Using an aerial drone with a drone mounted interface to dock an adapted payload to a surface mounted interface

Abstract

Aspects include a system for mounting, securing, and otherwise installing or uninstalling a payload from an originating drone to a stationary object, utilizing a frustoconical based docking system. The system includes (i) a drone, (ii) an integrated vertical drone mounted interface (DMI), (iii) an adapted payload (AP), and (iv) a surface mounted interface (SMI). The DMI is attached directly to the drone, while the SMI is attached directly to the installation location of the stationary object. The AP is a unit capable of coupling to both the DMI and the SMI. The DMI couples with the AP, and then the AP is either coupled or uncoupled from the SMI depending on whether the AP is being installed or uninstalled. Depending on the requirements for installing the AP, both the DMI and AP can be configured in various manners to take advantage of installing a payload vertically, horizontally, or with a claw attachment.

Description

[0001] USING AN AERIAL DRONE WITH A DRONE MOUNTED INTERFACE TO DOCK AN ADAPTED PAYLOAD TO A SURFACE MOUNTED INTERFACE

[0002] BACKGROUND

[0003] Autonomous drones, also referred to as unmanned aerial vehicles (UAVs) or remotely piloted aircraft (RPA) have widespread use in applications such as surveying, photography, and package delivery. Drones can quickly reach areas that would be difficult, dangerous, or otherwise inaccessible to humans. Drones can also provide video or photographic capture in any conceivable direction and can deliver small payloads to precise locations. Most drones operate by rotary flight. The nature of rotary flight means a drone is capable of both vertical and stationary flight. These characteristics would seem to make drones a prime candidate for performing labor intensive tasks such as replacing faulty aircraft warning lights at the top of radio towers. However, the limitations of stationary flight are such that maintenance and service applications are restricted to manipulations which do not create countervailing forces that would otherwise upset the stationary equilibrium.

[0004] Therefore, it is envisioned that for a drone to succeed at maintenance tasks, such as replacing lights on radio a tower, it will need to have an interface between the drone and the maintenance target.

[0005] SUMMARY

[0006] Embodiments include a system for mounted, securing, and otherwise installing or uninstalling a payload from an originating drone to a stationary object. The system includes a drone, an integrated vertical drone mounted interface (DMI), an adapted payload (AP), and a surface mounted interface (SMI). The DMI is attached directly to the drone. The SMI is attached directly to the installation location of the stationary object. The AP is a unit capable of coupling to both the DMI and the SMI. The DMI couples with the AP, and then the AP is either coupled or uncoupled from the SMI depending on whether the AP is being installed or uninstalled. Depending on the requirements for installing the AP, the DMI might be configured as a vertical drone mounted interface (vDMI), a horizontal drone mounted interface (hzDMI) or a claw drone mounted interface (cDMI), while the AP might be configured as either described (AP), a horizontal adapted payload (hzAP), or a claw adapted payload (cAP).

[0007] SUBSTITUTE SHEET (RULE 26) Further embodiments include a method for installing objects to a stationary platform using a drone, a DMI, an SMI, and an AP. When an AP is being installed on an SMI, the DMI couples with the AP, the drone travels to the SMI, AP docks with the SMI, the AP couples with the SMI, then the DMI uncouples from the AP.

[0008] Further embodiments include a method for uninstalling objects to a stationary platform using a drone, a DMI, an SMI, and an AP. When an AP is being uninstalled from an SMI, the drone travels to the AP that is coupled to the SMI, the DMI docks with the AP, the AP couples with the DMI, the SMI decouples from the AP, and the drone returns with the DMI and coupled AP.

[0009] Further embodiments include an apparatus which allows docking and coupling between an SMI and an AP. The components on the SMI include a drone mount receptor with an integrated locking mechanism which is operated by a motor. The component on the AP includes a drone mount guide which is attached to the bottom of the AP. The drone mount guide fits securely inside the drone mount receptor and has an indentation which allows for locking.

