35 results about "Launch craft" patented technology

A method of identifying a vessel as well as a vessel identifying device and a floating object and land installation including such a vessel identifying device. The vessel identifying device includes a processor operative to obtain a position of a vessel being sensed by a sensor, assign an identity to the vessel, which identity is assigned according to an identity assignment scheme of at least a part of a maritime tracking system, which maritime tracking system is an Automated Identification System (AIS), and provide an identification of the vessel according to the maritime tracking system, the identification including the assigned identity and the position of the vessel, and order a transmitter to transmit the identification of the vessel.

The present invention relates to an ion source (1), in particular an ion propellant for propelling a spacecraft, comprising a reservoir (2) for a propellant (3) having a solid state and being liquefiable to a liquid state, a heater (4) for liquefying the propellant (3) in the reservoir (2), an emitter (5) in fluid communication with the reservoir (2) for receiving a stream (S) of liquefied propellant (3) from the reservoir (2), an extractor (7) in front of the emitter (5) for extracting ions (3') from the liquefied propellant (3) of the emitter (5) and accelerating the extracted ions (3') away from the emitter (5), wherein at least one deflector (11) is disposed upstream of the emitter (3) in the stream (S) of the propellant (3) towards the emitter (5).

An unmanned aerial vehicle (UAV) launch tube (100) that comprises at least one inner layer of prepreg substrate (370) disposed about a right parallelepiped aperture (305), at least one outer layer of prepreg substrate (380) disposed about the right parallelepiped aperture (305), and one or more structural panels (341-344) disposed between the at least one inner layer of prepreg substrate (340) and the at least one outer layer of prepreg substrate (380). An unmanned aerial vehicle (UAV) launch tube (100) that comprises a tethered sabot (700,740) configured to engage a UAV within a launcher volume defined by an inner wall, the tethered sabot (700,740) dimensioned to provide a pressure seal at the inner wall and tethered to the inner wall, and wherein the tethered sabot (700,740) is hollow having an open end oriented toward a high pressure volume and a tether (740) attached within a hollow (910) of the sabot (700) and attached to the inner wall retaining the high pressure volume or attach to the inner base wall (1013). A system comprising a communication node (1500-1505) and a launcher (1520) comprising an unmanned aerial vehicle (UAV) in a pre-launch state configured to receive and respond to command inputs from the communication node (1500-1505).

The utility model discloses an automatic ball launching machine, include: shell, its top inner wall extends downward and has the launching barrel, the upper end of launching barrel is worn and is formed launching port to shell top, elastic launcher is set up in the launching barrel, and the upper end of elastic launcher and the circumferential side of launching barrel form the receiving space of containing the ball, and the transmission part of elastic launcher is equipped with and extends the launching barrel, drive mechanism is set up in the shell, and it includes drive motor and the swing arm of drive motor output end junction, wherein, swing arm is suitable in the drive of drive motor and rotates downward and pushes and presses transmission part to make elastic launcher drop to first state, when swing arm turns away from transmission part, elastic launcher rises and resets to second state to the ball and is shot out launching port. The utility model adopts above -mentioned structure, and the ball launching machine simple structure is small, and the weight is light.

This utility model relates to the technical field of automatic water supply devices. It provides an automatic water supply device for a ship unloader's water tank, used to add water to the tank. The device includes an on-machine docking mechanism mounted on the ship unloader and a lower-machine docking mechanism mounted on the ground and connected to a water source. The on-machine docking mechanism includes an on-machine adjusting component and a docking female head, which is located on the movable end of the adjusting component. The lower-machine docking mechanism has a docking male head. The on-machine adjusting component has a positioning signal transmitter, and the lower-machine docking mechanism has a positioning signal receiver. Through the cooperation of the positioning signal transmitter and receiver, the docking female head and the docking male head can be positioned. After positioning, the on-machine adjusting component automatically pushes the docking female head to move and dock with the docking male head, eliminating the need for manual operation and reducing the labor intensity of workers. The entire docking process is automated, improving the safety and reliability of the ship unloader's water replenishment operation.

A launcher for a zipline trolley system comprises a body, first and second arms, first and second connectors, first and second pads, and an actuating portion. The first and second arms extend from the body. The first and second connectors are pivotably connected to the first and second arms, respectively. The first and second pads are connected to the first and second connectors, respectively. The actuating portion comprises a sliding member and first and second pull arms. The first and second pull arms are connected to the first and second connectors, respectively. When the launcher is in a first configuration, the first and second pads are adapted to hold the trolley in place. Movement of the sliding member away from the body causes pivotable movement of the first and second connectors and a transition of the launcher to a second configuration to release the trolley.

