9results about "Floats" patented technology

The application discloses a low-altitude unmanned aerial vehicle with a protection function, and relates to the field of unmanned aerial vehicles.The unmanned aerial vehicle comprises a main body, paddle blades connected to the ends of four supporting arms of the main body, a chassis fixedly connected to the bottom of the main body, a shell fixedly connected to the bottom of the main body and inside the chassis, a camera main body fixedly connected to the inside of the shell, four bidirectional elastic connection structures eccentrically arranged between the shell and the inner side of the chassis, horizontal rotating blocks and vertical rotating blocks, horizontal link blocks elastically connected to the inner side of the chassis, and vertical link blocks elastically connected to the outer surface of the shell.The bidirectional elastic connection structures can make the related components adaptively rotate along the impact direction, efficiently convert the concentrated impact force from different directions into the rotary motion of the mechanism around the rotating supporting point, and realize the direction guidance and dispersion of the impact force.

This utility model discloses a surface water sampling device based on a drone, relating to the field of surface water sampling technology. It includes two portal frames, with a crossbeam between the lower ends of the two portal frames. A connecting seat is provided between the lower ends of the two portal frames and the crossbeam, and the portal frames are fixedly connected to the crossbeam via the connecting seat. Protective sleeves are provided at both ends of the crossbeam and on the outside of the portal frames. Floating blocks are provided on the two portal frames and above the connecting seat. Mounting plates are provided between the upper sides of the two portal frames, with both ends of the mounting plates engaging with the portal frames. A mounting groove is provided in the middle of the two mounting plates. The drone floats on the water surface via the floating blocks, avoiding the instability of the drone hovering on the water surface, resulting in higher accuracy of water stratification sampling and reducing the risk of the drone falling into the water.

This invention relates to the field of unmanned aerial vehicle (UAV) technology, and more particularly to a UAV for inspecting enclosed space facilities. The technical problem of this invention is to provide a UAV capable of protecting itself during the inspection of enclosed space facilities. The technical solution is as follows: A UAV for inspecting enclosed space facilities includes a UAV body, a support frame, a protective frame, a camera, an emergency stop switch, an air pump, etc.; the support frame is located at the bottom of the UAV body, and protective frames are symmetrically located on both sides of the UAV body, front and back, to protect the UAV's fan blades and prevent them from colliding with the inner wall of the pipe. A camera is located at the top of the UAV body, and an emergency stop switch is located on the upper right side of the support frame. This invention uses an air pump to inflate an airbag, allowing the airbag to expand and enabling the UAV body to float on the water surface when it falls into the water.

This invention relates to a low-altitude spacecraft capable of both amphibious takeoff and landing, belonging to the field of low-altitude aircraft technology. The invention increases the contact area between the hull and water by combining a flat hull bottom with a horizontal hull section, effectively improving the stability of the spacecraft during water navigation. Simultaneously, an arc-shaped hull lifting section is incorporated. During takeoff and as the spacecraft ascends, water flow is diverted along the arc structure, creating a dynamic water pressure difference above and below the hull, generating an upward lifting force to counteract water drag. Combined with the ground effect, this enhances the lift coefficient, helping the hull quickly rise above the water and complete takeoff. Furthermore, the invention employs a multi-layered, multi-wing layout structure, which, during operation, can generate a high lift coefficient through a power superposition effect, producing an excellent thrust-to-weight ratio and ensuring stable flight of the spacecraft.

This invention discloses a drone for river network inspection, relating to the field of river channel drone inspection technology. The floating device further includes a folding airbag, an inflation device, an air inlet, and a cylinder. The folding airbag is fixedly connected to the bottom of the shell, and the inflation device is fixedly connected to the top of the folding airbag. The inflation device is electrically connected to the spiral blade. The air inlet is located on the outer circumference of the inflation device. The cylinder is fixedly connected to the inner wall of the hollow shell. A gravity sensor is installed inside the hollow shell, and the gravity sensor is electrically connected to the cylinder. When the inflation device is activated, it inflates the folding airbag at the bottom, generating buoyancy after the device falls into the water, preventing the device from sinking to the bottom and being difficult to recover. During normal flight, the folding airbag is in a retracted state, avoiding excessive flight resistance due to the excessive size of the buoyancy device.

The utility model discloses a water sample collection device based on unmanned plane, including unmanned plane body, the unmanned plane body is equipped with the perception camera, buoyancy mechanism, sample bottle, negative pressure mechanism and sampling tube, the perception camera is configured as real -time collection environmental information, buoyancy mechanism is configured as the required buoyancy that water sample collection device floats on the water surface provides, sample bottle is configured as the water sample of containing collection, negative pressure mechanism is connected with sample bottle, is configured as make the negative pressure in sample bottle, to utilize the negative pressure of generating and suck the water sample to sample bottle in, sampling tube has the water outlet end and the water suction end, and the water outlet end is connected sample bottle, and the water suction end is equipped with filter piece, wherein, all components of water sample collection device except sample bottle have a barycenter, and the vertical straight line of barycenter coincides or approximately coincides with the axis of sample bottle. The utility model has realized water sample collection.

A firefighting float plane (10) having a fuselage (112), one or more wings (110), two floats (114, 116), a water scoop (120, 122) associated with each float for filling a water tank (300) of the firefighting float plane, and systems and / or methods for deploying the water scoops to prevent (and / or mitigate the effects of) asymmetric deployment and / or retraction of the water scoops.

The invention relates to a buoyancy system, intended to be connected to a structure of an aircraft comprising roll stabilization means comprising at least one floating mat, intended to be deployed on a water surface to reduce a rolling motion of the aircraft.