[0010] Further embodiments include an apparatus which allows docking and coupling between a DMI and an AP. The components on the AP include several drone mount receptors with integrated locking mechanisms which are each operated by a separate motor. The components on the DMI include several drone mount guides which are attached to the bottom of the DMI. The drone mount guide fits securely inside the drone mount receptor and has an indentation which allows for locking.

[0011] Additional features are realized through the techniques of the present invention. Other embodiments and aspects of the invention are described in detail herein and are considered part of the claimed invention. For a better understanding of the invention with the features, refer to the description and the drawings.

[0012] BRIEF DESCRIPTION OF DRAWINGS

[0013] The Detailed description is set forth with reference to the accompanying figures. In the figure, the left-most digit(s) of a reference number identifies the figure in which the reference number first appears. The use of the same reference numbers in different figures indicates similar or identical items or features.

[0014] SUBSTITUTE SHEET (RULE 26) Fig. 1 - Depicts a block diagram of an autonomous drone in accordance with an embodiment of this disclosure.

[0015] Fig. 2 - Depicts a block diagram for a UAV Controller

[0016] Fig. 3 - Depicts a perspective view of an AP installation on a SMI, located on a radio tower, using an autonomous drone in accordance with the embodiments of this disclosure.

[0017] Fig. 4 - Depicts a perspective view of an AP uninstallation on a SMI, located on a radio tower, using an autonomous drone in accordance with the embodiments of this disclosure.

[0018] Fig. 5 - Depicts a vertical drone mounted interface.

[0019] Fig. 6 - Depicts an adapted payload.

[0020] Fig. 7 - Depicts a horizontal drone mounted interface.

[0021] Fig. 8 - Depicts a horizontal adapted payload.

[0022] Fig. 9 - Depicts a surface mounted interface.

[0023] Fig. 10 - Depicts embodiments of the vDMI and AP in various stages of coupling.

[0024] Fig. 11 - Depicts embodiments of the hzDMI and AP in various stages of coupling.

[0025] Fig. 12 - Depicts embodiments of the AP and SMI in various stages of coupling.

[0026] Fig. 13 - Depicts a claw drone mounted interface.

[0027] Fig. 14 - Depicts a claw adapted payload.

[0028] Fig. 15 - Depicts embodiments of the cDMI and cAP various stages of coupling.

[0029] DETAILED FIGURE DESCRIPTIONS.

[0030] Figure 1 - Block Diagram of an Autonomous Drone in accordance with an Embodiment of this Disclosure

[0031] Figure 1 is an embodiment of an autonomous drone or unmanned aerial vehicle 100 with a Drone Mounted Interface 300. As used herein, the term “drone” refers to a vehicle that is capable of being piloted by a remote operator, a pre-programmed set of operations, adaptive programming, or artificial intelligence. The body of the drone includes a fuselage 101 and a plurality of thrust producing devices 102 which are configurable to produce both vertical lift and lateral thrust, and an onboard power source 106. Creating vertical lift and lateral thrust, allows the drone to rise vertically, descend vertically, change orientation, travel laterally, or move in a combination of lateral and vertical directions. By necessity, the thrust produced by the thrust producing devices 102 must be sufficient to lift the weight of the autonomous drone

[0032] SUBSTITUTE SHEET (RULE 26) with the DMI 300, and a coupled adapted payload 400. In one embodiment, the fuselage 101 is connected to three thrust producing devices 102(A-C).

[0033] Integrated into the UAV is a controller 200. The controller 200 is composed of processing circuits, memory, and at least one processor. The controller is cable of receiving programed instructions and effectuating those instructions. The controller 200 is capable of receiving information from and transmitting information to the thrust producing devices 102, thereby operating the thrust producing devices. The controller 200 is further capable of receiving information from positioning devices 103. In one embodiment, the positioning devices 103 include sensors such as an altimeter 103A, accelerometers 103B, gyroscopes 103C, or a global positioning satellite system “GPS” 103D. In another embodiment, the UAV is equipped with communication equipment 104 such as radio frequency “RF” receivers, transmitters, transceivers, or other such devices capable of sending and receiving communication signals. In another embodiment UAV is equipped with video or still cameras 105. The controller 200 is also capable of receiving and effectuating instructions to operate the coupling mechanism between the DMI 300 and a coupled adapted payload 400. In one embodiment the controller 200 is capable of receiving and effectuating instructions to operate the coupling mechanism between the adapted payload and a coupled SMI 500. In another embodiment, the controller is capable of receiving diagnostic information from the surface 600, through a completed circuit, when both the DMI 300 is docked with the AP 400 and the AP 400 is docked with the SMI 500.

