161results about "Helicopter landing platform" patented technology

The invention discloses modular mobile parking apron equipment, and relates to the technical field of vehicle-mounted parking aprons, and the modular mobile parking apron equipment is characterized in that the modular mobile parking apron equipment comprises a chassis and a PLC, the chassis is provided with a battery pack, a hydraulic station and a power distribution cabinet, and the PLC, the battery pack, the hydraulic station and the power distribution cabinet are electrically connected; the left side and the right side of the chassis are rotationally connected with a plurality of symmetrically-distributed wingspan plate folding mechanisms, and a plurality of telescopic arms staggered with the wingspan plate folding mechanisms are arranged in the chassis. The device has the independent working capacity, the mode of combining multiple driving oil cylinders, rotating shafts, connecting rods and connecting plates is adopted, the driving oil cylinders are controlled through the PLC, and the driving oil cylinders are driven to be matched with the rotating shafts, the connecting rods and the connecting plates; and the driving oil cylinder only needs to do back-and-forth linear motion to drive the wing unfolding plate of the parking apron to be opened and folded, so that the deployment efficiency of the vehicle-mounted parking apron is greatly improved, and the vehicle-mounted parking apron is more efficient to use.

An unmanned aerial vehicle rack is applicable to an unmanned aerial vehicle including a charging end. The unmanned aerial vehicle rack includes a mounting body, where the mounting body is configured to mount the unmanned aerial vehicle and to be parked on a parking platform; and an electrical connection cable including a first end and a second end, where a first fitting portion of the first end of the electrical connection cable is configured to electrically connect to the charging end, a second end of the electrical connection cable is connected to a second fitting portion at a bottom of the mounting body, and the second fitting portion is configured to electrically connect to a power supply end of the parking platform.

The present application provides an aircraft apron, including: a docking platform for carrying an aircraft; at least two position adjustment mechanisms arranged on the docking platform, the position adjustment mechanism including a movable first rocker arm and a second rocker arm, the first rocker arm and the second rocker arm can cross each other to form a clamping portion for clamping a structural member of the aircraft, and as the first rocker arm and the second rocker arm move, the formation position of the clamping portion changes, thereby driving the aircraft to move from a landing position to a target position. In addition, the present application also provides a vehicle including the above-mentioned aircraft apron. The aircraft apron provided by the present application can use a position adjustment mechanism to drag / push an aircraft that has landed on the docking platform, and move the aircraft from a landing position to a target position, thereby facilitating the operating device of the ground equipment to charge the aircraft, replace the load, replace the battery, or replenish raw materials.

A goods delivery terminal comprises a first module, a second module, a third module, and a fourth module. The third module and the fourth module are capable of transporting goods in a first direction and a second direction respectively, and the second direction intersects the first direction; At least one of the third module and the fourth module is capable of being solely arranged between the first module and the second module, and is capable of independently transporting the goods from the second module to the first module and from the first module to the second module; the third module and the fourth module are also capable of being arranged together between the first module and the second module, and are capable of relay transporting the goods from the second module to the first module and from the first module to the second module.

The utility model discloses an unmanned aerial vehicle platform, an unmanned aerial vehicle hangar and a vehicle, relates to the technical field of vehicles, and aims to solve the problem that an unmanned aerial vehicle cannot recognize the position when the unmanned aerial vehicle is arranged in the unmanned aerial vehicle platform. The unmanned aerial vehicle platform comprises a fixing base, a parking apron assembly and an upper fixing plate, the parking apron assembly comprises a first parking apron and a second parking apron, the first parking apron and the second parking apron are movably arranged on the fixing base in the first direction, and the upper fixing plate is arranged on the side, away from the fixing base, of the parking apron assembly and connected with the fixing base. The upper fixing plate comprises a cleaning assembly, and in the process that the first parking apron and the second parking apron are switched between the first state and the second state, the cleaning assembly is suitable for cleaning the parking apron assembly. Therefore, the first parking apron and the second parking apron are ensured to be clean and tidy, and identification and positioning of the unmanned aerial vehicle are facilitated.

