns" patented technology

A speedloader is provided, comprising a speedloader body. The speedloader body is provided with a cartridge loading cavity and a soft bullet loading cavity; a second pusher is slidably connected in the cartridge loading cavity, one side end of the speedloader body is connected with a magazine, and a first pusher is slidably connected in the soft bullet loading cavity. The first pusher is driven to push soft bullets into cartridges in the cartridge loading cavity, and the second pusher is driven to push soft bullets loaded into cartridges into the magazine, thereby achieving the purpose of rapid loading of bullets in batches.

Removable ammunition magazines for air guns, combinations of such a magazine with an air gun, and methods of use. The removable ammunition magazine includes a pellet feeder and a canister chamber. A puncture needle is disposed at the top end of the canister chamber, and a canister seat is disposed at a bottom end of the canister chamber. A lever with a cam is pivotably secured to a bottom end of the body, and a cam follower engages the cam and operatively coupled to the canister seat. The lever rotates between an open position, in which the canister seat is shifted away from a puncture needle, and a closed position, in which the canister seat is shifted toward the puncture needle. The lever is recessed within a recess in a bottom surface of the body in each of the first and second positions. The cam may have two detents to help hold the lever in the open and closed positions.

A toy gun and a gas cylinder piercing structure are provided. The gas cylinder piercing structure includes a screw base and a movable push rod unit. The screw base includes a circular through-hole and an annular block around it. A top of the annular block has a slot. The movable push rod unit includes a round push rod movably inserted in the circular through-hole, and a return spring between the screw base and the round push round. A top of the round push rod has a striker pin. The striker pin extends with a needle portion. The striker pin has an engagement lug and a notch. When the engagement lug is blocked by the annular block, the round push rod completely fills the circular through-hole. When the engagement lug is engaged with the slot, the notch and the circular through-hole together form an air vent channel.

A toy rounds blaster apparatus launching multiple projectile rounds with an energy source including a single launch spring for moving one or more pistons within one or more cylinders. A pressure distributor couples each of the one or more cylinders forward the one or more pistons, with an alignment system receiving a collection of the projectile rounds, for aligning individual projectile rounds between pressure distributor and the at least one barrel, with the pressure distributor coupling each of the one or more cylinders with a respective one of the individual projectile rounds. An actuator is linked with the energy source for causing the single launch spring of the energy source to move the one or more pistons and launch the projectile rounds.

A device for pneumatic launching of a drone includes a launch tube, a pressurization chamber situated at the rear of the tube and provided with a passage opening leading into the tube, and a device for temporarily closing the passage opening. The temporary closing device is arranged to change from a closed configuration to an open configuration instantaneously under the action of the gas pressure inside said chamber, after the latter has reached a trigger pressure, and the cross section of the passage opening is sufficiently large that, instantaneously with the change to the open configuration, the gas pressure prevailing in the chamber and the space located behind the drone, then in communication with each other, is the desired launching pressure for the drone.

A toy projectile launcher includes a housing, a launch canister, an air piston assembly, a trigger, a trigger lever having a distal end portion connected to the launch canister, a storage cylinder rotatably mounted within the housing and including a plurality of projectile seats, and a spring biasing the launch canister away from the storage cylinder, wherein each projectile seat is configured to receive a projectile. When the trigger is actuated, the trigger lever pulls the launch canister into engagement with one of the projectile seats of the storage cylinder to form a hermetic seal between the rear portion of the launch canister and one of the projectile seats.

The invention relates to a pneumatic cable throwing device applied to an underwater vehicle and a cable throwing method. The cable throwing device comprises a buoy, a gas cylinder, a shell, a cable, a release cavity, a base and a compressed air storage cavity. A buoy, a gas cylinder and a base are sequentially installed in an inner cavity of the shell from top to bottom, the bottom of the buoy and the top of the gas cylinder form a closed release cavity, a compressed air storage cavity is formed in the gas cylinder, the cable is arranged between the inner surface of the shell and the outer surface of the gas cylinder, one end of the cable is fixedly connected with the buoy, and the other end of the cable is fixedly connected with the base. Compressed air is stored in the compressed air storage cavity before the device works, the compressed air enters the release cavity and generates thrust on the buoy during working, the buoy drives the mooring rope to be ejected and thrown out, and the buoy floats on the water surface at a long distance. The cable throwing device has the advantages of being high in integration degree, stable in function, long in cable throwing distance, high in safety, wide in application range and the like, and the recycling requirement of the underwater vehicle under the complex sea condition can be well met.