[0034] Figure 2 - Block Diagram for a UAV Controller

[0035] Figure 2 is a block diagram embodiment of a controller which can effectuate the operations of a UAV 100 in accordance with methods described in this disclosure. A particular embodiment of a UAV controller 200 contains one or more processors 202, coupled to non-transitory computer readable storage (memory) 204 through an input / output (I / O) interface 201. Additional Data, including, for example, instructions for the processor 202 or other retrievable information, may be stored in storage 204, which may be storage device such as a hard disk drive or solid-state drive. The stored instructions in memory 202 or in storage 204 may include those enabling the processor to execute one or more aspects of the systems and methods of this disclosure. The I / O interface may be connected to components such as network or data communication interfaces 206 that are capable of connecting to a radio, wifi, cellular or other

[0036] SUBSTITUTE SHEET (RULE 26) network 210, power supplies 205, I / O controller 207 that operates input devices 212 such as flight sensors, positioning sensors, diagnostic sensors, output devices 211 such as thrust producing devices 102, a display controller 208 capable of operating a user interface or user displays 212 like an LCD screen, as well as a locking controller 209 which could be capable of operating the SMI or DMI locking mechanisms.

[0037] In certain embodiments, the memory on the controller may be configured to contain an operating system, executable instructions, data, flight plans, flight control parameters, sensor adjustment information, or other such data or instructions necessary to fly, navigate, and operate the UAV.

[0038] The data communication interfaces may allow the controller to use components that facilitate direct or wireless communication between the controller and a remote device. It is anticipated that such communications could facilitate the transfer of data or the remote execution of instructions. It is also anticipated that the data communication interface could receive diagnostic information from the AP or the SMI.

[0039] It is anticipated that the controller will receive positioning, telemetry, and status data from various components attached to the I / O interface, which will allow controller to operating the UAV in such a manner that it travels to the target location, docks with either the AP of the SMI, uncouples from either AP or SMI depending on whether an AP is being installed or uninstalled, and returns to the point of origin.

[0040] In certain embodiments, while docked with the AP and the SMI, the controller may receive data from the SMI, through an IO data interface, which it then in turn may store and / or transmit to a remote device.

[0041] Figure 3 - Perspective view of an AP installation on a SMI, using an autonomous drone in accordance with the embodiments of this disclosure.

[0042] In Figure 3(A-C), an embodiment of this disclosure is installing an AP onto an SMI. In this particular embodiment, the AP includes a radio tower warning light 403, that has been mounted into the AP housing 400. To initiate the process, the UAV 100 with a DMI 300 is placed on top of the AP 400 at a remote location, such that the DMI guides 301 are fully seated within

[0043] SUBSTITUTE SHEET (RULE 26) the DMI receptors 401. Upon receiving a signal that the DMI receptors are fully seated within the DMI guides, the UAV controller 200, or a series of sensors, engages the DMI receptor locking wheel 412, located in the AP, and the DMI is securely coupled to the AP.

[0044] The UAV is then remotely piloted to the SMI 500 where it positions the SMI guide 402 directly over the SMI receptor 501. Next, the UAV descends vertically, until the SMI guide is fully seated in the SMI receptor, at which point, a signal is sent to the UAV controller 200 the SMI 500 is correctly docked. The UAV controller 200 then engages the SMI receptor locks 506, securely coupling the AP 400 to the SMI 500. When the SMI receptor locks are engaged, a signal is sent to the UAV controller 200. Upon coupling between the AP and the SMI, the AP receives power through the SMI Power connection 509. The AP sends a signal to the UAV controller that it is receiving power. After the UAV has received signals that the SMI receptor locks are engaged and the AP is receiving power, the UAV controller disengages DMI receptor locks and remotely pilots the UAV back to where the process was initiated.