Disclosed are an apparatus and a method for controlling a takeoff / landing pad structure by using a hexapod mechanism. The method for controlling a takeoff / landing pad structure by using a hexapod mechanism comprises the steps of: receiving eVTOL information from an eVTOL if the eVTOL prepares for landing; predicting the impact weight to be applied to the takeoff / landing pad structure if the eVTOL touches down, by using the received eVTOL information; calculating a first spring stiffness and a first damper damping required for the suspension according to the predicted impact weight; and controlling the suspension by setting the spring stiffness and the damper damping of the suspension with the calculated first spring stiffness and first damper damping.

The application discloses an unmanned aerial vehicle hangar, which comprises a bottom plate, a side plate arranged along the circumference of the bottom plate and extending away from the bottom plate, and an exhaust mechanism arranged on the side plate and capable of communicating the parking cabin and the external environment to make the airflow generated in the parking cabin when the unmanned aerial vehicle is parked flow with the external environment.

An embodiment vertiport includes a body portion, a take-off and landing portion disposed in the body portion and spaced apart from the body portion by a predetermined gap, a door portion disposed in the gap between the take-off and landing portion and the body portion and configured to be opened and closed, an elevation portion disposed in the body portion and configured to be raised and lowered with respect to the body portion, and a power generating unit slidably coupled to the elevation portion, wherein the power generating unit is configured to produce electrical energy using a downdraft generated by a take-off and landing operation of an aircraft on the take-off and landing portion.

The application discloses an intelligent unmanned aerial vehicle (UAV) parking apron made of ultra-high performance concrete material and a manufacturing method thereof, and belongs to the technical field of UAV supporting facilities. The application solves the problems of poor material performance, lack of night reflective identification, low intelligence level, limited power supply and poor terrain adaptability of the existing parking apron. The main structure layer of the parking apron is composed of a panel made of ultra-high performance concrete, a yellow circular ring capable of reflecting light at night and a white H-shaped mark. The intelligent control system is composed of a GNSS positioning module, a solar panel, a battery, a microcomputer and an alarm, and can realize precise positioning, solar self-power supply, equipment operation monitoring and abnormal alarm. The height-adjustable support structure is composed of an anti-skid and corrosion-resistant bottom plate and a telescopic adjustable support. The application has stable structure, high wear resistance, night visible identification, high intelligence and high environmental adaptability, and can realize all-weather operation. The manufacturing method is simple and suitable for large-scale production, and can be widely applied to various outdoor UAV operation scenes.

The invention belongs to the technical field of smart city infrastructure, and discloses a bus station smart cabin device integrated with a low-altitude aircraft multifunctional use scenario, which comprises a smart cabin, a low-altitude aircraft support system, a smart logistics system, a smart traffic management system and a power supply system, and is characterized in that the smart cabin comprises a passenger service area and a functional area; a parking platform is arranged in the functional area; the low-altitude aircraft support system comprises a navigation module, an obstacle avoidance module, a communication module and an energy management module; the intelligent logistics system comprises an intelligent sorting module, a distribution module and a data management platform. The intelligent traffic management system comprises a traffic monitoring module and a data analysis module. The system has the beneficial effects that multiple functions are creatively integrated into a whole, and the system adapts to the intelligent construction requirements of infrastructures of different cities; good economic benefits, social benefits and environmental benefits can be generated, and the method has a wide application prospect.

The present invention discloses a helicopter pad landing assist system, comprising a pad surface and a signal mechanism. The pad surface is composed of an inner pad surface and an outer pad surface, and a mark is provided in the middle of the inner pad surface. The signal mechanism is composed of an adjustment component of a convertible signaler or signal light and a movable component that can keep the adjustment component hidden. The helicopter pad landing assist system can protect the signal mechanism and can also provide installation of different signal lights or signalers, which can be used at the same time, making it convenient for component installation and angle adjustment. At the same time, the signal mechanism can be hidden and opened through a drive assembly, which can effectively reduce the structural layout, realize the protection of the signal mechanism, help to extend the service life of each component, reduce the probability of component damage, and help the helicopter to automatically center and land.

