120results 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.

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.

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.

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 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.

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.

The invention discloses an aircraft take-off and landing system for a building, the building and an emergency response control method of the building. The aircraft take-off and landing system comprises a take-off and landing platform; the deployment mechanism is connected with the take-off and landing platform and used for driving the take-off and landing platform to move between a storage position where the take-off and landing platform is stored in the building and a deployment position where the take-off and landing platform extends out of the building; the door control assembly is used for being installed on an enclosure structure of a building to open and close a channel, and the lifting platform moves between the storage position and the deployment position through the channel. Through the working mode of deployment according to needs and storage after use, the problems that a traditional parking apron is large in occupied space, high in building structure requirement and limited in application are effectively solved; meanwhile, rapid and automatic deployment is carried out by responding to an emergency event signal, the system is allowed to be arranged in a safer building middle floor, and the response speed and rescue efficiency under the emergency condition are remarkably improved.

The invention discloses an unmanned aerial vehicle parking apron which comprises a parking apron plate, a first telescopic rod, a second telescopic rod, a sensing assembly, a driving assembly and a controller. One end of the first telescopic rod is connected with the movable end on the side edge of the parking apron plate through a first connecting piece, and one end of the second telescopic rod is connected with the movable end on the other side edge of the parking apron plate through a second connecting piece; the sensing assembly at least comprises a millimeter wave radar and an optical sensor. According to the invention, the damage caused by the deviation of the landing position or the unstable attitude of the unmanned aerial vehicle can be effectively reduced, and the landing safety and precision are improved; the parking apron is automatically adjusted according to the actual state of the unmanned aerial vehicle, dependence on experience of operators is reduced, operation is easier and more convenient, human errors are reduced, and operation efficiency and reliability are improved.

The present specification discloses a method and device for aligning a UAV. First, light curtain sensor data of the landing gear column of the UAV parked in the parking area collected by the light curtain sensor is acquired. Second, the corresponding position coordinates of the landing gear column of the UAV in the parking area are determined according to the light curtain sensor data. Finally, the push rod assembly is controlled to align the UAV in the parking area according to the position coordinates. The method can determine the corresponding position coordinates of the landing gear column of the UAV in advance, control each push rod assembly to apply a pushing force to the UAV at the same time, and improve the efficiency of aligning the UAV.

The invention discloses a double-layer aircraft take-off and landing platform capable of self-adapting to an inclined plane and a control method. The double-layer aircraft take-off and landing platform comprises a lower-layer fixing mechanism and an upper-layer take-off and The lower layer fixing mechanism is connected with the upper layer lifting plate through three rod pieces, and the three rod pieces are two telescopic rods driven by a stepping motor and a supporting rod with the fixed length. The joints of the three rod pieces and the lower layer fixing mechanism and the joints of the three rod pieces and the upper layer take-off and landing plate are universal joints; a gyroscope is arranged in the upper layer take-off and landing plate and electrically connected with the controller, and the controller is used for driving the stepping motor to stretch out and draw back according to an attitude signal detected by the gyroscope so as to dynamically adjust the levelness of the upper layer take-off and landing plate; the invention solves the problem of how to keep the take-off and landing platform horizontal on non-horizontal supporting surfaces such as stair handrails so as to improve the stability of an aircraft during landing.

The invention relates to an automatic spreading helicopter pad and a preparation method thereof. The method comprises the following steps: preparing pad base cloth; tailoring and sewing the base cloth: tailoring the base cloth into a plurality of unit blocks, and performing double-layer sewing on the tailored unit blocks; supporting ribs and torsional springs are installed, specifically, according to design requirements, the supporting ribs are correspondingly inserted into each double-layer sewn unit block, and the multiple torsional springs are installed on part of the supporting ribs; the edge of each unit block is covered and sewn, and the connecting sleeves are installed on the covered edges; splicing: splicing the plurality of unit blocks into a circular landing pad through the connecting sleeves and the connecting ribs; folding and packaging: folding the spliced landing pad into an umbrella-shaped structure, and bundling the umbrella-shaped structure into a roll by using a rope to form an automatic spreading helicopter landing pad product; when the rope is released, the torsion spring releases pressure and is opened, and the circular landing pad is automatically unfolded. The foldable and portable folding-type automatic spreading device can be quickly and automatically spread, and has the advantages of light weight, high bearing strength, folding portability and good environmental adaptability.

A drone delivery system provides to send or to receive the package conveniently and safely without going out of the building by using the platform installed at the vicinity of the window. The drone delivery system includes the drone having a first docking device, a standard box having a second docking device corresponding to the first docking device and a third docking device and a platform having a fourth docking device corresponding to the third docking device.

The invention relates to the technical field of unmanned aerial vehicle logistics, and particularly discloses a roof receiving device for unmanned aerial vehicle logistics and personnel connection, which comprises a receiving cabinet arranged on the roof of a building, the section of the receiving cabinet is L-shaped, the outer sides of the horizontal section and the vertical section of the receiving cabinet are respectively provided with a plurality of vertical cavities and transverse cavities, an opening of the vertical cavity is provided with a cabinet door through an elastic locking mechanism; the first parking apron is arranged at the top end of the horizontal section of the receiving cabinet and is communicated with the vertical cavity; the bearing box is arranged in the transverse cavity in a sliding mode, a second parking apron is arranged at the top end of the bearing box, and an opening of the bearing box is provided with a box door through an elastic locking mechanism; the driving mechanism is used for adjusting the bearing box to enter and exit the transverse cavity; and the limiting mechanism is arranged in the transverse cavity. According to the invention, the wide transverse and longitudinal spaces of the roof are fully utilized, a high-capacity three-dimensional storage structure integrating high and low storage units is constructed, and the intelligent goods sorting function is achieved.

The utility model relates to the technical field of buildings, in particular to a building with staggered balconies, which comprises a plurality of floors, balconies are arranged on two floors which are separated from each other by at least one floor, a landing space for an unmanned aerial vehicle to land is arranged on the balconies, and the landing space at least penetrates through the two floors. By the adoption of the design mode, due to the fact that the landing space penetrating through the at least two floors is formed on the balcony, when the unmanned aerial vehicle needs to deliver expresses to the home, the landing space can guarantee that the unmanned aerial vehicle enters the balcony from the position above a balcony handrail, and the expresses are safely delivered to the balcony ground of a target resident; therefore, an efficient logistics distribution mode is realized.

The invention discloses an implantable low-altitude aircraft take-off and landing platform which is characterized in that a plurality of support buildings are arranged on a foundation structure, and a plurality of first entrances connected to an external existing building are formed in the side faces of the support buildings; the structural frame is fixed and communicated to at least one support building, a lifting layer is arranged at the top of the structural frame, a hangar layer and a boarding layer are further arranged below the lifting layer, and the lifting part is arranged in the structural frame and comprises a lifting structure and a lifting platform; according to the implantable low-altitude aircraft take-off and landing platform, the take-off and landing layer, the hangar layer and the boarding layer are all arranged above the external existing building, so that the implantable low-altitude aircraft take-off and landing platform has a large installation space and can be well matched with the existing building; a plurality of first entrances connected to an external existing building are formed in the side face of the support building, and the lifting structure drives the lifting platform to be transferred among the lifting layer, the hangar layer and the boarding layer. In the using process of the lifting part of the functional building, personnel and materials are transferred from the eVTOL or transferred out of the functional building.