[0045] In another embodiment, the UAV controller does not control the DMI and SMI locking mechanism, rather, a sensor on the SMI guides 402, or points that close a circuit, come into contact with a contact point on the SMI receptor 501 which sends a signal to the DMI locking mechanism to engage the SMI locking mechanism 506; after which, a signal is sent to the DMI locking mechanism such that it disengages the DMI locking wheel 506, unlocking the DMI from the AP.

[0046] Figure 4 - Perspective view of an AP uninstallation on a SMI, using an autonomous drone in accordance with the embodiments of this disclosure.

[0047] In Figure 4 (A-C), an embodiment of this disclosure is uninstalling an AP 400 from an SMI 500, located on a radio tower. In this particular embodiment, the AP includes a radio tower warning light 403, that has been mounted into the AP housing 400. To initiate the process, a UAV 100 with a DMI 300 is remotely piloted to the AP 400, which is coupled to an SMI 500, which is mounted on a radio tower (surface) 600. Upon reaching the AP, the UAV positions the DMI guides 301 over the DMI receptors 401. Next the UAV descends vertically until the DMI guides are fully seated within the DMI receptors. Upon receiving a signal that the DMI

[0048] SUBSTITUTE SHEET (RULE 26) receptors are fully seated within the DMI guides, the UAV controller 200 engages the DMI receptor locking wheel 412, located in the AP, and the DMI is securely coupled to the AP.

[0049] Subsequently, the UAV controller 200 disengages the SMI receptor locks 506 releasing the AP from the SMI. The UAV with the DMI coupled to the AP is then remotely piloted back to the point of initiation.

[0050] In another embodiment, the UAV controller does not control the DMI and SMI locking mechanism, rather, a sensor on the DMI guides 301, or points that close a circuit, come into contact with a contact point on the DMI receptor 401 which sends a signal to the DMI locking mechanism to engage the DMI locking wheel; after which, a signal is sent to the SMI locking mechanism such that it disengages the SMI lock 506, unlocking the AP from the SMI.

[0051] Figure 5 - Vertical Drone Mounted Interface

[0052] Figure 5 is an embodiment of a vertical drone mounted interface (“vDMI”). The vDMI consists of a top plate 302 that attaches directly to a UAV 100. In one embodiment, the top plate is secured to the underside of a drone by fasteners, such as (but not limited to) bolts, screws, or locking pins, that extend from the drone fuselage, through the top plate, and are secured by locking nuts or locking pins. In another embodiment, the top plate is secured to the drone by two interlocking brackets, respectively attached to the top surface of the top plate and the lower surface of the drone. In another embodiment, the DMI top plate is secured to the UAV by a connector rod with one or more ball or hinged joints 702.

[0053] Attached to the underside of the top plate is two or more DMI legs 309. The DMI legs should be located at the same position as the DMI receptors on the AP, such that the DMI guides line up with the DMI receptors to facilitate coupling. Furthermore, the DMI legs should be attached equidistantly from one another along the circumference of a circle, so the overall weight of the DMI is balanced at a center point.

[0054] The DMI legs are composed of risers 303 and DMI Guides 301. The minimum length of risers 303, is the length necessary to accommodate the height of the adapted payload. In some embodiments the risers are permanently affixed to the top plate. The risers can be either hollow or solid. In other embodiments, the risers are interchangeable and secured to the top plate by

[0055] SUBSTITUTE SHEET (RULE 26) screwing them into threaded holes and / or securing them in place with locking pins. Attached to the bottom of the riser is a frustoconical guide 304 with a locking shank 306. The size of the locking shank is less than the smallest surface of the frustoconical guide. The notch 305 in the locking shank is a size necessary to accommodate the locking key 415. It is anticipated that the riser 303, frustoconical guide 304, and locking shank 306, collectively known as DMI legs 309, could be separate pieces that are attached together, or a singular piece.