A final approach and takeoff (FATO) surface for a VTOL aircraft redirects downwash as outwash and may capture outwash from the VTOL aircraft to generate electricity. The FATO surface system may include a central solid plateau configured to capture downwash from the VTOL aircraft to enhance a ground effect for optimal stabilization during takeoff and landing. A floor grate surrounding the plateau may allow outwash to pass through to a subsurface where the outwash is channeled to exhausts or at least one turbine for generating electricity from the outwash. Redirecting the downwash to outwash reduces undesirable effects such as noise and airspeed associated with the VTOL aircraft. The electricity may be used to recharge the VTOL, electric vehicles parked at a vertiport of the FATO surface system, may be used by a building at the vertiport, or may be delivered to a local power grid.

The utility model discloses a tenon-and-mortise structure all-aluminum parking apron which comprises a stand column, a tenon-and-mortise groove is formed in the top of the stand column, an I-shaped keel is arranged in an inner cavity of the tenon-and-mortise groove, a connecting piece is fixedly connected to the upper end of the stand column, an arc-shaped aluminum alloy plate is fixedly connected to one end of the I-shaped keel, and a plurality of aluminum alloy decks are arranged on the surface of the I-shaped keel. The lower end of the stand column is provided with a flange adjusting seat. According to the all-aluminum parking apron with the mortise and tenon joint structure, the all-aluminum parking apron is safer and firmer through cross connection in a mortise and tenon joint structure mode, water accumulation of the parking apron is effectively prevented, the parking apron can be kept clean and tidy, the service life of the all-aluminum parking apron can be prolonged, the overall dead weight is light, and the bearing capacity is good; and secondly, uniform arrangement is achieved in a multi-position thickened stand column supporting mode, the parking apron is stressed in a dispersed mode, the bearing capacity of the stand columns is improved through reinforcing base plates, and the overall safety coefficient is improved.

A modular flying car includes a ground vehicle (10) and a flight vehicle (20). The ground vehicle (10) includes a chassis (11), a first cabin (12) and a landing platform (13) for landing the flight vehicle (20). The flight vehicle (20) includes a second cabin (21) and a flight driving device (22). The flight vehicle (20) is capable of landing and taking off vertically on the landing platform (13) and connected with the ground vehicle (10) by interlocking. Users can choose to travel by the ground vehicle (10) or the flight vehicle (20), and can transfer between the ground vehicle (10) and the flight vehicle (20), to solve the traffic jam problem and make the realization of the flying car more feasible. A flying car system and a flying car sharing method are also disclosed.

The utility model relates to the field of unmanned aerial vehicle supporting facilities, in particular to an intelligent parking apron for a parking space, which is arranged above the parking space and comprises a plurality of upright posts, a parking plate and a lifting device, the upright posts are vertically arranged on a side line of the parking space, one end, far away from the parking space, of each upright post is connected with the parking plate, and the lifting device is arranged on the parking space. The lifting device is arranged on one side of the parking space and used for allowing people to go up and down the parking plate. The intelligent parking apron is arranged on the parking space and used for taking off and landing of the unmanned aerial vehicle, the problem that an independent parking apron occupies indoor space resources can be solved, the problem that articles are inconvenient to store and take out at a unified station can also be solved, the articles can be directly stored and taken out before and after parking, and the life convenience of people and the space utilization rate can be improved.

The application relates to the technical field of parking aprons, in particular to a high-rise building parking apron structure which comprises a parking apron main body and a suppression assembly. Directional air flow generated by the suppression assembly can counteract the outwash air flow generated when a helicopter takes off or lands, avoids the spread of the outwash air flow to the periphery of the parking apron main body, and eliminates the risk of flying sand, sundries and other foreign matters carried by the outwash air flow. The suppression assembly can also weaken the vertical impact force of the downwash air flow on the surface of the parking apron main body, reduce the scouring and cutting effect of the downwash air flow on the surface layer material of the parking apron main body, delay the wear of the parking apron main body structure, significantly prolong the service life of the parking apron main body structure, and reduce the maintenance cost.

