WO2021117296A1 - 屋根構造 - Google Patents
屋根構造 Download PDFInfo
- Publication number
- WO2021117296A1 WO2021117296A1 PCT/JP2020/031329 JP2020031329W WO2021117296A1 WO 2021117296 A1 WO2021117296 A1 WO 2021117296A1 JP 2020031329 W JP2020031329 W JP 2020031329W WO 2021117296 A1 WO2021117296 A1 WO 2021117296A1
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- WO
- WIPO (PCT)
- Prior art keywords
- drone
- cover
- roof
- port
- accommodating portion
- Prior art date
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Images
Classifications
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- E—FIXED CONSTRUCTIONS
- E04—BUILDING
- E04B—GENERAL BUILDING CONSTRUCTIONS; WALLS, e.g. PARTITIONS; ROOFS; FLOORS; CEILINGS; INSULATION OR OTHER PROTECTION OF BUILDINGS
- E04B7/00—Roofs; Roof construction with regard to insulation
- E04B7/16—Roof structures with movable roof parts
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- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02S—GENERATION OF ELECTRIC POWER BY CONVERSION OF INFRARED RADIATION, VISIBLE LIGHT OR ULTRAVIOLET LIGHT, e.g. USING PHOTOVOLTAIC [PV] MODULES
- H02S20/00—Supporting structures for PV modules
- H02S20/20—Supporting structures directly fixed to an immovable object
- H02S20/22—Supporting structures directly fixed to an immovable object specially adapted for buildings
- H02S20/23—Supporting structures directly fixed to an immovable object specially adapted for buildings specially adapted for roof structures
- H02S20/24—Supporting structures directly fixed to an immovable object specially adapted for buildings specially adapted for roof structures specially adapted for flat roofs
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60L—PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES; SUPPLYING ELECTRIC POWER FOR AUXILIARY EQUIPMENT OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRODYNAMIC BRAKE SYSTEMS FOR VEHICLES IN GENERAL; MAGNETIC SUSPENSION OR LEVITATION FOR VEHICLES; MONITORING OPERATING VARIABLES OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRIC SAFETY DEVICES FOR ELECTRICALLY-PROPELLED VEHICLES
- B60L53/00—Methods of charging batteries, specially adapted for electric vehicles; Charging stations or on-board charging equipment therefor; Exchange of energy storage elements in electric vehicles
- B60L53/30—Constructional details of charging stations
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60L—PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES; SUPPLYING ELECTRIC POWER FOR AUXILIARY EQUIPMENT OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRODYNAMIC BRAKE SYSTEMS FOR VEHICLES IN GENERAL; MAGNETIC SUSPENSION OR LEVITATION FOR VEHICLES; MONITORING OPERATING VARIABLES OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRIC SAFETY DEVICES FOR ELECTRICALLY-PROPELLED VEHICLES
- B60L53/00—Methods of charging batteries, specially adapted for electric vehicles; Charging stations or on-board charging equipment therefor; Exchange of energy storage elements in electric vehicles
- B60L53/50—Charging stations characterised by energy-storage or power-generation means
- B60L53/51—Photovoltaic means
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/08—Helicopters with two or more rotors
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/02—Aircraft not otherwise provided for characterised by special use
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F1/00—Ground or aircraft-carrier-deck installations
- B64F1/12—Ground or aircraft-carrier-deck installations for anchoring aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F1/00—Ground or aircraft-carrier-deck installations
- B64F1/36—Other airport installations
- B64F1/362—Installations for supplying conditioned air to parked aircraft
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- E—FIXED CONSTRUCTIONS
- E01—CONSTRUCTION OF ROADS, RAILWAYS, OR BRIDGES
- E01F—ADDITIONAL WORK, SUCH AS EQUIPPING ROADS OR THE CONSTRUCTION OF PLATFORMS, HELICOPTER LANDING STAGES, SIGNS, SNOW FENCES, OR THE LIKE
- E01F3/00—Landing stages for helicopters, e.g. located above buildings
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- E—FIXED CONSTRUCTIONS
- E04—BUILDING
- E04B—GENERAL BUILDING CONSTRUCTIONS; WALLS, e.g. PARTITIONS; ROOFS; FLOORS; CEILINGS; INSULATION OR OTHER PROTECTION OF BUILDINGS
- E04B7/00—Roofs; Roof construction with regard to insulation
- E04B7/16—Roof structures with movable roof parts
- E04B7/166—Roof structures with movable roof parts characterised by a translation movement of the movable roof part, with or without additional movements
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- E—FIXED CONSTRUCTIONS
- E04—BUILDING
- E04B—GENERAL BUILDING CONSTRUCTIONS; WALLS, e.g. PARTITIONS; ROOFS; FLOORS; CEILINGS; INSULATION OR OTHER PROTECTION OF BUILDINGS
- E04B7/00—Roofs; Roof construction with regard to insulation
- E04B7/18—Special structures in or on roofs, e.g. dormer windows
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- E—FIXED CONSTRUCTIONS
- E04—BUILDING
- E04D—ROOF COVERINGS; SKY-LIGHTS; GUTTERS; ROOF-WORKING TOOLS
- E04D13/00—Special arrangements or devices in connection with roof coverings; Protection against birds; Roof drainage ; Sky-lights
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- E—FIXED CONSTRUCTIONS
- E04—BUILDING
- E04H—BUILDINGS OR LIKE STRUCTURES FOR PARTICULAR PURPOSES; SWIMMING OR SPLASH BATHS OR POOLS; MASTS; FENCING; TENTS OR CANOPIES, IN GENERAL
- E04H6/00—Buildings for parking cars, rolling-stock, aircraft, vessels or like vehicles, e.g. garages
- E04H6/44—Buildings for parking cars, rolling-stock, aircraft, vessels or like vehicles, e.g. garages for storing aircraft
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- E—FIXED CONSTRUCTIONS
- E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
- E05F—DEVICES FOR MOVING WINGS INTO OPEN OR CLOSED POSITION; CHECKS FOR WINGS; WING FITTINGS NOT OTHERWISE PROVIDED FOR, CONCERNED WITH THE FUNCTIONING OF THE WING
- E05F15/00—Power-operated mechanisms for wings
- E05F15/70—Power-operated mechanisms for wings with automatic actuation
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- E—FIXED CONSTRUCTIONS
- E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
- E05F—DEVICES FOR MOVING WINGS INTO OPEN OR CLOSED POSITION; CHECKS FOR WINGS; WING FITTINGS NOT OTHERWISE PROVIDED FOR, CONCERNED WITH THE FUNCTIONING OF THE WING
- E05F15/00—Power-operated mechanisms for wings
- E05F15/70—Power-operated mechanisms for wings with automatic actuation
- E05F15/73—Power-operated mechanisms for wings with automatic actuation responsive to movement or presence of persons or objects
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- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02J—CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
- H02J50/00—Circuit arrangements or systems for wireless supply or distribution of electric power
- H02J50/10—Circuit arrangements or systems for wireless supply or distribution of electric power using inductive coupling
- H02J50/12—Circuit arrangements or systems for wireless supply or distribution of electric power using inductive coupling of the resonant type
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- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02J—CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
- H02J7/00—Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries
- H02J7/34—Parallel operation in networks using both storage and other dc sources, e.g. providing buffering
- H02J7/35—Parallel operation in networks using both storage and other dc sources, e.g. providing buffering with light sensitive cells
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- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02S—GENERATION OF ELECTRIC POWER BY CONVERSION OF INFRARED RADIATION, VISIBLE LIGHT OR ULTRAVIOLET LIGHT, e.g. USING PHOTOVOLTAIC [PV] MODULES
- H02S20/00—Supporting structures for PV modules
- H02S20/20—Supporting structures directly fixed to an immovable object
- H02S20/22—Supporting structures directly fixed to an immovable object specially adapted for buildings
- H02S20/23—Supporting structures directly fixed to an immovable object specially adapted for buildings specially adapted for roof structures
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60L—PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES; SUPPLYING ELECTRIC POWER FOR AUXILIARY EQUIPMENT OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRODYNAMIC BRAKE SYSTEMS FOR VEHICLES IN GENERAL; MAGNETIC SUSPENSION OR LEVITATION FOR VEHICLES; MONITORING OPERATING VARIABLES OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRIC SAFETY DEVICES FOR ELECTRICALLY-PROPELLED VEHICLES