High pressure compressor system for compressed air or gas rifles or pistols comprising a motor (1) that rotates a shaft (2) connected to at least one crankshaft (32) having at least two crankpins (7,8), a first crankpin (7) and a second crankpin (8), each of which is respectively attached to connecting rods (3, 4), which connecting rods (3, 4) are outphased with respect to one another: a first connecting rod (3) a second connecting rod (4), a second piston (12), and a second sleeve (13) surrounding the first piston (11), and at least partially surrounding the second piston (12) and both crankpins (7, 8), said second sleeve (13) being connected to the first sleeve (28) and including through holes (5, 6) for the fluid to pass into the second sleeve (13), and at least one guide tube (14, 19) that surrounds the second sleeve (13) and, at least partially, the second piston (12), and a second valve (16) that defines a fluid inlet into the second sleeve (13).

The invention relates to the technical field of air cannon launching, in particular to an air cannon launching device which comprises an air chamber, a piston, a launching tube, a diaphragm assembly, an air supply assembly and a pressure adjusting assembly. The pressure adjusting assembly drives the piston to move, so that the size of the gas storage cavity is reduced, and then the pressure intensity in the gas storage cavity is increased. And when the pressure intensity in the gas storage cavity exceeds the bearable limit of the diaphragm assembly, the diaphragm assembly is broken down. The transmitting tube is instantaneously communicated with the gas storage cavity, and the high-pressure gas can be instantaneously released. And the high-pressure gas flowing into the launching tube pushes the projectile to be ejected at an extremely high ejection speed. Compared with a traditional piston type air cannon launching device, the piston type air cannon launching device is simplified in structure and lower in failure rate. And compared with a traditional double-membrane-breaking type air cannon launching device, high-pressure gas release is extremely efficient, and membrane loss is reduced. Compared with a traditional electromagnetic valve type air cannon launching device, the electromagnetic valve type air cannon launching device is not limited by the response rate of an electromagnetic valve any more.

Automatically-reloading air guns and methods associated therewith. The automatically-reloading air gun includes a barrel fixedly carried by a frame, and a vent aperture in fluid communication with a firing chamber. Actuation of a release mechanism from an engaged position to a disengaged position allows a charge of compressed gas to slide a firing piston forward to force a projectile in the firing chamber into the breach end of the barrel. The compressed gas can exhaust out of the vent aperture from the firing chamber when the firing piston is in the extended position. The return spring slides the firing piston rearwardly to the retracted position after the compressed gas has exhausted from the firing chamber to automatically reload a new projectile into the firing chamber.

Launcher apparatus and methods of a toy projectile blaster piston air compression element and breech bolt having a connected cylinder driving arm, and a piston driving arm at the piston. A cylinder cam pathway track and a piston cam pathway track at a firing mechanism positions a piston cam follower linkage tracking end at the piston cam pathway track, and a cylinder cam follower linkage tracking end at the cylinder cam pathway track pivoted at a conveyor of an integral a trigger assembly. A cylinder follower projection is brought into contact with the cylinder driving arm and a piston cam follower projection is brought into contact with the piston driving arm, for fluid communication to outwardly launch the received projectile rounds.

Break barrel airguns are provided with a loading system that uses the cocking action of the break barrel type airgun to charge an energy storing device. A rotary style magazine is provided that enables multi-shot capability for the airgun. The magazin is held by a magazine holder and engages with engagement components that reduce backlash, prevent backwards rotation of the magazine, and ensure alignment of the projectile holders in the magazine with the opening of the barrel.

A gas canister replacement structure of a toy gun has a main structure including a push carrier, a carrier opening, a pressurized gas canister, a gas canister carrier, a carrier magnetic attraction portion, a magnetic element, and an elastic element. Based on such a structure, the gas canister carrier is fixed to the elastic element and the magnetic element only by means of the carrier magnetic attraction portion, so that it only needs to pull the push carrier through the barrel portion to expose the carrier opening in order to allow the gas canister carrier to be removed with a bare hand for replacement of the pressurized gas canister disposed therein, so as to achieve an effect of easy and efficient replacement of the pressurized gas canister.