The utility model provides an unmanned aerial vehicle intelligent parking apron, and relates to the unmanned aerial vehicle parking apron technical field, the unmanned aerial vehicle intelligent parking apron comprises a mounting shell and a parking assembly, the parking assembly comprises a parking shell and a GPS module, the mounting shell and the parking assembly are provided with a first balance mechanism and a second balance mechanism, and the first balance mechanism comprises a rack. According to the intelligent parking apron for the unmanned aerial vehicle, the parking shell is rotationally connected with the fixed rod through the mounted bearing A, and the mounted bearing A is connected with the balancing weight A through the T-shaped rod, so that a labor-saving lever is formed by taking the mounted bearing A as a resisting arm, the fixed rod as a fulcrum and the T-shaped rod as a power arm; the force application end of the T-shaped rod, namely the end, fixed to the T-shaped rod, of the balancing weight A, is always downward, the shutdown shell fixed to the upper end of the mounted bearing A is always kept horizontal, and when the device is placed on an inclined site, although a mounting shell is inclined, the shutdown shell is still kept horizontal under the action of a labor-saving lever.

The utility model discloses a parking apron aluminum structure fireproof device which comprises a parking apron, a beam column structure is arranged at the bottom of the parking apron, a water passing seat is fixedly connected to the outer side of the parking apron, a fire extinguishing mechanism is arranged on the water passing seat, a fire hydrant is arranged on one side of the fire extinguishing mechanism, and a connecting mechanism is arranged between the fire hydrant and the fire extinguishing mechanism. The fire extinguishing mechanism comprises a plurality of pairs of protection seats, each protection seat is provided with a protection groove, a rotating seat is arranged in each protection groove, the bottom end of each rotating seat is fixedly connected with a first rotating shaft, and each first rotating shaft is fixedly connected with a worm wheel. According to the fireproof device for the aluminum structure of the parking apron, the fire extinguishing nozzle is rotated out from the interior of the protection seat through the retracting and releasing motor, then the movable seat is driven by the movable motor to move, the movable seat moves to drive the fire extinguishing nozzle to move to be in the working position, fire disasters on the surface of the parking apron and a beam column structure are effectively extinguished, and therefore safety can be effectively improved.

An ecological intelligent building suitable for a low-altitude aircraft and vehicle vertical traffic system comprises a longitudinal building space system, vertical traffic, low-altitude traffic, an air garden, an ecological system and an intelligent management and control system, and a cross-layer, complete and independent family living space is formed in a villa unit vertical stacking mode. A longitudinal building space system of a ground villa is re-carved, a staggered terrace and overhanging design is adopted for the overall building modeling, a vertical double-channel independent public transport system is arranged for vertical traffic and low-altitude traffic, and an intelligent management and control system is provided with an independent indoor intelligent center for each villa unit. Through the vertical overlapping design of the villa units, on the premise of high plot ratio, a longitudinal space experience and neighborhood communication mode of ground courtyard combination is re-engraved, the problem of low living quality generally existing in traditional high-rise residences is solved, and intelligent and ecological building space facing the future is constructed.

Disclosed herein is an evacuation system for apartments in a building comprises: a) a support surface adapted for holding an evacuation air vehicle, said evacuation platform is configured to be installed on the exterior side of a building, outside one or more designated evacuation apertures in a peripheral wall of one or more building units, wherein the evacuation platform is adapted with an alignment mechanism configured to manually, or controllably shift said evacuation platform between a stored position and alignment with said designated evacuation aperture, b) an evacuation air vehicle held on said evacuation platform in a stored state and is configured to fly one or more persons that evacuate thereto from said building to a determined destination, wherein said evacuation air vehicle is configured to extend, with said support surface, within the interspace between two adjacent evacuation apertures on subsequent building floors, and one or more controllers configured to monitor and / or control the operation of various components of said evacuation system.

The present application relates to the technical field of parking apron, and proposes an assembled helicopter parking apron, which is arranged on a high-rise roof and ground and further comprises: a whole frame structure apron support frame formed by interconnecting and locking a first support pipe and a second support pipe of modular design, a modular frame body is laid on the apron support frame and locked, thereby forming a whole parking apron, the first support pipe and the second support pipe can enhance the bearing strength of the connecting part after being connected and locked, are suitable for hoisting and transportation and rapid assembly on site, the modular design of the parking apron meets the take-off and landing requirements of different areas of various types of helicopters, solves the technical defects of the prior art, such as high difficulty, environmental pollution, long construction period, high construction cost and complex design of the connecting part of the steel-aluminum structure parking apron, and the parking apron cannot be disassembled, moved and reassembled after being built, and cannot be added or modified on the already built high-rise building, and the parking apron can realize the advantages of lightweight design, factory production standardization and on-site assembly convenience.