- B60L2200/00—Type of vehicles
- B60L2200/10—Air crafts
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- E—FIXED CONSTRUCTIONS
- E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
- E05Y—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES E05D AND E05F, RELATING TO CONSTRUCTION ELEMENTS, ELECTRIC CONTROL, POWER SUPPLY, POWER SIGNAL OR TRANSMISSION, USER INTERFACES, MOUNTING OR COUPLING, DETAILS, ACCESSORIES, AUXILIARY OPERATIONS NOT OTHERWISE PROVIDED FOR, APPLICATION THEREOF
- E05Y2400/00—Electronic control; Electrical power; Power supply; Power or signal transmission; User interfaces
- E05Y2400/10—Electronic control
- E05Y2400/40—Control units therefor
-
- E—FIXED CONSTRUCTIONS
- E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
- E05Y—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES E05D AND E05F, RELATING TO CONSTRUCTION ELEMENTS, ELECTRIC CONTROL, POWER SUPPLY, POWER SIGNAL OR TRANSMISSION, USER INTERFACES, MOUNTING OR COUPLING, DETAILS, ACCESSORIES, AUXILIARY OPERATIONS NOT OTHERWISE PROVIDED FOR, APPLICATION THEREOF
- E05Y2900/00—Application of doors, windows, wings or fittings thereof
- E05Y2900/10—Application of doors, windows, wings or fittings thereof for buildings or parts thereof
- E05Y2900/13—Type of wing
-
- E—FIXED CONSTRUCTIONS
- E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
- E05Y—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES E05D AND E05F, RELATING TO CONSTRUCTION ELEMENTS, ELECTRIC CONTROL, POWER SUPPLY, POWER SIGNAL OR TRANSMISSION, USER INTERFACES, MOUNTING OR COUPLING, DETAILS, ACCESSORIES, AUXILIARY OPERATIONS NOT OTHERWISE PROVIDED FOR, APPLICATION THEREOF
- E05Y2900/00—Application of doors, windows, wings or fittings thereof
- E05Y2900/10—Application of doors, windows, wings or fittings thereof for buildings or parts thereof
- E05Y2900/13—Type of wing
- E05Y2900/148—Windows
- E05Y2900/152—Roof windows
- E05Y2900/154—Skylights
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- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02J—CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
- H02J2310/00—The network for supplying or distributing electric power characterised by its spatial reach or by the load
- H02J2310/40—The network being an on-board power network, i.e. within a vehicle
- H02J2310/44—The network being an on-board power network, i.e. within a vehicle for aircrafts
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02B—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO BUILDINGS, e.g. HOUSING, HOUSE APPLIANCES OR RELATED END-USER APPLICATIONS
- Y02B10/00—Integration of renewable energy sources in buildings
- Y02B10/10—Photovoltaic [PV]
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E10/00—Energy generation through renewable energy sources
- Y02E10/50—Photovoltaic [PV] energy
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/60—Other road transportation technologies with climate change mitigation effect
- Y02T10/70—Energy storage systems for electromobility, e.g. batteries
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/60—Other road transportation technologies with climate change mitigation effect
- Y02T10/7072—Electromobility specific charging systems or methods for batteries, ultracapacitors, supercapacitors or double-layer capacitors
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T90/00—Enabling technologies or technologies with a potential or indirect contribution to GHG emissions mitigation
- Y02T90/10—Technologies relating to charging of electric vehicles
- Y02T90/12—Electric charging stations
Definitions
- the present invention relates to a roof structure including a drone port on which a drone can take off and land.
- UAVs Unmanned Aerial Vehicles
- drones small unmanned aerial vehicles
- UAVs Unmanned Aerial Vehicles
- Drones are inexpensive and easy to operate, so there have been high costs and dangers such as taking aerial photographs and inspecting high places and dangerous places with the camera mounted on the drone. Such work can be done cheaply and easily with a drone.
- drones are often manually operated mainly by operators using remote controllers.
- drones can be made to fly autonomously by mounting various sensors such as position sensors, image sensors, and acceleration sensors in addition to cameras.
- various drones using such autonomously flying drones are used. Research and development of various services and systems are underway.
- the surveillance cameras are fixed at the place where they are installed, so if you try to install surveillance cameras so that blind spots do not occur, you will need a large number of surveillance cameras, and installation of surveillance cameras It is difficult to secure a place, and the cost for installation work and maintenance will increase. It is expected that such problems will be solved if the drone is equipped with cameras and sensors and the drone can automatically patrol and monitor the premises.
- a drone dock that can take off and land, can be charged, and has a function as a housing is installed on the site to be monitored, and the drone is autonomously moved from the drone dock. Take off and land on the drone to perform autonomous flight of a predetermined flight path, send the monitoring data acquired by the camera mounted on the drone to the server, and check the monitoring data from a remote terminal etc.
- An automatic drone security system is disclosed.
- Non-Patent Document 1 a demonstration experiment of a patrol monitoring service using an autonomous flight monitoring drone was conducted for large facilities such as prisons where human patrol security is performed, and some of the services are operated. It is stated that has been started.
- Non-Patent Document 1 also shows how a drone dock capable of taking off and landing and charging a drone as described in Patent Document 1 is installed on the premises. At present, it seems that some of the demonstration experiments and operations of services for large facilities have begun, but in the future, it will spread to general housing and the premises of the housing will be automatically drone. It is expected that services such as monitoring will be provided.
- Patent Document 2 describes a drone that can be installed in an outdoor space of a building such as a common corridor in an apartment house, a hospital or other building, and can deliver luggage by the drone.
- the port is listed.
- the drone port described in Patent Document 2 has a fixing member that can be fixed between the floor and the ceiling outside the building, or a handrail outside the building, and a flat surface for receiving luggage from the drone. It is provided with a stage so that the stage can be moved and returned by a predetermined distance in a substantially horizontal direction by rotating and / or sliding with respect to the fixing member while maintaining the horizontal state of the flat surface portion.
- Patent Document 3 describes a balcony structure of a building in which a parcel can be delivered directly to each dwelling unit even in an apartment house when delivering a home using a drone.
- the balcony structure of the building described in Patent Document 3 is a balcony structure including adjacent dwelling units and continuous balconies along the dwelling units, and has a protruding floor portion protruding outward from the outer reference surface of the balcony, and the protruding floor.
- Patent Document 2 and Patent Document 3 disclose the invention of a drone port provided in a house, both of them are installed in an apartment house and are installed in an outdoor common corridor or a balcony. Therefore, the drone port described in Patent Document 2 installed in a common corridor having an outdoor floor and ceiling cannot be installed when an outdoor common corridor is not provided as in a detached house. Further, in the invention described in Patent Document 3, it is necessary to provide a protruding floor portion that projects further outward than the outer reference surface of the balcony, and it is not possible to secure a space for providing the protruding floor portion on the outside of the balcony. Not applicable in some cases.
- the inventions described in Patent Document 2 and Patent Document 3 are also drone ports for home delivery services using drones, and drones flying from the outside temporarily deliver luggage.
