337 results about "Hangar" patented technology

The invention discloses a data transmission system and method of an unmanned aerial vehicle, and belongs to the field of unmanned aerial vehicles. The system comprises an unmanned aerial vehicle, an unmanned aerial vehicle hangar and a vehicle, the unmanned aerial vehicle hangar is located outside the vehicle, and a beacon plate with a communication function is arranged in the unmanned aerial vehicle hangar; the unmanned aerial vehicle is used for collecting first data and sending the first data to the beacon plate based on the first data transmission parameter; and the beacon board is used for receiving the first data and sending the first data to a central control platform of the vehicle based on the second data transmission parameter. The unmanned aerial vehicle hangar is deployed outside the vehicle, the beacon plate with the communication function is arranged in the unmanned aerial vehicle hangar, the beacon plate is used for receiving the first data collected by the unmanned aerial vehicle, shielding interference of a vehicle body metal structure on wireless signals is avoided, and it is guaranteed that the first data can be stably transmitted to the beacon plate; the first and second data transmission parameters are set based on different transmission stages, the transmission strategy is flexibly adjusted, and the integrity and transmission efficiency of data transmission are improved.

The invention discloses an unmanned aerial vehicle routing inspection area path planning method, system and device based on mountain photovoltaic and a medium, and belongs to the technical field of photovoltaic power station routing inspection. The geographical environment and layout information of a photovoltaic power station area are obtained, and a photovoltaic area routing inspection route map is generated through AI three-dimensional modeling; constructing an inspection task based on the route map; according to the position of the hangar and the position of the inspection area, generating an optimized inspection path by using a path planning algorithm; one-key start and stop operation is realized through a vehicle-mounted unmanned aerial vehicle hangar, unmanned aerial vehicle autonomous inspection is executed, and visible light image data and infrared thermal imaging data are acquired; and performing defect identification and positioning on the monitoring data through a dual-light fusion automatic identification algorithm to generate a defect detection report. The problems that the mountain photovoltaic power station is low in inspection efficiency, the path is not optimized and the identification accuracy is low are solved, the inspection efficiency and accuracy are remarkably improved, the labor cost and the safety risk are reduced, and a powerful tool is provided for fine management and fault prevention of the photovoltaic power station.

The invention relates to the technical field of push-pull type hangar gates, in particular to a push-pull type hangar gate and a gate mounting construction method.The push-pull type hangar gate comprises an upper mounting frame and a lower mounting frame, and a set of movable door plates, a set of limiting door plates and a plurality of sets of splicing door plates are slidably mounted in the upper mounting frame and the lower mounting frame; the two sides of each splicing door plate can be in butt joint with the corresponding movable door plate and the corresponding limiting door plate, a driving part is installed at the front end of the lower installation frame and can push the corresponding movable door plate to move, the two splicing door plates can be automatically spliced, and the two splicing door plates can be manually disassembled to be opened. The driving part and the movable door plate can be quickly mounted, so that the sliding door can be conveniently and electrically pushed, the labor burden is reduced, the pushing efficiency is improved, any two groups of spliced door plates can be conveniently opened, entrances of different sizes can be conveniently opened in a hangar, and convenience, rapidness and time saving are achieved.

The utility model relates to the technical field of unmanned aerial vehicle supporting facilities, in particular to an unmanned aerial vehicle hangar with the adjustable layer number and an operation system thereof, and the unmanned aerial vehicle hangar comprises an operation warehouse layer, a first guarantee warehouse layer and a power module. The operation library layer is provided with a containing cavity for containing the lifting platform, and the number of the operation library layer is at least one; the first guarantee library layer is detachably connected with the operation library layer, and the operation library layer and the first guarantee library layer are arranged in a laminated mode in the preset direction. According to the unmanned aerial vehicle hangar with the adjustable layer number, a detachable connection mode is adopted, the first guarantee warehouse layer and the operation warehouse layer can be flexibly assembled and disassembled, space is saved, and the unmanned aerial vehicle hangar is suitable for various deployment scenes. The first guarantee library layer manages electric power and operation states in a centralized manner, simplifies management, improves efficiency, and ensures safe charging. The construction and maintenance cost is reduced through the modular and detachable design, the first guarantee library layer is shared to serve the multiple operation library layers, the cost is further reduced, and the resource utilization rate is increased.