This application provides a method, device, and storage medium for generating a low-altitude aircraft takeoff and landing area. The low-altitude aircraft arrival and departure area includes a touchdown / takeoff positioning circle, a safety zone, and an obstacle restriction zone. The obstacle restriction zone is funnel-shaped and includes a conical platform area and a cylindrical area connected in sequence. The method includes: acquiring the aircraft's technical parameters; determining the minimum outer circle diameter of the aircraft based on the technical parameters; and determining the areas of the touchdown / takeoff positioning circle, the safety zone, and the obstacle restriction zone based on the minimum outer circle diameter and a preset geometric ratio. The preset geometric ratio is the ratio between the diameter of the touchdown / takeoff positioning circle, the ring width of the safety zone, the bottom diameter of the conical platform area, and the top diameter of the conical platform area. By using the minimum outer circle diameter of the aircraft as the core, the area of ​​the low-altitude aircraft arrival and departure area is determined, resulting in a reasonable layout, saving area, and improving space utilization.

To provide a building that allows collection of transported goods received from an unmanned aerial vehicle with a small or no travel distance. [Solution] A building 100 has a flat roof 50 and another roof 60 with a rooftop wall 62, and has multiple floors, with each floor having multiple dwelling units or rooms to which the transported item L is to be transported. The flat roof 50 receives the transported item L from an unmanned aerial vehicle D, and automatic doors 65 are provided on the rooftop wall 62. A transport path 30 extending vertically across multiple floors leads to the automatic doors 65, and an elevator 35 automatically transports the transported item L inside the transport path 30. The transported item L received from the unmanned aerial vehicle D is transferred to the elevator 35 through the automatic doors 65, and the elevator 35 descends to the destination floor, and the transported item L is automatically transported to the destination.

The present invention discloses a hollow lander for an electric vertical take-off and landing aircraft, which includes a transport vehicle and a reticulated platform. A load-bearing bracket is bolted to the lower end of the reticulated platform. A lifting section is installed at the rear end of the load-bearing bracket. A lifting pillar is installed in the middle of the lifting section. The lifting pillar is composed of several standard section members. A pillar base is welded to the lower top end of the lifting pillar. The load-bearing bracket, the lifting section, the standard section, and the lifting pillar are all made of hollow steel beam structures. The reticulated platform and the load-bearing bracket form a landing platform, and the landing platform can be separated from the lifting section. Through this device, the present invention can raise the height of the entire aircraft or reduce the time spent in the landing and hovering stage, thereby greatly reducing the running time of the aircraft in the stage with the fastest energy consumption rate, successfully achieving the purpose of saving energy, and the saved energy also improves the endurance of the aircraft.

A final approach and takeoff (FATO) surface for a VTOL aircraft redirects downwash as outwash and may capture outwash from the VTOL aircraft to generate electricity. The FATO surface system may include a central solid plateau configured to capture downwash from the VTOL aircraft to enhance a ground effect for optimal stabilization during takeoff and landing. A floor grate surrounding the plateau may allow outwash to pass through to a subsurface where the outwash is channeled to exhausts or at least one turbine for generating electricity from the outwash. Redirecting the downwash to outwash reduces undesirable effects such as noise and airspeed associated with the VTOL aircraft. The electricity may be used to recharge the VTOL, electric vehicles parked at a vertiport of the FATO surface system, may be used by a building at the vertiport, or may be delivered to a local power grid.

To provide a compact and convenient drone station. [Solution] A drone station for launching and landing unmanned aerial vehicles, comprising station units that can be stacked one on top of the other and are capable of launching and landing at least one unmanned aerial vehicle, the station unit having a box-shaped housing and a stage housed in the housing, the stage being slidable horizontally between a housed state in which it is housed in the housing and an open state in which it is exposed from the housing and is capable of launching and landing the unmanned aerial vehicle.