- the drone ports described in Patent Documents 2 and 3 do not take into consideration the influence of weather such as wind, rain, and snow.
- the common corridor is a passage for people to pass through, and the balcony is used to hang laundry, etc. Because of this, people may enter the space, and things such as the outdoor unit of the air conditioner may be placed in the space, so the space that can be used as a common corridor or balcony will be smaller due to the installed drone port, or the drone.
- a drone port on the roof which is usually installed in every house without people entering or placing objects on it.
- the roof of a house is often a sloped roof such as a gable roof, a hipped roof, or a one-sided roof, rather than a horizontal flat roof. Therefore, the drone dock as described in Patent Document 1 cannot be installed as it is on the sloping roof. Even if it is installed, it is unstable and there is a risk of falling.
- Patent Document 2 and Patent Document 3 do not describe that the drone port is installed on the roof, and even if it is installed on the roof, the roof is different from the common corridor and the balcony, and is around.
- the present invention has been made in view of the above circumstances, and a drone port can be provided on a sloping roof so that a drone can take off and land in a stable manner.
- the purpose is to provide a roof structure that can be protected from the effects of the weather.
- the roof structure according to the present invention accommodates a sloping roof that covers the upper part of the building and a drone that is provided so as to cut out a part of the sloping roof so that the bottom surface is substantially horizontal.
- the drone accommodating portion is provided with an entrance / exit through which the drone can enter and exit, and the cover is configured to be openable / closable, and the entrance / exit is opened / closed by opening / closing the cover.
- the roof structure according to the present invention is based on the driving means for driving the opening and closing of the cover, the information acquisition means for acquiring the takeoff and landing information of the drone, and the takeoff and landing information acquired by the information acquisition means. It is characterized by including a control means for controlling the drive means to open and close the cover.
- the roof structure according to the present invention is characterized in that the drone port includes a non-contact charging means capable of charging the drone while the drone is landing on the drone port.
- the roof structure according to the present invention is characterized in that the outer surface of the cover is provided with a solar cell, and the non-contact charging means charges the drone using the electric power generated by the solar cell.
- the second roof structure according to the present invention has a size capable of accommodating a sloping roof covering the upper part of the building and a drone provided by cutting out a part of the sloping roof so that the bottom surface is substantially horizontal.
- the cover is fixed to the bottom surface of the drone accommodating portion, and the bottom surface of the drone accommodating portion protrudes to the outside of the inclined roof. It is configured to be movable between the above and the state where the roof is housed inside the inclined roof, and the doorway is opened and closed by the movement of the bottom surface.
- the roof structure according to the present invention has a sloping roof covering the upper part of the building and a drone accommodating portion having a size capable of accommodating a drone provided by cutting out a part of the sloping roof so that the bottom surface is substantially horizontal.
- a drone port provided on the bottom surface of the drone accommodating portion for the drone to take off and land, a cover covering the opening formed in the inclined roof for the drone accommodating portion, and the drone accommodating portion are provided.
- the door is provided with an entrance and exit through which the drone can enter and exit, and the cover is configured to be openable and closable.
- the doorway is opened and closed by opening and closing the cover, and the drone is accommodated by cutting out a part of a sloping roof.
- the drone port can be provided so that the drone can take off and land stably even on a sloping roof. it can.
- a cover is provided for the drone housing to cover the opening formed in the sloping roof, and the cover can be opened and closed, and the drone provided in the drone housing can be accessed by opening and closing the cover. Since the doorway opens and closes, by opening the cover and opening the doorway of the drone housing, the drone can take off and land at the drone port provided on the bottom of the drone housing through the doorway. ..
- the drone housing is large enough to accommodate the drone, and with the drone landing at the drone port, the cover can be closed to close the doorway of the drone housing, so wind, rain, snow, etc. You can protect your drone from the effects of the weather.
- the roof structure according to the present invention is based on the driving means for driving the opening and closing of the cover, the information acquisition means for acquiring the takeoff and landing information of the drone, and the takeoff and landing information acquired by the information acquisition means. It is characterized by including a control means for controlling the drive means to open and close the cover, and the drive means is driven by the control means based on the takeoff and landing information of the drone acquired by the information acquisition means, and the drone is externally provided. Close the cover when flying or when the drone is landing on the drone port, and control the cover to open to open the doorway of the drone containment only when the drone takes off and landing at the drone port. Can be done.
- the drone capable of autonomous flight starts from the drone port of the roof structure according to the present invention, and after flying, returns to the drone port of the roof structure according to the present invention, and the drone capable of autonomous flight arrives and departs.
- the cover is automatically opened when the drone takes off and landing from the drone port without manually operating the cover, and is automatically opened at other times. Since the cover can be closed, even when the drone is flying autonomously 24 hours a day, 365 days a year, the drone landing inside the drone housing or at the drone port can be exposed to wind, rain, snow, etc. Can be protected from the effects.
- the roof structure according to the present invention is characterized in that the drone port includes a non-contact charging means capable of charging the drone while the drone is landing on the drone port.
- the drone port includes a non-contact charging means capable of charging the drone while the drone is landing on the drone port.
- the drone can be charged without connecting a charging cable or the like. Therefore, when the drone port with the roof structure according to the present invention is used as the base point for the arrival and departure of the drone capable of autonomous flight, when the drone returns to the drone port with the roof structure according to the present invention and lands. Since the drone can be automatically charged without manual operation for charging, it is possible to enable autonomous flight of the drone 24 hours a day, 365 days a year.
- the roof structure according to the present invention is characterized in that the outer surface of the cover is provided with a solar cell, and the non-contact charging means charges the drone using the electric power generated by the solar cell. , Can save power for charging the drone.
- the second roof structure according to the present invention has a size capable of accommodating a sloping roof covering the upper part of the building and a drone provided by cutting out a part of the sloping roof so that the bottom surface is substantially horizontal.
- the drone accommodating part is provided and the bottom surface of the drone accommodating part is substantially horizontal and the drone port is provided on the bottom surface, the drone port is provided so that the drone can take off and land stably even on a sloping roof. be able to.
- a cover is provided for the drone housing to cover the opening formed in the sloping roof, the cover is fixed to the bottom of the drone housing, and the bottom of the drone housing is outside the sloping roof.
- the drone housing is large enough to accommodate the drone, and with the drone landing on the drone port, you can move the bottom so that it fits inside the sloping roof and close the entrance and exit of the drone housing. Because it can, the drone can be protected from the influence of the weather such as wind, rain and snow.
- FIG. 1A A partial cross-sectional front view showing a state in which the cover is opened in the roof structure of FIG. 1A, and is a view taken along the line XX of FIG. 1A.
- FIG. 2 is a view showing a state in the middle of opening and closing the cover in a partial cross-sectional front view of FIG. 2A.
- FIG. 2 is a view showing a state in which the cover is closed in a partial cross-sectional front view of FIG. 2A.
- FIG. 3A is a cross-sectional side view showing a state in which the cover is closed in the roof structure of FIG. 3A.
- FIG. 4A shows an example of the roof structure which concerns on 2nd Embodiment of this invention, and is the figure which shows the state which the doorway is closed.
- the figure which shows the state which the doorway is open in the perspective view of FIG. 4A.
- It is a partial cross-sectional front view which shows the state which the doorway is closed in the roof structure of FIG. 4A, and is the YY arrow view of FIG. 4A.
- the inclined roof 2 covering the upper part of the building and a part of the inclined roof 2 are cut out so that the bottom surface 31 is substantially horizontal.
- a drone accommodating portion 3 having a size capable of accommodating the drone D provided in the above, a drone port 4 provided on the bottom surface 31 of the drone accommodating portion 3 capable of taking off and landing, and a sloped roof 2 for the drone accommodating portion 3.