[0056] In certain embodiments the locking shank contains a proximity sensor 307, connected by a wire which extend through a hollow center of the DMI legs, or along the exterior of solid DMI legs, and attaches to an interface 308 which allows connection to the UAV controller. In one embodiment, the proximity sensor is placed on the bottom of the locking shank such that a proximity signal can be received by the UAV controller, signaling to the UAV controller when the drone is fully seated.

[0057] In another embodiment the locking shank contains a metal contact, connected by a wire which extend through a hollow center of the DMI legs, or along the exterior of solid DMI legs, and attaches to an interface which allows connection to the UAV controller. When the locking shank is fully seated in the DMI receptor on the AP, a metal contact in the DMI receptor makes direct contact with the locking shank metal contact. The metal contact in the DMI receptor is connected to a wire which can be connected to sensors, controllers, other transitional connectors.

[0058] Figure 6 - Adapted Payload

[0059] Figures 6(A-D) are various perspective of an embodiment of an adapted payload. The AP has an enclosure 404, formed by a mounting plate 405, walls 407, and a bottom plate 406. Means to join the pieces of the AP enclosure together include, but are not limited to fasteners, adhesives, locking brackets, or threaded connections.

[0060] The top surface of the AP is a mounting plate which has two or more DMI receptors 401 which penetrate the mounting plate. The DMI receptors are located at the same position as the DMI legs 309, such that the DMI receptors line up with the DMI guides 301 to facilitate coupling. The DMI receptors 401 have a frustoconical sidewall that matches the taper and size of the DMI guide 301, and a cylindric well 413 that extends below the frustoconical sidewall. The

[0061] SUBSTITUTE SHEET (RULE 26) cylindric well should be deep enough such that the locking shank 306 on the DMI guide 301 can fully seat. The DMI cylindric well 413 should have a cutout opening that is up 180 degrees of circumference of the cylinder well and a height that is greater than the height of the DMI locking wheel 412. It is anticipated that the DMI receptors could be once piece that is attached to penetrations in the mounting plate 405, or the frustoconical receptor is milled or molded into the receptor, and the cylinder well is attached to the underside of the mounting plate. In one embodiment, a contact point connected to a wire is located at the bottom of the cylinder well 413 for the purposes of making contact with a contact point on the bottom of the DMI guide’s locking shank 306.

[0062] The payload 403 is attached to the top of the mounting plate 405 and centered such that the overall adapted payload is balanced. Means to attach the payload to the mounting plate include but are not limited to use of fasteners, locking brackets, or adhesives. In one embodiment, the payload is a tower warning light that receives electrical power through a wire that penetrates the mounting plate and connects to a electrical contact points on the bottom of the SMI guide locking shank.

[0063] On the underside of the AP mounting plate 405, inside the AP enclosure 404, a locking wheel is set on a shaft that is located at the center of the mounting plate. The locking wheel is rotated by a servo motor 414 or other mechanical device capable of producing rotational force. In one particular embodiment, wherein the mounting plate has three DMI receptors 401, the locking wheel has three locking keys 415 attached or built into its rim. The locking keys 415 are of a size such that when the DMI guides locking shank 306 is fully seated in the DMI receptor, the locking keys overlap the locking shank’s notch 305, and secure the DMI guides 301 into the DMI receptors 401. It is anticipated that the number of locking keys on the rim of the locking wheel will equal the number of DMI receptor guides that are located on the mounting plate. In one embodiment, the servo motor 414 or other mechanical device capable of producing rotational force will be powered by a battery located in the AP. It is also anticipated that the servo motor or other mechanical device capable of producing rotational force could receive power from a wire that connects to the SMI 500. It is also anticipated that the servo motor or other mechanical device capable of producing rotational force could receive power through both a battery and the SMI, or that the SMI could provide power to a rechargeable battery, thus maintaining its charge.