A loading device comprises a body having an upper portion and a lower portion, wherein the upper portion includes a plurality of circumferentially arranged sections, separated by a plurality of circumferentially arranged distribution walls; and the lower portion includes a central opening, which is symmetrical about a centerline and has an circumference around which a plurality of circumferentially arranged pellets queue tubes are configured to allow each of the queue tubes to receive pellets, via a top inlet connected to each of the circumferentially arranged sections of the upper portion.

The present disclosure provides an onboard electric pump assembly for an air gun. The onboard electric pump assembly includes: a high-speed DC motor powered by a battery; a controller that is operable by a user through a user interface, where the controller is configured to control the high-speed DC motor, and a mounting structure to mount the high-speed DC motor within the air gun an air gun.

The invention discloses a hypergravity field penetration simulation test device, which comprises an air cannon, a launching bullet, a support mechanism, a penetration test mechanism and an acceleration mechanism, and is characterized in that the launching bullet is arranged in the air cannon, the air cannon is arranged in the support mechanism, the bottom of the support mechanism is connected with the top of the penetration test mechanism, and the acceleration mechanism is arranged in the support mechanism; high-pressure gas is filled into the air cannon to push the launching bomb to realize launching; the acceleration mechanism comprises a centrifugal machine and a hanging basket, and the acceleration mechanism provides a super-gravity field environment for the penetration simulation test through rapid rotation; the launching bomb intrudes into the test device to simulate the penetration process. According to the hypergravity field penetration simulation test device provided by the invention, the hypergravity field is applied to the test model through the centrifugal machine, and the test model and a prototype are similar in power, motion and energy, so that a more real penetration process is simulated, various parameters can be conveniently changed, multiple repeated tests can be carried out, and the test efficiency is improved. The test efficiency and the refinement degree are greatly improved, the cost is remarkably reduced, and damage is reduced.

A toy launcher with a housing and a toy projectile holder thereon. A lever arm extends outside the housing and is connected for pivoting movement relative thereto. A piston and cylinder arrangement is located in the housing, with the piston being resiliently biased toward a first end of the cylinder and being moveable toward a second end thereof to a cocked position by the lever arm being pivoted from a first position to a second position. The cylinder is configured to deliver compressed air to the toy projectile holder. A releasable piston catch holds the piston in the cocked position, and is releasable by the trigger or movement of the lever arm itself such that the piston is driven by the biasing element toward the first end of the cylinder to deliver compressed air to the toy projectile holder for launching. The toy projectile can be a foam dart.

A system for underwater hunting contains a plurality of components which allow for customization of the speargun based on the user's needs and the conditions where a user is hunting. By allowing rapid additions or removals of certain components, the invention allow the user to easily modify the firing characteristics of the speargun, and thus target a wider range of prey across a wider range of environmental conditions than those designs currently available in the prior art.

A speargun having ratchet mounted to or integrated into the stock of the speargun to aids in the stretching of the elastic bands to load the speargun. The ratchet is connected to the elastic bands and allows a user to stretch the elastic bands to load the speargun incrementally instead of all at once. The ability to incrementally load the power using a ratchet not only makes it easier to load the speargun, but also enables the same speargun to be used for a variety of spearfishing applications where different amounts of force are optimal to propel the spear.

A foldable break barrel air gun that is movable from a stowed configuration to a use configuration. The foldable break barrel air gun includes a stock having a butt stock pivotally connected to a forestock in which a firing engine is located. A barrel having a muzzle end and a breech end is provided, with the barrel being pivotally connected to the forestock proximate the breech end. A cocking linkage has a first portion that is pivotally connected to the barrel and a second portion that is connected and / or engaged with the firing engine by a releasable linkage connection. With the releasable linkage connection released, the butt stock is foldable relative to the forestock, and the barrel is foldable relative to the forestock such that the butt stock is arranged in proximity to and preferably attachable to the barrel proximate to the muzzle end in the stowed configuration.