- a cover 5 covering the formed opening 35 and an entrance / exit 36 provided in the drone accommodating portion 3 through which the drone D can enter / exit are provided, and the cover 5 is configured to be openable / closable. It is designed to do.
- the drone accommodating portion 3 is provided so as to cut out a part of the inclined roof 2 covering the upper part of the building, and the bottom surface 31 of the drone accommodating portion 3 is substantially horizontal. Since the drone port 4 is provided on the bottom surface 31, the drone port 4 can be provided so that the drone D can take off and land stably even in a building having a sloping roof 2 instead of a horizontal flat roof.
- the drone port 4 is provided on the roof, people do not usually enter or place objects near the drone port 4, so the drone port can be used in lowlands such as gardens or balconies. Compared to the case where it is installed in a place where people can enter, when the drone D takes off and landing at the drone port 4, it may hit a person or an object and injure the person, or the drone D or the object may be damaged. The risk can be reduced, and the risk of the drone port 4 and the drone D being mischievous or stolen can also be reduced.
- the drone accommodating portion 3 has a size capable of accommodating the drone D, and a cover 5 covering the opening 35 formed in the inclined roof 2 for the drone accommodating portion 3 is provided so as to be openable and closable.
- a cover 5 covering the opening 35 formed in the inclined roof 2 for the drone accommodating portion 3 is provided so as to be openable and closable.
- the doorway 36 where the drone D provided in the drone housing 3 can enter and exit is opened and closed, so that the drone D lands on the drone port 4 provided on the bottom 31 of the drone housing 3.
- the cover 5 By closing the cover 5 while the cover 5 is closed, the doorway 36 of the drone housing 3 is closed while the drone D is housed in the drone housing 3, and the drone D is protected from the influence of weather such as wind, rain, and snow. can do.
- the sloping roof 2 is a sloping roof that covers the upper part of the building.
- the sloping roof 2 has a linear ridge 21 extending substantially horizontally and a ridge 21 at the top thereof, and the sloping roof 2 is inclined diagonally downward from the ridge 21 to both sides.
- An example is shown in the case of a so-called gable roof, which is substantially mountain-shaped by the two roof surfaces 22 and 23.
- An attic space 24 is provided between the ceiling of the room of the building and the sloping roof 2.
- the drone accommodating portion 3 is provided so as to cut out a part of the inclined roof 2, and the bottom surface 31 of the drone accommodating portion 3 is substantially horizontal.
- the sloping roof 2 is a gable roof, and as shown in FIG. 1A, the drone accommodating portion 3 is provided so as to partially cut out a portion of the ridge 21 extending substantially horizontally of the sloping roof 2.
- the bottom surface 31 of the drone accommodating portion 3 is located below the ridge 21 and is formed in a substantially rectangular plane shape. It is provided so as to be parallel or substantially vertical.
- the drone accommodating portion 3 is provided so that the inclined roof 2 is cut out substantially vertically downward toward the bottom surface 31 to the size of the bottom surface 31.
- the opening 35 is a substantially chevron-shaped opening similar to the shape of the inclined roof 2 formed on the roof surface 22 and the roof surface 23 of the inclined roof 2 by providing the drone accommodating portion 3.
- the space from the opening 35 to the bottom surface 31 located substantially vertically below the opening 35 is the drone accommodating portion 3.
- the underside of the sloping roof 2 is an attic space 24, and the bottom surface 31 is located at a position equal to or higher than the ceiling height position of the room under the attic space 24 so that the drone housing portion 3 fits in the attic space 24. It is preferable to be provided.
- the side wall 32 is provided on each of the four surfaces extending substantially vertically upward from the four sides of the bottom surface 31 which is the side surface of the drone accommodating portion 3 to the opening 35, so that the drone accommodating portion 3 and the attic space 24 are provided on the side wall 32. It may be partitioned by.
- the bottom surface 31 extends from the roof surface 22 to the roof surface 23 in a direction substantially perpendicular to the longitudinal direction of the ridge 21, and is the longitudinal length of the opposite ridge 21 of the bottom surface 31.
- the sides substantially parallel to the direction coincide with the sides substantially parallel to the longitudinal direction of the opposite ridge 21 of the opening 35, respectively, and are located on the surfaces of the roof surface 22 and the roof surface 23.
- the drone port 4 is provided on the bottom surface 31 of the drone accommodating portion 3.
- the drone port 4 is a circular flat plate-shaped member having a size that allows the drone D to take off and land on the drone port 4, and is on the bottom surface 31. Will be installed.
- the drone accommodating portion 3 is formed so that the drone D fits inside the drone accommodating portion 3 with the drone D landing on the drone port 4. Since the bottom surface 31 is a substantially horizontal flat surface, the drone port 4 can be stably installed on the bottom surface 31.
- the drone port 4 may be provided with the non-contact charging means 41.
- the non-contact charging means 41 performs non-contact power transmission to the secondary battery for driving the drone D included in the drone D without connecting an electric wire for power supply and without using a metal contact, a connector, or the like.
- the drone D can be charged while the drone D has landed on the drone port 4.
- the non-contact power transmission method of the non-contact charging means 41 includes an electromagnetic induction method using an induced electromotive force generated in a coil on the power receiving side due to a magnetic flux generated by a current flowing through the coil on the power transmitting side, and an electromagnetic induction method using the coil on the power transmitting side and Like a magnetic field resonance method that utilizes the fact that an LC resonance circuit is formed by a coil and a capacitor whose resonance frequencies are matched on the receiving side, and the magnetic field generated by the current flowing through the coil on the transmitting side is transmitted to the coil on the receiving side by resonance.
- a magnetic field coupling method that uses the energy of the magnetic field as a medium for power transmission an electric field coupling method that uses the energy of the electric current generated when the electrodes installed on the transmitting side and the power receiving side are brought close to each other for power transmission, etc.
- the non-contact charging means 41 provided in the drone port 4 a device on the transmission side suitable for the non-contact power transmission method supported by the drone D may be appropriately used.
- the power source of the non-contact charging means 41 a power source drawn into the building from the electric power company may be used.
- the drone accommodating portion 3 is surrounded by the attic space 24, so that the power cable of the non-contact charging means 41 of the drone port 4 is passed through the attic space 24.
- the power outlet of the attic space 24 can be easily wired without any special wiring work.
- the drone port 4 has a circular flat plate shape, but another rectangular flat plate shape or the like may be used, and any shape may be used as long as the drone D can take off and land.
- the drone port 4 is configured to be installed on the bottom surface 31 as a separate member from the bottom surface 31 of the drone accommodating portion 3, but the drone port 4 and the bottom surface 31 are integrated. It may be configured as a member. In that case, the drone port 4 and the bottom surface 31 can be flushed without a step, there is no concern that the foot of the drone D will slip off the drone port 4, and the installation work of the drone port 4 can be performed on site with the building materials integrated. It can be omitted, and the management cost can be omitted by reducing the number of members.
- the drone port 4 and the bottom surface 31 are configured as separate members, they can be easily replaced when the drone port 4 is to be replaced, or the drone port 4 is provided so as to be movable with respect to the bottom surface 31. Since there are also advantages such as being able to do so, it may be appropriately selected whether to use separate members or to integrate them.
- the cover 5 covers the opening 35 formed in the sloping roof 2 for the drone accommodating portion 3.
- the opening 35 is a substantially chevron-shaped opening having a shape similar to the shape of the inclined roof 2 formed on the roof surface 22 and the roof surface 23 of the inclined roof 2, and is shown in FIG. 1B.
- the cover 5 is formed in a substantially chevron shape to match the shape of the opening 35.