The invention discloses a dual-hangar collaborative operation system for high-frequency inspection. The dual-hangar collaborative operation system comprises a remote server and two hangar subsystems which are adjacently deployed in an electric power inspection base station, the remote server communicates with the main control modules of the two hangar subsystems through the Ethernet and is used for issuing operation instructions and receiving motor state data and meteorological data. And the main control modules of the two hangar subsystems are in communication connection and are used for sharing meteorological data and operation state data and executing collaborative scheduling logic to realize parallel processing of take-off preparation and landing storage of the unmanned aerial vehicle. Depending on a double-hangar collaborative scheduling strategy, parallel processing of takeoff preparation and landing storage is achieved in a daily scene, while a first hangar executes takeoff preparation (cabin door opening, platform ascending and pressing rod loosening), a second hangar synchronously completes landing storage (unmanned aerial vehicle centering, pressing rod fixing and cabin door closing), and the unmanned aerial vehicle is taken off. And the total time consumption of single operation is shortened to be within 120s from 200s of a single-machine library.

The invention provides a modularized drawer type unmanned aerial vehicle hangar, and relates to the technical field of unmanned aerial vehicle hangars, the modularized drawer type unmanned aerial vehicle hangar comprises a plurality of unmanned aerial vehicle parking cabin structures which are stacked together in sequence, and the unmanned aerial vehicle parking cabin structures are detachably arranged so that the number of the unmanned aerial vehicle parking cabin structures can be increased or decreased; and a connecting structure is arranged on the unmanned aerial vehicle parking cabin structure. The multiple unmanned aerial vehicle parking cabin structures are arranged, the multiple unmanned aerial vehicle parking cabin structures can be independently disassembled and combined, and the number of the unmanned aerial vehicle parking cabin structures can be selected according to the actual situation; due to the fact that the multiple unmanned aerial vehicle parking cabin structures are detachably connected, the single unmanned aerial vehicle parking cabin structure is small in size and light in weight relative to the whole, and the requirement for carrying tools during transportation is lowered.

A hangar is provided for an unmanned aerial vehicle, and is suitable for being arranged on a vehicle. The hangar includes a hangar body, the hangar body being configured to accommodate the unmanned aerial vehicle; a charging apparatus, the charging apparatus being arranged in the hangar body, and the charging apparatus being configured to charge an unmanned aerial vehicle battery, wherein the unmanned aerial vehicle battery includes a first battery mounted on the unmanned aerial vehicle and / or a second battery outside the unmanned aerial vehicle; and a battery pick-and-place apparatus, the battery pick-and-place apparatus being arranged in the hangar body, and the battery pick-and-place apparatus being configured to detach the first battery from the unmanned aerial vehicle and / or mount the second battery into the unmanned aerial vehicle.

The invention discloses an impulse turbine runner abrasion loss detection method and system, an unmanned aerial vehicle hangar with a sealing door is arranged on a shell of an impulse turbine, and an unmanned aerial vehicle is placed in the unmanned aerial vehicle hangar; after the water-turbine generator set stops, the unmanned aerial vehicle is controlled to fly in the machine shell according to a set planning route, and a rotating wheel of the impulse turbine is scanned through scanning equipment carried on the unmanned aerial vehicle; and generating an actual model of the runner at the current moment based on the scanned data, comparing the actual model with a reference model of the runner, and determining the abrasion loss of the runner. The unmanned aerial vehicle hangar is arranged in the machine shell, the automatic scanning technology is adopted, non-contact type three-dimensional model comparison is achieved, high-precision three-dimensional abrasion detection can be achieved without disassembling the rotating wheel, and the detection efficiency and precision are remarkably improved.

The invention relates to the technical field of unmanned aerial vehicle paddle position adjustment, and particularly discloses a hangar unmanned aerial vehicle paddle position adjusting device, which is applied to the technical field of unmanned aerial vehicle paddle position adjustment, and comprises a hangar, a landing mechanism and an unmanned aerial vehicle, four groups of paddles are arranged on the unmanned aerial vehicle, and the landing mechanism is arranged in the hangar; the hangar comprises a nest box body, a left top door and a right top door, two sets of left rocker arms are arranged on the left side of the top of the nest box body and located on the front side and the rear side of the top of the nest box body, one ends of the two sets of left rocker arms are hinged to the nest box body, and the other ends of the two sets of left rocker arms are hinged to the left top door; elastic soft plates are arranged on the side edges of the left top door, the middle portions of the elastic soft plates are fixed to the left top door, two buffer areas are formed between the left top door and the elastic soft plates, and a dot matrix type pressure sensor and an anti-abrasion layer are arranged on the side, away from the left top door, of each elastic soft plate.