This invention relates to the field of launching device technology, and provides a spring-driven launching device for firefighting, military and police use. The device includes a control unit, a drive unit, a housing, and one or more launching units. Each launching unit includes a launching tube, a pressure spring, and a launching element. The pressure spring is built into the launching tube for energy storage, storing potential energy and providing driving force through compression or torsion. The launching element is installed inside the launching tube and is launched when the spring releases its potential energy. The drive unit is driven by a motor or mechanically. This invention employs a multi-tube modular design combining spring power and mechanical drive, abandoning the traditional gunpowder-activated, high-pressure gas cylinder-driven mode. It effectively solves the problems of single-tube launchers—limited functionality, low efficiency, and poor adaptability—and avoids the defects of traditional multi-tube devices—complex structure, low safety, and fixed launching modes. The overall structure is compact, reliable in operation, and safe to use, making it practically valuable in fire emergency rescue, police non-lethal response, and various high-risk space disposal scenarios.

A toy vehicle launcher assembly for launching toy vehicles includes a housing and a launcher at least partially disposed within the housing. The launcher includes a loading mechanism, an actuator mechanism, and a pushing mechanism. The loading mechanism includes a first arm having a handle portion and a second arm having an engagement extension. The handle portion is configured to pivot along a first axis to move the engagement extension, and the first arm is longer than the second arm. The actuator mechanism includes a latch. The pushing mechanism includes a launching member having a first end for engaging with the latch and a second end opposite the first end for engaging the toy vehicle. Rotating the handle portion of the loading mechanism toward the pushing mechanism causes the engagement extension to laterally pull the launching member toward the actuator mechanism.

A shooting target launcher, associated components and methods. The launcher spins one or more helicopter-like shooting targets to launch the targets. A target connector receives the targets. The target connector is rotated about an axis of rotation to rotate the targets about the axis of rotation. The targets have fan blades that, when rotated, propel the target through the air.

A launch system includes a launcher and a launch vehicle. The launch vehicle upper portion has a diameter greater than the lower portion, which includes a propulsion system. The launcher includes: a launch tube, a piston assembly, and an actuation system. The piston assembly is selectively movable along a piston axis, co-axial with the central axis of the launch tube, between two axial positions to thereby eject the launch vehicle from the launch tube. The piston assembly includes a piston member, and a launch load application member projecting upwardly from the piston member. The launch load application member provides load-bearing contact to the launch vehicle, and is laterally off-set from the central axis. The actuation system is coupled to the piston assembly and selectively accelerates the piston assembly between the two axial positions, thereby imparting a launch force to the launch vehicle via the launch load application member during launch.

The utility model relates to the buckle type quick release type launcher bottom cover in the field of launcher bottom cover, including launcher cylinder and bottom cover main part, bottom cover main part inserts in the top of launcher cylinder, and the left and right sides of bottom cover main part's bottom all are equipped with locking mechanism, and locking mechanism includes first locking wedge, second locking wedge and push -back, first locking wedge is assembled in the bottom of bottom cover main part, second locking wedge is assembled in the inner chamber of launcher cylinder, and push -back inserts in the outside of launcher cylinder, and the return spring is connected between push -back and launcher cylinder, and the outside of push -back is connected with the pressing plate, and the inner chamber of launcher cylinder is provided with the heat dissipation groove. The buckle type quick release type launcher bottom cover, prolongs the service life of locking mechanism and whole launcher bottom cover, guarantees the stability and reliability of launcher bottom cover, maintains good heat dissipation performance, and clean dust can be discharged through the inclined plane of heat dissipation groove, further guarantees the normal use of launcher bottom cover.

The application discloses an unmanned ship for offshore illegal ship monitoring and driving away, which comprises a fish-fin-like monitoring device on the top of the ship body, a tail smoke outlet, a main suction cup on the bottom of the ship body, a suction cup mechanical arm and a flexible net launching device; the front end face of the fish-fin-like monitoring device is provided with an infrared camera and a light emitter, and the rear end face is provided with a rearview camera; the tail smoke outlet can discharge colored smoke into the air; the suction cup mechanical arm comprises a mechanical arm and a suction cup impact device, the suction cup impact device can be adsorbed on the target ship body and drive the impact pin to impact the target ship body; and the flexible net launching device is used for launching the flexible net to the propeller of the target ship. Through the integration of the fish-fin-like monitoring device, the multi-dimensional interference system, the mechanical adsorption structure and the flexible net launching device, the application realizes the whole-process monitoring, step-by-step interference and forced stopping of the offshore illegal ship, and the unmanned ship has the characteristics of high mobility, strong adaptability and multi-functional integration, and can efficiently work under complex sea conditions.