- the cover 5 is configured to be openable and closable, and the doorway 36 provided in the drone accommodating portion 3 for entering and exiting the drone D is opened and closed by opening and closing the cover 5.
- the doorway 36 is opened and closed.
- a part or all of the opening 35, and the cover 5 is configured so that a part or all of the opening 35 can be opened and closed, and when the cover 5 is in an open state, the open part of the opening 35 is open.
- the opening 35 is closed.
- the doorway 36 may have a size that allows the drone D to enter and exit the drone accommodating portion 3 through the doorway 36. Therefore, if the opening 35 is larger than the size that the drone D enters and exits, the cover 5 is opened. Only a part of the doorways 36 of 35 may be opened.
- the cover 5 is provided so that the entire cover 5 opens and closes by sliding the outside of the inclined roof 2 along the longitudinal direction of the ridge 21.
- the cover 5 is fitted into the opening 35 so that the cover 5 is substantially flush with the roof surface 22 and the roof surface 23 around the opening 35.
- the cover 5 is formed in a shape similar to the shape of the inclined roof 2, and when the cover 5 is closed, the cover 5 is substantially flush with the surrounding roof surface 22 and the roof surface 23. Therefore, if the cover 5 is closed while the drone D is landing on the drone port 4, the cover 5 is substantially integrated with the inclined roof 2 and does not impair the design of the exterior of the building. Further, even in a strong wind such as a typhoon, when the cover 5 is closed, the cover 5 becomes substantially flush with the surrounding roof surface 22 and the roof surface 23, and it is difficult for an extra force to be applied to the cover 5. Hard to break.
- the solar cell 7 may be provided on the surface of the cover 5.
- the solar cell 7 is a flat panel-shaped device that converts sunlight shining on the solar cell 7 into electricity.
- the cover 5 since the cover 5 is designed to open and close by sliding the outside of the inclined roof 2, the solar cell 7 does not interfere with the opening and closing of the cover 5, and the solar cells of various thicknesses do not interfere with the opening and closing of the cover 5. 7 can be used.
- the solar cell 7 and the non-contact charging means 41 of the drone port 4 may be connected by an electric wire, and the electricity generated by the solar cell 7 may be used for charging the drone D by the non-contact charging means 41. By doing so, the power for charging the drone D can be saved.
- a storage battery for storing the electricity generated by the solar cell 7 may be provided.
- the electricity generated by the solar cell 7 is stored in the storage battery. Therefore, the electric power stored in the storage battery can be used for charging the drone D in a cloudy weather or the like, and the electric power can be utilized without waste.
- the roof structure 1 is based on the drive means 51 for driving the opening and closing of the cover 5, the information acquisition means 52 for acquiring the takeoff and landing information of the drone D, and the takeoff and landing information of the drone D acquired by the information acquisition means 52.
- the cover 5 is provided with a control means 53 that controls the drive means 51 to open and close the cover 5, and the cover 5 is configured to automatically open and close according to the takeoff and landing of the drone D to the drone port 4.
- a first rail 61 is provided on the back side of the top portion of the substantially chevron-shaped cover 5 along the direction in which the top portion extends.
- a bar 63 having a first carriage 62 that moves in the first rail 61 along one rail 61 at its tip is drone so that the bar 63 can rotate in the vertical direction about the base end of the bar 63.
- the building 21 of the accommodating portion 3 is attached to one upper portion of a side surface perpendicular to the extending direction.
- the bar 63 is rotatable from a substantially vertical state in which the first carriage 62 at the tip is located at the upper portion in a direction in which the tip falls inward of the drone accommodating portion 3 around the base end.
- the first carriage 62 When the 63 is in a substantially vertical state, the first carriage 62 is positioned higher than the building 21.
- the first carriage 62 is movable along the first rail 61 by the first wire 64 and the second wire 65.
- One end of the first wire 64 is fixed to one end side of the first rail 61, is wound around a pulley included in the first carriage 62 at an intermediate portion, and the other end is connected to the drive means 51.
- One end of the second wire 65 is fixed to the other end side of the first rail 61, is wound around a pulley included in the first carriage 62 at an intermediate portion, and the other end is connected to the drive means 51.
- the drive means 51 can apply tension to the first wire 64 and the second wire 65 to wind or unwind the first wire 64 and the second wire 65.
- an electric motor is used as the driving means 51.
- the driving means 51 is also configured to drive the rotation of the bar 63.
- a shaft that is rotated by driving a drive means 51 that is an electric motor, a first gear that is fixed to the tip of the shaft, and a bar 63 that is attached to the base end of the bar 63 and meshes with the first gear.
- the drive means 51 may be configured to drive the rotation of the bar 63 by a second gear that is rotated by the rotation of the first gear in a direction that rotates in the vertical direction.
- the second wire 65 is fixed to the side and one end of the second wire 65 is fixed to the other end side of the first rail via the pulley of the first carriage 62, one end side of the first rail 61 and the first carriage 62.
- Tension is applied to the first wire 64 and the second wire 65 in a direction in which the distance between the first rail 61 and the other end side of the first rail 61 becomes longer and the distance between the first rail 61 and the first carriage 62 becomes longer.
- the first carriage 62 is in a stationary state with respect to the drone accommodating portion 3, but the first carriage 62 can move in the first rail 61, and the first rail 61 is on the cover 5.
- the tension applied to the first wire 64 and the second wire 65 causes the first rail 61 side to move with respect to the first carriage 62 that is stationary with respect to the drone accommodating portion 3.
- the cover 5 moves on the inclined roof 2 along the direction in which the ridge 21 extends.
- the drive means 51 winds up the first wire 64 to wind out the second wire 65
- the cover 5 opens the doorway 36 so that one end side of the first rail 61 approaches the first carriage 62. Move to.
- the first wire 64 is unwound and the second wire 65 is wound by the driving means 51, the other end side of the first rail 61 is the first carriage as shown by the arrow in FIG. 2A.
- the cover 5 moves in the direction of closing the doorway 36 so as to approach 62.
- a second carriage 68 is provided.
- the second carriage 68 is attached to one end side of the lower first rail 61 on the back side of the two inclined surfaces having a substantially chevron shape of the cover 5, and the second rail 67 is the position of the second carriage 68.
- the ridge 21 of the bottom surface 31 is attached to each end along the extending direction.
- the bar 63 is moved downward from the state where the bar 63 is substantially vertical and the first carriage 62 at the tip is higher than the ridge 21 due to the vertical rotation of the bar 63 driven by the driving means 51. Since the first carriage 62 moves to a state where the first carriage 62 is inside the drone accommodating portion 3, as shown in FIG. 2A, the cover 5 is moved along the direction in which the ridge 21 extends. After moving horizontally in parallel in the closing direction on the sloping roof 2, as shown in FIGS. 2B and 2C, by rotating the bar 63 downward, the cover 5 is lowered by the amount that the first carriage 62 is lowered.
- the cover 5 is closed so that the cover 5 fits into the opening 35 so that the cover 5 and the inclined roof 2 around the opening 35 are substantially flush with each other.
- the bar 63 is rotated upward to lift the cover 5 onto the inclined roof 2, and then the cover 5 is horizontally translated by the first wire 64 and the second wire 65.
- the second rail 67 is on the side opposite to the one side to which the bar 63 is attached on the side surface perpendicular to the direction in which the ridge 21 of the drone accommodating portion 3 extends so as to follow the movement of the cover 5.
- the rail is a path that rises from the bottom surface 31 near the other side surface facing each other by the amount of upward rotation of the bar 63, and then extends horizontally toward one side surface to which the bar 63 is mounted horizontally. ing.