Various projectile launching devices are disclosed herein. In one aspect, the projectile launching device includes a gas-powered projectile agitator, an anti-jam assembly, and a compressed gas canister frame positioned below a body of the device. In another embodiment, the projectile launching device includes a rear-loading hopper and a projectile agitator which is actuated by mechanical power via a linkage with a pump handle.

Break barrel airguns are provided with a loading system that uses the cocking action of the break barrel type airgun to charge an energy storing device. A rotary style magazine is provided that enables multi-shot capability for the airgun. The magazin is held by a magazine holder and engages with engagement components that reduce backlash, prevent backwards rotation of the magazine, and ensure alignment of the projectile holders in the magazine with the opening of the barrel.

A toy projectile launcher having a projectile container, a cocking slide, and a housing is disclosed. The projectile container contains projectile holders that are adapted to hold a projectile, such as a foam dart. The cocking slide can be moved forward and backward. The housing houses a launch barrel and an air piston assembly. When the cocking slide is moved backward the air piston barrel moves backward, and a projectile holder is moved into a firing position. The foam dart is held in place by a resilient stopper. When the cocking slide is moved forward an air nozzle engages a surface of the resilient stopper and advances through the projectile holder, pushing the foam dart into the launch barrel. An airtight seal is formed between the launch barrel and air piston assembly.

An air rifle device for using a cylinder of carbon dioxide as a propellant includes a housing having a front end, a rear end, a top side, and a bottom side defining a chamber extending through the housing. A barrel coupled to the front end is in fluid communication with the chamber. A clip removably couplable to the housing holds a plurality of projectiles. A canister removably mounted to the housing holds a propellant. The canister comprises a neck and a body. A collar configured to receive the neck is mounted to the housing. A cradle configured to receive the body is coupled to the housing. The cradle is aligned with the collar to facilitate coupling the canister to the collar. A trigger mechanism mounted to the housing expels a quantity of the propellant into the barrel sufficient to propel one of the plurality of projectiles outwardly through the barrel.

A flying vehicle is disclosed with a plurality of projectile systems that each contains a projectile for projecting at another flying device. The flying vehicle can include a control system, a flight system in communication with the control system for enabling the flying vehicle to fly, a first projectile system in communication with the control system and a second projectile system in communication with the control system. The control system determines, based on a characteristic of a target flying vehicle, whether to implement a first mode utilizing the first projectile system or a second mode utilizing the second projectile system to capture the target flying vehicle.

A cover for a non-lethal gun magazine is disclosed. The cover includes an external shell that has a top side, a bottom side, a wall that connects the top side and the bottom side, and an inner chamber. The cover includes a first opening located on the top side of the external shell, which is configured to receive a non-lethal gun magazine and the inner chamber is configured to fittingly hold the non-lethal gun magazine. The cover further includes a recessed area within the inner chamber that is configured to receive and hold a compressed gas cartridge. In addition, the cover includes a second opening within the wall that connects the top side and the bottom side, which is contiguous with the recessed area and is configured to enable manual contact with the compressed gas cartridge (when such compressed gas cartridge is held within the recessed area).

A projectile includes a shell defining a cavity and one or more retainers. A bolo is disposed within the cavity and a backplate is engaged with the one or more retainers. The backplate is configured to separate from the shell to release the bolo in response to imbalanced forces resulting from deploying the projectile.

The present disclosure provides an onboard electric pump assembly for an air gun. The onboard electric pump assembly includes: a high-speed DC motor powered by a battery; a controller that is operable by a user through a user interface, where the controller is configured to control the high-speed DC motor, and a mounting structure to mount the high-speed DC motor within the air gun an air gun.

A device for pneumatic launching of a drone includes a launch tube, a pressurization chamber situated at the rear of the tube and provided with a passage opening leading into the tube, and a device for temporarily closing the passage opening. The temporary closing device is arranged to change from a closed configuration to an open configuration instantaneously under the action of the gas pressure inside said chamber, after the latter has reached a trigger pressure, and the cross section of the passage opening is sufficiently large that, instantaneously with the change to the open configuration, the gas pressure prevailing in the chamber and the space located behind the drone, then in communication with each other, is the desired launching pressure for the drone.