A dart launcher and dart magazine for alleviating improper dart placement concerns with a forward matching dart profile. The dart magazine is short and does not extend into the launch chamber of the launcher. The magazine has an open top with a dart restrainer that is moved when the magazine is inserted into the launcher causing an upper-most dart in the magazine to be biased out of the magazine and into the launch chamber. The launcher includes a dart placement structure in the launch chamber to locate the upper-most dart. The dart placement structure may be shaped as an arm allowing positioning of each dart also free of the magazine while facilitating automatic firing of the darts from the magazine.

This invention discloses a modular impact interception device for use on unmanned aerial vehicles (UAVs), comprising a launcher ram, a loading mechanism, a rebound launch mechanism, a streamlined outer shell, and a launcher mounting chassis, employing a modular design. The launcher ram has a wedge-shaped armor-piercing section at its front end and a magnetic suction device and auxiliary holes at its bottom, allowing for quick replacement in conjunction with the loading mechanism. The rebound launch mechanism achieves precise linkage between locking, triggering, and high-speed launch through the coordinated action of a longitudinal high-strength launch spring and a transverse tenon-and-mortise latching traction spring. Upon impact with the target, it drives the launcher ram to rebound and penetrate the core component. The device features a streamlined shape and a sealed design to reduce wind resistance, supports both pure physical impact and composite strike modes filled with thermite and expanded graphite powder, and is adaptable to multi-rotor and fixed-wing UAVs for installation in various orientations. This invention eliminates the need for explosives or self-destructive impacts, significantly reducing the cost of a single countermeasure, greatly improving interception accuracy and safety, and is reusable.

The utility model relates to rescue equipment technical field especially rescue electromagnet throws and throws the bullet, including the bullet body with the accommodation cavity, the rear part screw thread connection of bullet body has the tail cone with the taper contraction section, the outside of tail cone is provided with a plurality of tail vane, the rear end surface of tail vane and the rear end surface of tail cone between reserve the distance for avoiding electromagnetic transmitter coil end plate, still include: rescue assembly, set up in the front of bullet body, the taper contraction section is configured as when throwing and throwing the bullet flight and push rescue assembly acceleration, buffer assembly, set up in the inside of the accommodation cavity of bullet body, be configured as absorbing the launch impact, through this technical scheme, can through rescue assembly in the flight acceleration, while buffer assembly can effectively absorb the launch impact, protect inside rescue assembly, improve the rescue success rate.

A multi-launcher space launch assembly includes a movable platform for the assembly, transporting, and vertical positioning of varied launchers. The platform cooperates with a fixed table and a jet deflector, which are situated in a launch area. The infrastructure also includes adaptable fluid refuelling modules compatible with various flow and pressure profiles. The system is adapted to accommodate variations in the height and diameter of launchers by way of modular components.

This utility model relates to an angle-adjustable hail testing device, comprising a base frame, a mounting frame, and an adjustment frame. The adjustment frame slides back and forth on the upper end of the base frame and slides left and right on the front end of the ice hockey launching device, allowing the launching position of the ice hockey to be freely adjusted in the horizontal plane. Photovoltaic modules are mounted on the mounting frame. The guide plate on the inner side of the base frame and its semi-circular guide hole cooperate with the fastener at the lower end of the mounting frame. Moving the fastener along the guide hole drives the mounting frame to rotate back and forth around the rotation connection point, flexibly adjusting the tilt angle of the photovoltaic modules. By tightening the fastener passing through the guide hole, the mounting frame is stably locked at any desired tilt angle, effectively solving the problem of ice hockey only impacting vertically. It simultaneously controls the tilt angle of the mounting frame with photovoltaic modules and the horizontal position of the launcher, accurately simulating the real working condition of hail impacting photovoltaic modules at different tilt angles, thus improving the accuracy of photovoltaic module reliability testing.

The application discloses a kind of unmanned aerial vehicle multi-direction launch net trapping device and method, square main control bin is fixedly arranged in frame side direction;Cone is arranged above frame, cone is connected with unmanned aerial vehicle fuselage by high-strength alloy material, cone base connects rotating shaft;Cone is peripherally arranged multiple net trapping launch units;Miniature laser range finder, infrared distance measuring module are installed in frame side edge, after target is determined and locked by algorithm of central control module, drive cone and rotating shaft bidirectional brake, realize horizontal rotation adjustment, the transmitter of net trapping launch unit is pneumatically launched net, and multi-direction multi-target synchronous net trapping is realized.The application can realize multi-direction target synchronous capture, improve the capture success rate of different moving speed target;Increase self-stabilizing buffer device, guarantee fuselage stability;Through the cooperative work of sensor and range finder, combined with net body traction body design, the precise regulation and control of capture net parameter is realized, and the capture demand of different scenes is adapted.