- the cover 5 may be opened and closed by driving the drive means 51, and as an opening / closing mechanism of the cover 5, a slide door opening / closing mechanism used for the rear door of a car, a plug door used in a train, a bus, or the like. An opening / closing mechanism or the like may be used. Further, instead of an opening / closing mechanism for opening and closing the cover 5 so as to slide the outside of the inclined roof 2, a door pocket into which the cover 5 can be inserted is provided on the roof surface 22 and the roof of the inclined roof 2 next to the drone accommodating portion 3.
- an opening / closing mechanism such as a sliding door that opens / closes the cover 5 by moving the cover 5 in and out of the door pocket, or a shaft is passed through the top of the cover 5 and this shaft is used as a fulcrum. , One or both of the two inclined surfaces of the cover 5 are rotated to open and close the cover 5, or vice versa.
- a butterfly open opening / closing mechanism may be used such that the cover 5 is opened from the top of the cover 5 with the shaft as a fulcrum.
- the information acquisition means 52 and the control means 53 are configured as functions of a computer 9 including a CPU, a memory, an input / output device, and a bus that connects them so as to be able to send and receive signals to each other.
- the computer 9 performs various information processing and control by executing various programs stored in the storage device connected to the memory or the input / output device by the CPU.
- the computer 9 outputs information in the computer 9 such as a storage device that can store various programs and data such as a hard disk, an input device such as a keyboard and a mouse for a person to input information to the computer 9, and a display.
- the computer 9 can control various devices connected to the input / output device based on various programs.
- the device connected to the input / output device of the computer 9 may be secondarily connected to the computer 9 wirelessly via a communication device that can communicate wirelessly connected to the input / output device. It suffices if it is connected to the computer 9 so as to be able to send and receive signals.
- the computer 9 includes programs for executing the functions of the information acquisition means 52 and the control means 53, and by executing these programs, the computer 9 functions as the information acquisition means 52 and the control means 53. It has become.
- the information acquisition means 52 acquires the takeoff and landing information of the drone D.
- the takeoff and landing information of the drone D acquired by the information acquisition means 52 is information used by the control means 53 to open and close the cover 5.
- the control means 53 controls the opening and closing of the cover 5 so that the cover 5 is opened only when the takeoff and landing operation is performed, and is closed at other times.
- the takeoff / landing information of the drone D acquired by the information acquisition means 52 opens the cover 5 when the drone D flying outside the drone accommodating unit 3 starts the landing operation to the drone port 4.
- the takeoff and landing information of the drone D may further include identification information for identifying the drone D, the information acquisition means 52 acquires the identification information, and the control means 53 uses the identification information to use the drone D. If the opening and closing of the cover 5 is controlled after the identification, the cover 5 will not be opened and closed when another unintended drone different from the drone D approaches.
- the approach and separation sensor 54 that detects the approach and separation of the drone D to the cover 5 and the drone port 4 detect the contact of the drone D with the drone port 4.
- a contact sensor 55 is provided, the approach / separation sensor 54 and the contact sensor 55 are connected to an input / output device of the computer 9, and the information acquisition means 52 is input from the approach / separation sensor 54 and the contact sensor 55 input to the computer 9.
- the detection signal of the drone D is acquired as takeoff and landing information of the drone D.
- the approach separation sensor 54 is a sensor for detecting the approach and separation of the drone D, and is, for example, a Doppler sensor using a microwave transmission signal transmitted from the sensor and a reflection signal reflected by a reflecting object.
- the approach / separation sensor 54 is attached to the cover 5 or the inclined roof 2 in the vicinity of the cover 5 so that the drone D can detect the approach / separation to the cover 5.
- the contact sensor 55 is a sensor for detecting whether the drone D is in contact with the drone port 4 and is in a landing state, or whether the drone D is not in contact with the drone port 4 and the drone D is in a flying state. It has become.
- the control means 53 controls the drive means 51 to open and close the cover 5 based on the takeoff and landing information of the drone D acquired by the information acquisition means 52.
- the drive means 51 is connected to an input / output device of the computer 9, and the control means 53 controls the drive means 51 when the takeoff and landing information of the drone D is input from the information acquisition means 52.
- a signal is generated and output to the driving means 51.
- the drive means 51 is driven by a control signal from the control means 53 to open and close the cover 5.
- the approach separation sensor 54 notifies that the drone D is approaching. Is input to the computer 9.
- the information acquisition means 52 receives the detection signal of the approach of the drone D by the approach / separation sensor 54
- the information acquisition means 52 outputs the landing / opening information for opening the cover 5 to the control means 53 as takeoff / landing information.
- the control means 53 receives the landing opening information from the information acquisition means 52
- the control means 53 controls the drive means 51 to open the cover 5 and open the doorway 36 of the drone D.
- a detection signal indicating that the drone D is in contact with the drone port 4 is sent by the contact sensor 55 provided in the drone port 4. It is input to the computer 9.
- the information acquisition means 52 receives the detection signal of the contact of the drone D with the drone port 4 by the contact sensor 55, the information acquisition means 52 outputs the landing closing information for closing the cover 5 to the control means 53 as takeoff and landing information.
- the control means 53 drives the drive means 51 to close the cover 5.
- the contact sensor 55 inputs a detection signal to the computer 9 informing that the drone D is no longer in contact with the drone port 4 or the contact state has changed.
- the information acquisition means 52 receives a detection signal from the contact sensor 55 to notify that the drone D is no longer in contact with the drone port 4 or the contact state has changed, the information acquisition means 52 opens the cover 5 as takeoff / landing information.
- the takeoff opening information is output to the control means 53.
- the control means 53 drives the drive means 51 to open the cover 5.
- the approach / separation sensor 54 inputs a detection signal to the computer 9 informing that the drone D is moving away from the cover 5.
- the information acquisition means 52 receives the detection signal of the departure of the drone D by the approach separation sensor 54
- the information acquisition means 52 outputs the takeoff closing information for closing the cover 5 to the control means 53 as takeoff / landing information.
- the control means 53 drives the drive means 51 to close the cover 5.
- the approach / separation sensor 54 and the contact sensor 55 are provided so that the information acquisition means 52 acquires the takeoff / landing information of the drone D based on the detection signals from the approach / separation sensor 54 and the contact sensor 55.
- the information acquisition means 52 receives a time measuring signal from the time measuring means according to the time when the drone D takes off and landing at the drone port 4. It may be used as the takeoff and landing information of the drone D acquired in.
- the computer and the computer 9 are communicably connected by, for example, via the Internet, and the drone D is connected.
- the command signal for the drone D to take off and land at the drone port 4 may be acquired by the information acquisition means 52 and used for opening and closing the cover 5 as the takeoff and landing information of the drone D.
- a sensor for detecting wind, rain, snow, etc. is provided on the cover 5 or near the cover 5, and when the wind speed, rain, snow, etc. above a certain level that affects the flight of the drone D is detected, the wind, etc.
- the information acquisition means 52 uses the detection signal of the sensor that detects rain, snow, etc.
- the computer 9 is connected to the Internet, the weather forecast information is acquired from the Internet, and the weather forecast information is obtained by the drone D of the information acquisition means 52. In addition to being used as takeoff and landing information, the takeoff and landing information may be transmitted to a computer that controls the drone D so that the drone D can take off and land at the drone port 4.
- the cover 5 is configured to open and close automatically, and when the drone D takes off and landing on the drone port 4, the cover 5 is opened and the drone D lands on the drone port 4. Since the cover 5 is closed when the drone D is not in the drone housing 3 and when the drone D is in the drone port 4, it is landing on the drone port 4 due to the influence of the weather such as wind, rain, and snow.
- the inside of the drone accommodating portion 3 including the drone D can be protected.