The invention discloses a hangar unmanned aerial vehicle wind disturbance resisting landing system based on multi-mode perception, which comprises an unmanned aerial vehicle, a hangar, a wind speed and direction detection unit and a visual identification unit, and is characterized in that the wind speed and direction detection unit is arranged on the hangar, and the visual identification unit is arranged on the unmanned aerial vehicle; the hangar comprises a base and a parking apron, the parking apron is rotationally connected to the base, and the landing area is arranged on the parking apron; a centering driving device and two bin covers are arranged on the parking apron, and the centering driving device is used for driving the unmanned aerial vehicle to center; the two bin covers are rotationally connected to the two longitudinal sides of the parking apron correspondingly, the bin covers are configured to be switched among a closed state, a windproof state and an open state, and when the bin covers are in the windproof state, the bin covers rotate to the highest position; the centering driving device comprises two transverse push rods and two longitudinal push rods, and the landing area is located between the two transverse push rods and the two longitudinal push rods; during landing, when the wind speed and wind direction detection unit detects that the wind speed is larger than a preset threshold value, the bin cover is controlled to be switched to the windproof state.

This application discloses a path planning method, apparatus, medium, and product for an aircraft traction system in confined spaces, relating to the field of aircraft path planning technology. The method includes: establishing a kinematic model of the aircraft traction system located in a hangar; constructing a path planning mathematical model based on the kinematic model; employing an improved hybrid algorithm to perform path search on the aircraft traction system based on the path planning mathematical model to obtain the target path of the aircraft traction system; the improved hybrid algorithm is derived from a hybrid algorithm, and the improvements include: using RS curves for bidirectional node expansion; setting the cost function to include the cumulative historical cost from the starting node to the current node and the heuristic cost from the current node to the target node; and establishing a closed table distinguishing between forward and backward directions. This application realizes path planning for an aircraft traction system in confined spaces.

The utility model provides a kind of unmanned plane vertical take-off and landing hangar, it is related to pressure vessel detection technical field, including the hangar body of one side top opening sliding slot, and the take-off and landing mechanism slidingly arranged in sliding slot, and unmanned plane body is parked on take-off and landing mechanism by landing frame, take-off and landing mechanism includes the sliding plate of being arranged in sliding slot by sliding assembly, four positioning blocks of being slidably arranged in different positioning slots, and the positioning assembly of being arranged in sliding plate and being connected four positioning blocks, four positioning slots are opened in sliding plate top end face, and the length direction of adjacent two positioning slots is perpendicular to each other;Positioning assembly controls four positioning blocks to move to the above of sliding plate and drives four positioning blocks mutually close, to landing frame center clamping and fixing.The utility model realizes the automatic vertical take-off and stable storage of unmanned plane body, improves the practical convenience, safety and stability of unmanned plane body.

1. The name of this design product: UAV hangar. 2. Purpose of this design product: used for docking, data transmission and charging of drones. 3. The key point of the design of this product lies in its shape. 4. The picture or photo that best illustrates the design points: three-dimensional picture.

The invention discloses a locking mechanism, a cabin door assembly, a vehicle-mounted unmanned aerial vehicle hangar with the cabin door assembly and a vehicle. A sliding bracket; the locking piece is movably arranged on the sliding support between a locking position and an unlocking position, the locking piece is matched with the locking piece in a locking mode at the locking position so that the sliding support and the locking piece can be relatively fixed, and the locking piece is matched with the locking piece in a disengaged mode at the unlocking position; and the driving sliding block is arranged on the sliding support, and the driving sliding block is used for driving the locking piece to move between the unlocking position and the locking position. According to the locking mechanism, the cabin door can be stably and reliably locked and closed after being closed, so that the cabin door can stably and reliably lock the vehicle-mounted unmanned aerial vehicle hangar, and the vehicle-mounted unmanned aerial vehicle hangar has a good anti-theft effect.