The present application relates to a kind of electromagnetic emission systems, belong to fire-fighting technical field, solve the problem that it is difficult to realize long-distance fire extinguishing in prior art, the flight distance of fire extinguishing bomb is difficult to control when launching fire extinguishing bomb.The present application includes: launch turret, electromagnetic launcher, detection device;The launch turret includes: pitch transmission mechanism, azimuth transmission mechanism and cradle;The pitch transmission mechanism is used to adjust the pitch angle of cradle;The azimuth transmission mechanism is used to adjust the circumferential direction of cradle;The electromagnetic launcher and detection device are all installed on the cradle;The detection device is used to detect target position;The electromagnetic launcher includes: drive coil and launch armature;The drive coil can drive the launch armature displacement by electromagnetic induction;The launch armature and load are arranged side by side, for launching load.The present application realizes the adjustment of launch direction and distance, realizes long-distance launch.

Charging system for a remotely controlled bait boat (2) with rechargeable energy storage, comprising a stationary charging device (1) with at least one inductive transmitter unit (3), a bait boat (2) with at least one corresponding inductive transmission unit, characterized in that the stationary charging device (1) is designed for positioning the bait boat (2) in a charging position, wherein, when positioning the bait boat (2) in the charging position, a contactless energy transfer takes place between the inductive transmitter unit (3) and the corresponding inductive transmission unit.

A digit-mounted, spring-assisted device for launching a projectile in response to a launching motion of a finger by a user. The digit-mounted device may comprise a securing means for securing a launcher to the digit of the user. The securing means may comprise a strap, loop, or cinch. The digit-mounted device may further comprise a launch guide extending outwardly from a base member. A projectile may be mounted onto or into the launch guide. A spring may be mounted on the digit-mounted device which is placed under tension when the user prepares to make a launching motion with the digit. The projectile is launched in response to the user making a launching motion with the digit, using the thumb as a tensioning means. The spring is released from tension upon making a launching motion with the digit, adding to the force given to the projectile upon launch. The projectile may take a wide variety of forms.

The utility model discloses a fiber optic probe transmitter, including the launch gun, be equipped with the restriction component on the launch gun, be equipped with auxiliary assembly on the launch gun, through the restriction component that sets up in the launch gun, can be in the time of putting the cylinder through the restriction bullet one self -adaptation telescopic adjustment, make the restriction post stably limit the cylinder of putting, cooperate with the restriction buckle and the restriction bolt, realize the quick and reliable fixing of the cylinder of putting, has simplified the process of putting, has improved the measuring efficiency, and the auxiliary assembly that sets up in the launch gun can be adjusted according to the condition of the buffer board, effectively reduces the injury that the circuit board is caused in the process of putting or using and shakes, collides.

The utility model discloses a balloon launcher, including the casing of gun shape and fan, and the casing is spliced by left and right two parts, and the front end of casing inserts the launch pipe of axial telescopic, and the tail portion of launch pipe is equipped with the necking of smaller diameter, and the top of casing is equipped with the cartridge groove, and cartridge groove is from the upper side opening to the rotatable cartridge module of clamping in it, and cartridge module includes the rotary drum, and the edge of rotary drum is equipped with a plurality of axial through -hole a along circumference, and axial through -hole a evenly distributes along circumference to form the cartridge, and cartridge inserts the balloon core of tubular, and balloon core is used for the sleeve joint of slender tubular balloon, and cartridge groove bottom is equipped with the through -hole b of transverse penetration, and the output of necking, fan is respectively located at the front and back two ends of through -hole b, and cartridge module index rotation switches different cartridge and through -hole b alignment. Adopt fan inflation, and can manual continuous ramming launch after loading once, and the interesting of this balloon launching device is good, and except as toy, still can be used in the entertainment place place and is made atmosphere.

1. Name of the product in this design: Vessel Dynamic Flexible Denial Launcher. 2. Purpose of this design: To launch a propeller-driven entanglement net, using propeller entanglement technology to achieve the denial and interception of ships. 3. The key design feature of this product is its shape. 4. The image or photograph that best illustrates the design's key points: a 3D model.

1. The name of the design product: unmanned aerial vehicle honeycomb launcher. 2. The use of the design product: for launching unmanned aerial vehicle in cylinder. 3. The design points of the design product: in shape. 4. The picture or photo that best shows the design points: perspective view.

The application discloses a recess type negative oxygen ion machine and a use method. A bearing plate is used for supporting and containing objects. A launching plate is rotationally connected to the end of the bearing plate and is used for rotating into a vertical state to form a supporting space with the bearing plate or rotating into a horizontal state to be stacked and accommodated with the bearing plate. A negative oxygen ion launcher is installed in the launching plate and is used for releasing negative ions to the supporting space. The application has the beneficial effect that the recess type semi-closed space is formed by surrounding the bearing plate and the launching plate, the negative ions are gathered upward along the inclined surface, a stable high-concentration negative ion layer is formed in the breathing area, diffusion waste is avoided, the absorption distance is shorter, the efficiency is higher, and the utilization rate is greatly improved.