- the drone port 4 can be provided with the non-contact charging means 41 capable of charging the drone D when the drone D is landing, and in that case, the drone D is provided by the non-contact charging means 41.
- the roof structure 1 is a system that automatically patrols and monitors the surroundings of the building having the roof structure 1 by the drone D, and a system that automatically and periodically inspects the building having the roof structure 1 by the drone D. It is preferably used as a drone port for resident a drone D that automatically operates by autonomous flight, as used in the above.
- patrol monitoring is performed by autonomous flight, and then the drone D is returned to the drone port 4 again.
- the drone D hits people and things when taking off and landing at the drone port 4.
- the drone D can be safely taken off and landed at the drone port 4 without any risk of such a problem.
- the cover 5 automatically opens and closes and the drone D can automatically charge the drone D by the non-contact charging means 41 just by landing on the drone port 4, the cover 5 can be opened and closed, the drone D can be charged, and the like. It enables autonomous flight of Drone D 24 hours a day, 365 days a year without the need for human operation.
- the cover 5 when the cover 5 is closed, the cover 5 is substantially flush with the roof surface 22 and the roof surface 23 and is substantially integrated with the inclined roof 2. Therefore, the drone port 4 can be provided on the sloping roof 2 without significantly impairing the design of the appearance of the sloping roof 2, and the wind that hits the cover 5 can be applied to the surrounding sloping roof 2 even during a strong wind such as a typhoon. It is possible to reduce the risk of the cover 5 being parried and being damaged due to a large force being applied to the cover 5.
- the drone port 4 may be provided with a locking means for locking the drone D and fixing it to the drone port 4 when the drone D lands.
- the locking means can switch between a locked state in which the drone D is fixed to the drone port 4 and an unlocked state in which the drone D is released from the fixed state of the drone port 4, and can be used for takeoff and landing of the drone D to the drone port 4. At the same time, it is configured to automatically control the switching between the locked state and the unlocked state.
- the locking means for example, when the drone D is provided with a foot so that the foot touches the ground at the time of landing, the foot may be fixed. If the foot of the drone D is, for example, a foot consisting of four vertical parts extending downward from the main body of the drone D and two horizontal parts extending between the lower ends of the two vertical parts, the lock is used.
- a hook-shaped member that can be engaged with each horizontal portion is provided in the drone port 4 so as to be rotatable on a vertical surface, so that the hook-shaped member is engaged with the horizontal portion. The state and the unlocked state released from the engagement can be switched by rotating the hook-shaped member.
- the legs of the drone D are composed of a plurality of vertical portions extending downward from the main body of the drone D and a flange portion provided at the lower end of each vertical portion and larger than the thickness diameter of each vertical portion.
- a plate member having a groove portion that is cut out to a diameter larger than the diameter of the vertical portion and smaller than the size of the flange portion and can be engaged with the vertical portion can be rotated on a horizontal plane.
- the locking means may be appropriately configured according to the shape of the drone D and the like, and may lock the main body of the drone D instead of the legs of the drone D, or the drone D may be locked in the drone port 4. Anything can be used as long as it can be fixed to the lock state and can be switched between the locked state and the unlocked state.
- a driving means for driving the switching of the locking means is provided, and for example, the contact sensor 55 that detects the contact state of the drone D with respect to the drone port 4 Using the detection signal, when the drone D comes into contact with the drone port 4, the locking means is switched to the locked state, the locked state is maintained during the contact, and when the contact of the drone D from the drone port 4 disappears, the locking means is switched.
- the drive means for switching the locking means may be controlled so as to switch to the unlocked state and maintain the unlocked state while there is no contact.
- the drone accommodating portion 3 is provided so as to partially cut out a portion of the ridge 21 extending substantially horizontally of the inclined roof 2, and the roof surface 22 and the roof surface 23 are provided so as to be cut out.
- the drone accommodating portion 3 may be provided so as to cut out either the roof surface 22 or the roof surface 23.
- FIGS. 3A and 3B show a state in which the opening 35 is formed only on the roof surface 22 and the drone accommodating portion 3 is provided.
- the cover 5 covering the opening 35 may have a substantially rectangular flat plate shape so as to be substantially flush with the roof surface 22 when the cover 5 is closed.
- the drone accommodating portion 3 may be provided so that the inclined roof 2 is cut out downward from the opening 35 so that the bottom surface 31 is provided downward at a distance from the opening 35, and FIG. 3A may be provided.
- the inclined roof 2 may be provided so as to be cut out in the lateral direction from the opening 35.
- a substantially horizontal bottom surface 31 extends from the lower end side of the opening 35 toward the inside of the inclined roof 2, and the drone port 4 is provided for the length of the bottom surface 31 extending. It suffices if the cover 5 can be closed with the drone D landing on the drone port 4 with a sufficient size.
- the method of providing the drone accommodating portion 3 inside from the opening 35 may be appropriately determined according to the slope of the roof surface 22.
- the roof structure 1 can be applied even in the case where the sloping roof 2 is a one-way roof composed of a roof surface having one slope.
- the drone accommodating portion 3 is provided so as to cut out the inclined roof 2 from the opening 35 in the lateral direction, and the opening 35, that is, the entrance / exit 36 is the drone accommodating portion. If it is not located vertically above the drone port 4 provided on the bottom surface 31 of the 3, when the drone D takes off and landing at the drone port 4, it is not vertically up and down but diagonally to the doorway 36.
- the drone port 4 may be provided so as to be movable so that the drone D can take off and land at the drone port 4 vertically and vertically. For example, in the drone accommodating portion 3 of FIGS.
- the drone port 4 can be moved in the horizontal direction. After the cover 5 is opened, move to a position where the inclined roof 22 etc. does not hang vertically above the range required for takeoff and landing of the drone D of the drone port 4 so that the drone port 4 protrudes outward. Then, the drone D may take off and land, and after the takeoff and landing is completed, the drone port 4 may be moved inward so as to be housed inside the drone accommodating portion 3, and the cover 5 may be closed.
- the moving mechanism of the drone port 4 may be configured by using, for example, a rack and pinion, a linear motion cylinder, or the like so that a rail is provided on the bottom surface 31 and the drone port 4 moves along the rail.
- the roof structure 1a according to the second embodiment will be described with reference to FIGS. 4A to 5B.
- the roof structure 1a according to the present embodiment shows an example in the case of the same inclined roof 2 as the roof structure 1 shown in FIGS. 1A to 2C, and the same ones are the same. It is indicated by a symbol.
- the roof structure 1 shown in FIGS. 4A to 5B shows an example in the case of the same inclined roof 2 as the roof structure 1 shown in FIGS. 1A to 2C, and the same ones are the same. It is indicated by a symbol.
- the cover 5 covering the opening 35 provided in the inclined roof 2 is configured to be openable and closable, and when the cover 5 is opened and closed, a part of the opening 35 or a part of the opening 35 or The doorway 36 through which the entire drone D can enter and exit was opened and closed, but in the roof structure 1a according to the present embodiment, the cover 5 covering the opening 35 provided in the inclined roof 2 can be opened and closed. It is not configured and is fixed to the bottom surface 31. Then, instead of the driving means 51 provided for driving the opening and closing of the cover 5 in the roof structure 1, in the roof structure 1a, a driving means 51a for moving the bottom surface 31 in the vertical direction is provided below the bottom surface 31. There is.
- the drive means 51a for example, an electric cylinder, a hydraulic cylinder, an electric jack, or the like can be used.
- the bottom surface 31 and the cover 5 fixed to the bottom surface 31 are integrally moved upward.
- the cover 5 has a substantially chevron shape that matches the shape of the opening 35, and the lower sides of the two inclined surfaces of the cover 5 are fixed to the inclined surface 22 and the inclined surface 23 side of the substantially rectangular bottom surface 31, respectively.