The application relates to the technical field of unmanned vehicle hangars, in particular to a self-cleaning unmanned vehicle hangar, which comprises a hangar box body, an opening is formed at the upper end of the hangar box body, and a mounting cavity is formed at the inner side of the hangar box body; a mounting frame is arranged at the inner side of the mounting cavity, a lifting mechanism is fixedly arranged on the mounting frame, a sand blocking plate is fixedly connected to the lifting end of the lifting mechanism, the sand blocking plate is conical, a receiving platform is fixedly connected above the sand blocking plate, the receiving platform comprises a supporting frame and a supporting net plate, the supporting frame is rectangular, the supporting net plate is formed at the inner side of the supporting frame, and the supporting net plate supports unmanned vehicles; and a homing mechanism for moving the position of the unmanned vehicle is arranged on the supporting frame. Through the above technical scheme, the sand and dust on the receiving platform can be automatically cleaned, a large amount of sand and dust can be prevented from accumulating on the receiving platform, and the accuracy of the unmanned vehicle homing in the hangar can be ensured.

The utility model provides an unmanned aerial vehicle hangar which comprises a cabin body, at least one cabin door, at least one first transmission rod and at least one second transmission rod. A cabin opening is formed in the top of the cabin body. The first transmission rod corresponds to the cabin door, the first end of the first transmission rod is rotationally connected to the cabin body around a first pivot axis, and the second end of the first transmission rod is rotationally connected to the cabin door around a second pivot axis. The second transmission rod corresponds to the cabin door, the first end of the second transmission rod is rotationally connected to the cabin body around a third pivot axis, and the second end of the second transmission rod is rotationally connected to the cabin door around a fourth pivot axis. Wherein the first pivot axis, the second pivot axis, the third pivot axis and the fourth pivot axis are arranged in parallel, so that the cabin door can be movably connected to the cabin body between a closed position and an open position. According to the unmanned aerial vehicle hangar, the overlarge space inside and outside the cabin cannot be occupied, and the influence on take-off and landing of an unmanned aerial vehicle is reduced.

This utility model relates to the field of drone receiving and discloses a drone receiving system. The drone receiving system includes a hangar main body, a control unit, a positioning module, a platform component, and a drive component. This application, by incorporating a retractable and movable platform component and a rotatable protective plate, allows the system to switch between a flat and enclosed state. In the flat state, the protective plate and the flat plate together form a flat landing surface, facilitating safe take-off and landing of the drone. In the enclosed state, the protective plate and the flat material receiving cavity effectively prevent accidental slippage or damage to materials during delivery, significantly improving the safety and reliability of material transfer. This design is suitable for fully automated operations, especially for unattended delivery scenarios.

1. The name of the design product: UAV hangar elevator. 2. The use of the design product: used for lifting objects to facilitate the loading and unloading of objects by UAVs. 3. The design points of the design product: in shape. 4. The picture or photo that best indicates the design points: perspective view. 5. The bottom of the design product is not easily visible or not visible during use, and the top view is omitted.

The invention discloses an unmanned aerial vehicle stereoscopic hangar, and particularly relates to the technical field of unmanned aerial vehicle storing and taking equipment, the unmanned aerial vehicle stereoscopic hangar comprises a bottom plate, a protection frame is arranged at the upper end of the bottom plate, an alarm is arranged at the upper end of the protection frame, a conveying device is arranged on one side of the upper end of the bottom plate, and one end of the conveying device extends out of the protection frame; a storage cabinet is arranged on the other side of the upper end of the bottom plate, a lifting device is arranged in the middle of the upper end of the bottom plate, and a containing device is arranged in the middle of the outer surface of the lifting device. According to the three-dimensional hangar for the unmanned aerial vehicle, the containing pieces on the upper side and the lower side of the conveying device can alternately and circularly work, when the containing pieces carrying the unmanned aerial vehicle are conveyed to the inner cavity of the protection frame, the containing pieces on the lower portion are synchronously conveyed to the upper working position, the follow-up landing unmanned aerial vehicle can be continuously borne, and the waiting time of single-station bearing of a traditional hangar is avoided; and the receiving and storage efficiency of the unmanned aerial vehicle is remarkably improved.

The invention relates to the technical field of new energy station intelligent inspection, in particular to a new energy station intelligent safety inspection method and system, and the method comprises the steps: judging whether an inspection condition is satisfied, and starting an unmanned plane inspection task if the inspection condition is satisfied; generating a dynamic inspection path; performing intelligent safety inspection on the new energy station based on the dynamic inspection path, and collecting personnel operation image information of a target area in real time; the personnel operation image information is transmitted to the cloud server through the hangar center; and the cloud server identifies unsafe behaviors according to the personnel operation image information, marks key information of the hidden danger picture, determines the operation personnel with nonstandard behaviors and information thereof according to the key information, and outputs a potential safety hazard prompt signal. According to the invention, unmanned aerial vehicle inspection full coverage, least time and high unmanned aerial vehicle safety inspection efficiency are realized through dynamic path planning, hidden danger identification reminding is carried out, illegal behaviors are corrected in time, the station safety supervision efficiency and the production safety level are improved, and energy safety and green low-carbon development are guaranteed.