[0064] SUBSTITUTE SHEET (RULE 26) At least one SMI guide 402 is attached to the underside of the AP bottom plate 406. The SMI guide 402 is composed of a frustoconical guide 408, a notch 409, and a locking shank 410. In the embodiment of this disclosure wherein there is only one SMI guide 402, it is centered at the middle of the bottom plate 406. In certain embodiments where in the AP has more than one SMI guide402, they are positioned equidistant from one another, along a circular pattern, such that the center of gravity for the AP is at the center of the bottom plate 406. In certain embodiments, the bottom of the SMI guide locking shank has a metal contact point 411 which is connected to a wire that connects to a contact in the bottom inner surface of the cylindric well of a SMI receptor 501.

[0065] Figure 7 - Horizontal Drone Mounted Interface

[0066] Figure 7 is an embodiment of a horizontal drone mounted interface (“hzDMI”). The hzDMI consists of a UAV mounting plate 701, a connector rod with one or more ball or hinged joints 702, a back plate 703, two or more DMI legs 309. In one embodiment, the ball joint connector rod 702 is secured to both the UAV mounting plate 701 and back plate 703 with a threaded connection or a locking pin. The UAV mounting plate 701 is attached to the underside of the drone 100, and is secured by fasteners, such as (but not limited to) bolts, screws, or locking pins, that extend from the drone fuselage 101, through the UAV mounting plate 701, and are secured by locking nuts or locking pins. In another embodiment, the UAV mounting plate701 is secured to the drone by two interlocking brackets, respectively attached to the top surface of the UAV mounting plate and the lower surface of the drone. Attached to the backplate 703 are two or more DMI legs 309. The DMI legs 309 should be located at the same position as the DMI receptors 401 on the AP 400, such that the DMI guides 301 line up with the DMI receptors 401 to facilitate coupling.

[0067] In certain embodiments, a counterbalance is attached to the back plate, opposite of the DMI legs. The counterbalance may be composed of a track 704, a weight 706, and a stop at the end of the track 705. The mechanism to slide the counterbalance weight could include manual adjustment, a belt driven motor, a motor driven cog along a track, motor driven cog which slides a track, cables and a motor, or other such methods, known in the art, to move a counterbalance weight 706 along a track 704. In certain embodiments, the counterbalance mechanism is operated by the UAV controller 200. In other embodiments, the counterbalance

[0068] SUBSTITUTE SHEET (RULE 26) operation is triggered by a sensor or signal which indicates that the SMI locking mechanism 506 has engaged or disengaged from the AP locking shanks 410.

[0069] The DMI legs are composed of risers 303, the minimum length of which is necessary to accommodate the height of the adapted payload. In some embodiments the risers are permanently affixed to the back plate. In other embodiments, the risers are interchangeable and secured to the back plate by screwing them into threaded holes and / or securing them in place with locking pins. Attached to the bottom of the riser is a frustoconical guide 304 with a locking shank 306. The size of the locking shank is less than the smallest surface of the frustoconical guide 304. The notch 305 in the locking shank is a size necessary to accommodate the locking key. It is anticipated that the riser 303, frustoconical guide 304, notch 305, and locking shank 306, collectively known as DMI legs 303, could be separate pieces that are attached together, or a singular piece.

[0070] In certain embodiments the locking shank 306 contains a proximity sensor 307, connected by a wire which extend through a hollow center of the DMI legs 303, or along the exterior of solid DMI legs 303, and attaches to an interface which allows connection to the UAV controller 200. In one embodiment, the proximity sensor 307 is placed on the bottom of the locking shank such that a proximity signal can be received by the UAV controller 200, signaling to the UAV controller 200 when the DMI guide 301 is fully seated.