- the end of the drone accommodating portion 3a formed by the bottom surface 31 and the cover 5 in the direction in which the ridge 21 extends is a substantially triangular opening due to the two inclined surfaces of the cover 5 and the bottom surface 31.
- this opening serves as an entrance / exit 36a through which the drone D enters / exits.
- the entrance / exit 36a is formed at a place different from the opening 35, and the drone accommodating portion 3a is substantially integrated with the inclined roof 2.
- the doorway 36a is closed and closed. From there, when the drone accommodating portion 3a is moved so as to protrude to the outside of the inclined roof 2 by the driving means 51a, the entrance 36a is exposed and opened, and the drone D is drone of the drone accommodating portion 3a via the entrance 36a. It is possible to take off and land at port 4.
- the doorway 36a is opened and closed by moving the bottom surface 31 in the vertical direction by the driving means 51a.
- the inclined roof 2 A drone accommodating portion 3a is provided so as to cut out the roof surface 22 in the horizontal direction, and the bottom surface 31 extends from the lower side of the opening 35 of the roof surface 22 to the inside of the inclined roof 2 and has an opening in the bottom surface 31.
- the drone accommodating portion 3a including the bottom surface 31 and the cover 5 is moved horizontally by the driving means 51a so that the drone accommodating portion 3a protrudes from the roof surface 22.
- the doorway 36a may be opened.
- the direction in which the drone accommodating portion 3a is moved by the driving means 51a is the vertical direction or the horizontal direction
- the amount of movement of the drone accommodating portion 3a due to the opening and closing of the entrance / exit 36a is reduced according to the gradient of the roof surface 22. It may be decided as appropriate.
- the moving direction of the drone accommodating portion 3a is not limited to the vertical direction and the horizontal direction, but may be, for example, an oblique direction, and any doorway 36a through which the drone D can enter and exit the drone accommodating portion 3a may be opened and closed.
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Abstract
Description
本実施形態に係る屋根構造1は、図1Aから図2Cに示すように、建物の上部を覆う傾斜屋根2と、底面31が略水平になるように傾斜屋根2の一部を切り欠くようにして設けられるドローンDを収容可能な大きさのドローン収容部3と、ドローン収容部3の底面31に設けられるドローンDが離着陸可能なドローンポート4と、ドローン収容部3のために傾斜屋根2に形成された開口部35を覆うカバー5と、ドローン収容部3に設けられるドローンDが出入り可能な出入口36と、を備え、カバー5が開閉可能に構成され、カバー5の開閉によって出入口36が開閉するようになっている。
次に、第2の実施形態に係る屋根構造1aについて図4Aから図5Bを参照しつつ説明する。本実施形態に係る屋根構造1aは、図4Aから図5Bに示すように、図1Aから図2Cに示した屋根構造1と同様の傾斜屋根2の場合の例を示しており、同じものは同じ符号で示している。図1Aから図2Cに示す屋根構造1では、傾斜屋根2に設けられた開口部35を覆うカバー5を開閉可能に構成しており、カバー5が開閉することによって、開口部35の一部または全部であるドローンDが出入り可能な出入口36が開閉するようになっていたが、本実施形態に係る屋根構造1aでは、傾斜屋根2に設けられた開口部35を覆うカバー5は、開閉可能に構成されておらず、底面31に固定されるようになっている。そして、屋根構造1でカバー5の開閉を駆動するために設けていた駆動手段51の代わりに、屋根構造1aでは、底面31の下部に底面31を上下方向に移動させる駆動手段51aが設けられている。駆動手段51aには、例えば、電動シリンダ、油圧シリンダ、電動ジャッキ等を用いることができる。図4B及び図5Bに示すように、駆動手段51aによって底面31を上方に移動させることで、底面31と底面31に固定されたカバー5とが一体となって上方に移動する。カバー5は開口部35の形状に合わせた略山形の形状となっており、カバー5の2つの傾斜面の下辺部が略矩形の底面31の傾斜面22及び傾斜面23側の辺にそれぞれ固定されたようになっているので、底面31及びカバー5によって形成されているドローン収容部3aの棟21が延びる方向の端部は、カバー5の2つの傾斜面と底面31とによって略三角形の開口部となっており、この開口部がドローンDが出入りする出入口36aとなっている。このように、屋根構造1aのドローン収容部3aは、出入口36aが、開口部35とは異なる場所に形成されており、ドローン収容部3aが傾斜屋根2と略一体となるように傾斜屋根2の内側に収まった状態のときには、出入口36aが塞がれて閉じた状態となる。そこから、駆動手段51aによってドローン収容部3aを傾斜屋根2の外側へせり出すように移動させると、出入口36aが露出して開いた状態となり、ドローンDが出入口36aを介してドローン収容部3aのドローンポート4に離着陸することができるようになっている。
2 傾斜屋根
3、3a ドローン収容部
31 底面
35 開口部
36、36a 出入口
4 ドローンポート
41 無接点充電手段
5 カバー
51、51a 駆動手段
52 情報取得手段
53 制御手段
7 太陽電池
D ドローン
Claims (7)
- 建物の上部を覆う傾斜屋根と、
底面が略水平になるように前記傾斜屋根の一部を切り欠くようにして設けられるドローンを収容可能な大きさのドローン収容部と、
前記ドローン収容部の前記底面に設けられる前記ドローンが離着陸可能なドローンポートと、
前記ドローン収容部のために前記傾斜屋根に形成された開口部を覆うカバーと、
前記ドローン収容部に設けられる前記ドローンが出入り可能な出入口と、
を備え、
前記カバーが開閉可能に構成され、前記カバーの開閉によって前記出入口が開閉することを特徴とする屋根構造。 - 前記カバーの開閉を駆動する駆動手段と、
前記ドローンの離着陸情報を取得する情報取得手段と、
前記情報取得手段によって取得された前記離着陸情報に基づいて前記駆動手段を制御して前記カバーを開閉させる制御手段と、
を備えることを特徴とする請求項1に記載の屋根構造。 - 前記ドローンポートが、前記ドローンが前記ドローンポートに着陸している状態で前記ドローンを充電可能な無接点充電手段を備えることを特徴とする請求項1に記載の屋根構造。
- 前記カバーの外面に太陽電池を備え、
前記無接点充電手段が、前記太陽電池によって発電された電力を用いて前記ドローンを充電することを特徴とする請求項3に記載の屋根構造。 - 建物の上部を覆う傾斜屋根と、
底面が略水平になるように前記傾斜屋根の一部を切り欠くようにして設けられるドローンを収容可能な大きさのドローン収容部と、
前記ドローン収容部の前記底面に設けられる前記ドローンが離着陸可能なドローンポートと、
前記ドローン収容部のために前記傾斜屋根に形成された開口部を覆うカバーと、
前記ドローン収容部に設けられる前記ドローンが出入り可能な出入口と、
を備え、
前記カバーが、前記ドローン収容部の前記底面に固定されており、
前記ドローン収容部の前記底面が、前記傾斜屋根の外側へせり出した状態と、前記傾斜屋根の内側に収まった状態との間で移動可能に構成されており、前記底面の移動によって前記出入口が開閉することを特徴とする屋根構造。 - 前記ドローンポートが、前記ドローンが前記ドローンポートに着陸している状態で前記ドローンを充電可能な無接点充電手段を備えることを特徴とする請求項2に記載の屋根構造。
- 前記カバーの外面に太陽電池を備え、
前記無接点充電手段が、前記太陽電池によって発電された電力を用いて前記ドローンを充電することを特徴とする請求項6に記載の屋根構造。
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