Provided are a portable aircraft communication navigation system detection device and a detection method for the same. The portable aircraft communication navigation system detection device comprises a body, a radio frequency signal analysis assembly, a radio frequency signal generation assembly, a control assembly, and the like. The radio frequency signal analysis assembly comprises a standing wave analysis module, a power / frequency analysis module, a 30 dB attenuator, two radio frequency input ports, and one radio frequency output port. The radio frequency signal generation assembly comprises a radio frequency module, a program-controlled attenuator, a communication signal output port, and a navigation signal output port. The control assembly comprises a main control unit, a touch display, and the like. The present application is dedicated to solving the technical problems that hidden faults of an external field communication system cannot be found, a navigation system requires many first-line maintenance support devices, and a compass signal cannot be received in a hangar or hangar, thereby leading to the fact that the compass cannot be checked. The present application can quickly complete the first-line in-situ performance detection of short-wave radio stations, ultra-short-wave radio stations, filters, power adders, antennas, and the like, and is suitable for the inspection of communication navigation devices of various types of aircraft.

This invention pertains to a ship hangar-boat conversion system in the field of ship technology. An upper deck (2) is located aft of the flight deck (1), with the flight deck (1) and the upper deck floor (3) flush. An unmanned surface vessel (USV) passageway (4) is located below the flight deck (1), with the lower deck floor (9) and the USV passageway floor (5) flush. A hinged deck (8) is located aft of the upper deck floor (3), and a lifting platform (12) is located on the lower deck floor (9) below the hinged deck (8). A slot (18) is located on the USV passageway floor (5) along the extension direction of the USV passageway (4), and a hinged USV slideway (10) is installed within the slot (18). The ship hangar-boat conversion system described in this invention alleviates the shortcomings of traditional USV retrieval and deployment, which are slow and prone to damage. It transforms the occasional use of high-end equipment such as drones and USVs into routine equipment, enabling drone / USV / mother ship collaboration and improving space utilization.

Provided are a horizontal moving device for short-distance movement of a UAV in a hangar and a transfer method thereof, comprising a bracket for accommodating and limiting the wheels of the UAV, both ends of the bracket being fixed with mounting racks, one of the mounting racks being provided with a traction device for pulling or pushing the device, the bottom of each mounting rack being provided with a heavy load caster for supporting movement of the device, and the mounting rack being provided with a direction locking mechanism, and the heavy load caster being connected or separated from the direction locking mechanism by controlling the state of the direction locking mechanism, so as to limit or release the rotation freedom of the heavy load caster. By means of the V-shaped clamping groove and the caster capable of quickly switching the locking mode, the UAV can be stably placed on the device after being jacked up, flexible turning, directional movement and rotation in place of the UAV in a narrow space are realized, and the problems of damage to the UAV and low transfer efficiency in the process of traditional manual pushing or simple tool movement are effectively solved. The device has the advantages of simple structure, easy operation, reliable bearing, high safety, etc.

The utility model relates to the field of unmanned plane, disclose a kind of unmanned plane hangar with automatic charging structure, including base, the top of base is fixedly connected with box, the inside of box is provided with fixed mechanism, the fixed mechanism includes slide rail, the bottom of slide rail is fixedly connected in the bottom of base, the outer wall of slide rail is slidably connected with lifting plate, the outer wall of base is fixedly connected with outer support, the outer wall of lifting plate is hinged with connecting rod A, the outer wall of connecting rod A is slidably connected with outer connecting block. In the utility model, under the cooperation of slide rail, lifting plate, connecting rod B, clamping plate, pawl, ratchet wheel, step rope, foot pedal, pawl is separated from ratchet wheel by stepping down step rope, lifting plate is driven to move down by lifting foot pedal, and then clamping plate moves along guide slide rod, realize the fixation of unmanned plane, ensure its transport stability and calibrate and the contact position of charging plate.