[0071] In another embodiment the locking shank 306 contains a metal contact, connected by a wire which extend through a hollow center of the DMI legs 303, or along the exterior of solid DMI legs 303, and attaches to an interface which allows connection to the UAV controller 200. When the locking shank 306 is fully seated in the DMI receptor 401 on the AP 400, a metal contact in the DMI receptor 401 makes direct contact with the locking shank metal contact 307. The metal contact in the DMI receptor 401 is connected to a wire which can be connected to sensors, controllers, other transitional connectors.

[0072] Figure 8 -Horizontal Adapted Payload

[0073] Figure 8 is an embodiment of a horizontal adapted payload. The hzAP has an enclosure 801, formed by a mounting plate, structural frame supports, and a side plate. The hzAP should have

[0074] SUBSTITUTE SHEET (RULE 26) a center of gravity that is directly below the center of the drone and is used in conjunction with the hzDMI. The hzAP works in conjunction with a vDMI.

[0075] The top surface of the hzAP is a mounting plate 802 which has one or more DMI receptors 401 which penetrate the mounting plate. The DMI receptors 401 are located at the same position as the DMI legs 303, such that the DMI receptors 401 line up with the DMI guides 301 to facilitate coupling. The DMI receptors 401 have a frustoconical sidewall that matches the taper and size of the DMI guide 301, and a cylindric well 413 that extends below the frustoconical sidewall. The cylindric well 413 should be deep enough such that the locking shank 306 on the DMI guide 301 can fully seat. The DMI cylindric well 413 should have a cutout opening that is up 180 degrees of circumference of the cylinder well and a height that is greater than the height of the DMI locking wheel 412. It is anticipated that the DMI receptors 401 could be once piece that is attached to penetrations in the mounting plate, or the frustoconical receptor is milled or molded into the receptor, and the cylinder well is attached to the underside of the mounting plate 802. In one embodiment, a contact point 307 connected to a wire is located at the bottom of the cylinder well 413 for the purposes of making contact with a contact point on the bottom of the DMI guide’s 301 locking shank 306.

[0076] The payload is attached to the side plate 803. The side plate 803 is a surface that is adjacent and perpendicular to the mounting plate 801. In one embodiment the side plate 803 and mounting plate 802 are directly joined together along an edge. In another embodiment, the side plate 803 and mounting plate 802 are joined along an edge, but also have a structural frame that may be, but are not limited to, a cube, cuboid, or right triangular prism. In order to achieve a center of gravity that is directly underneath the vDMI, weights can be added to different parts of the structural frame.

[0077] Means to attach the payload to the side plate include but are not limited to use of fasteners, locking brackets, or adhesives. In one embodiment, the payload is a tower warning light that receives electrical power through a wire that penetrates the mounting plate 802 and connects to electrical contact points on the bottom of the SMI guide locking shank 410.

[0078] On the underside of the AP mounting plate 802, inside the AP enclosure, a locking wheel 412 is set on a shaft that is located at the center of the mounting plate. The locking wheel is rotated

[0079] SUBSTITUTE SHEET (RULE 26) by a servo motor 414 or other mechanical device capable of producing rotational force. In one particular embodiment, wherein the mounting plate has three DMI receptors 401, the locking wheel 412 has three locking keys 415 attached or built into its rim. The locking keys 415 are of a size such that when the DMI guides locking shank 410 is fully seated in the DMI receptor 401, the locking keys 415 overlap the locking shank’s notch 305, and secure the DMI guides 301 into the DMI receptors 401. It is anticipated that the number of locking keys 415 on the rim of the locking wheel will equal the number of DMI receptors 301 that are located on the mounting plate 802. In one embodiment, the servo motor 414 or other mechanical device capable of producing rotational force will be powered by a battery located in the AP. It is also anticipated that the servo motor 414 or other mechanical device capable of producing rotational force could receive power from a wire that connects to the SMI 500. It is also anticipated that the servo motor or other mechanical device capable of producing rotational force could receive power through both a battery and the SMI, or that the SMI could provide power to a rechargeable battery, thus maintaining its charge.