The invention discloses a balance control method and device for a hangar, electronic equipment and a storage medium, and the method comprises the steps: determining a second rotation angle of each reference bearing part on a rotating device if the angle orientation of a target part on the rotating device is not in a preset angle interval; the second rotation angle is a rotation angle generated by each reference bearing part relative to the reference marker when the rotation of the rotating device is completed, and the reference bearing parts are bearing parts for bearing objects on the rotating device; each second rotating angle comprises a reference angle deviation generated by a reference bearing part on the rotating device when the rotating device rotates; determining a correction angle based on the second rotation angle; and based on the corrected angle, driving the rotating device to perform angle adjustment, so that the angle orientation of the target component on the rotating device is in a preset angle interval. According to the scheme, the deviation angle generated after rotation can be accurately corrected, and accurate balance control over the rotating device in the hangar is achieved.

The utility model discloses a ventilation grille, an unmanned aerial vehicle garage and a vehicle. The ventilation grille is applied to the unmanned aerial vehicle garage and comprises grille holes and a mounting part, the grille holes are suitable for communicating an unmanned aerial vehicle containing cavity in the unmanned aerial vehicle garage with the external environment, and the ventilation grille is suitable for being detachably mounted on the unmanned aerial vehicle garage through the mounting part. According to the ventilation grille, the ventilation grille is detachably mounted on the unmanned aerial vehicle garage through the mounting part, so that the ventilation grille can be detached and cleaned or replaced at any time, the problem that the ventilation and heat dissipation performance is reduced due to long-term accumulation of dirt (such as dust and foreign matter) is solved, and the durability and heat dissipation performance of the ventilation grille are improved.

The invention belongs to the field of aircraft design, and particularly relates to a long-endurance aircraft layout design structure which is characterized in that a fuselage is divided into three sections which are arranged side by side, and wings are divided into three sections which are connected end to end; the fuselages are connected with the adjacent wings through rotating shafts, and the adjacent fuselages are connected through rotating shafts; the adjacent wings can be driven to be close to or away from each other by controlling the rotating shafts to rotate; the fuselage and the wings can form a hangar storage form, a take-off and landing operation form and an air flight form. Firstly, the hangar storage form size of the long-endurance airplane is compact, the spanwise size is favorably controlled, and the airplane can be conveniently stored in the hangar and subjected to other operations; secondly, design constraints such as geometric dimensions, lift force characteristics, control capacity and load impact are considered in the take-off and landing operation form, and the aircraft is supported to complete catapult-assisted take-off and landing arresting operation. Finally, the span-chord ratio of the air flight form is large, the aerodynamic efficiency is improved, and the mission ability of the aircraft is enhanced.

The application provides a mine tunnel inspection unmanned aerial vehicle and positioning system based on laser radar and UWB ranging, and relates to the technical field of mine tunnel unmanned aerial vehicle inspection.The application can adapt to the positioning of the unmanned aerial vehicle in the mine tunnel environment through 360 laser radar and UWB ranging, so that the unmanned aerial vehicle can fly safely in the mine tunnel environment where light is dim and dust spreads due to long-term closure, and can land accurately in the preset hangar when necessary, thereby solving the key problem of the autonomous inspection of the unmanned aerial vehicle in the mine tunnel and expanding the application scenario of the unmanned aerial vehicle system in the inspection task.The application obtains the position and attitude of the unmanned aerial vehicle in the launch inertial system through the laser radar, so as to provide feedback control for the position and speed control module, and obtains the distance between the unmanned aerial vehicle and the UWB base station, so as to obtain the approximate position of the unmanned aerial vehicle in the mine tunnel and the relative position relationship with the hangar, thereby realizing the preliminary positioning of the landing point of the unmanned aerial vehicle, and being beneficial to the accurate positioning and landing of the unmanned aerial vehicle in the preset hangar.

The utility model relates to an unmanned plane technical field discloses a hangar system for unmanned plane power supply, including commercial power input module and hangar core control module, the output end electric connection of commercial power input module has many power management module, the output end electric connection of many power management module has communication navigation module and mechanical execution module's input respectively, many power management module and hangar core control module two -way electric connection, communication connection of communication navigation module's output and mechanical execution module's input. In the utility model, through commercial power and solar energy parallel connection access many power management module, realized the complementary power supply of commercial power, solar energy, charges for battery group simultaneously, gets rid of single battery capacity limit, still guarantees unmanned plane to continue working when power failure, satisfies the long -term operation demand of unmanned plane.