[0080] At least one SMI guide 402 is attached to the hzAP side plate 803, opposite the attached payload 403. The SMI guide 402 is composed of a frustoconical guide 408, a notch 410, and a locking shank 410. In the embodiment of this disclosure wherein there is only one SMI guide 402, it is centered at the middle of the side plate 803. In certain embodiments where in the AP has more then one SMI guide 402, they are positioned equidistant from one another, along a circular pattern, such that the center of gravity for the AP is at the center of the bottom plate. In certain embodiments, the bottom of the SMI guide locking shank 401 has a metal contact point 411 which is connected to a wire that connects to a contact in the bottom inner surface of the cylindric well of a SMI receptor 501.

[0081] Figure 9 - Surface Mounted Interface

[0082] Figure 9A is an embodiment of a Surface Mounted Interface 500. The SMI 500 is composed of at least one SMI receptor 501, an SMI locking mechanism 507, and a SMI base plate 508. In certain embodiments, the SMI 500 also has a SMI controller 502 that capable of operating the locking mechanism, receiving data or diagnostic information from the surface, and communicating with the UAV controller 200. It is anticipated that the SMI receives electrical power from an external source, a battery, or a combination of external power and rechargeable batteries 509. The SMI receptor 501 has frustoconical sidewalls 503 with a taper that matches

[0083] SUBSTITUTE SHEET (RULE 26) the taper of the SMI guide 402, and a cylindric well that extends below the frustoconical sidewalls 503. The cylindric well should be deep enough such that the locking shank 410 on the SMI guide 402 can fully seat. The SMI cylindric well should have a cutout opening that is up 180 degrees of circumference of the cylinder well and a height that is greater than the height of the SMI key lock or SMI locking wheel. As seen in Figure 9B, the bottom of the SMI receptor cylinder well will have contact points 510 and 511, which are wired to the SMI power source 509, and are capable of providing power and data transfer to the AP 400 through an input connection 509 on the SMI guide 501.

[0084] In one embodiment the SMI 500 has only one SMI receptor 501. In this embodiment, the SMI guide’s locking shank 410 is secured in place with an SMI key lock 506, which moves is rotated by a servo motor 507, or other mechanical device capable of rotary operation. It is anticipated that the servo motor 507 or other mechanical device capable of rotary operation will be operated by a SMI controller 502 and will receive power from the SMI power source 509. In another embodiment, the SMI key lock is activated by sensors on the bottom of the SMI guide 402, or sensors on the from the AP 500, that indicate DMI receptors 401 have locked onto DMI guides 301.

[0085] In another embodiment, the SMI has multiple SMI receptors 501, and a locking wheel 412. The locking wheel is set on a shaft that is located at the center of the SMI base plate 508. The locking wheel is rotated by a servo motor 414 or other mechanical device capable of producing rotational force. In one particular embodiment, wherein the mounting plate has three SMI receptors, the locking wheel has three locking keys 415 attached or built into its rim. The locking keys are of a size such that when the SMI guides locking shank 410 is fully seated in the SMI receptor 501, the locking keys overlap the locking shank’s notch 409, and secure the SMI guides 402 into the SMI receptors 501. It is anticipated that the number of locking keys 415 on the rim of the locking wheel 412 will equal the number of SMI receptor guides 501. It is anticipated that the servo motor, or other mechanical device capable of rotary operation will be operated by a SMI controller 502 and will receive power from the SMI power source 509. In another embodiment, the SMI locking wheel 412 is activated by sensors on the bottom of the SMI guide 402, or sensors on the from the AP 500, that indicate DMI receptors 401 have locked onto DMI guides 301. In another particular embodiment the locking shanks involves the use of several servo motors, operating servo horns or linear gears.

[0086] SUBSTITUTE SHEET (RULE 26) The SMI controller 502 may be composed of processing circuits, memory, and may contain one or more processors. The controller is cable of receiving programed instructions and effectuating those instructions. It is anticipated that the controller will be able to directly through wired connection, or indirectly through wireless connections, interact with the UAV controller 200. In certain embodiments, the SMI controller 502 can be connected to sensors that can be transmitted to the UAV controller 200, and from the UAV controller 200 to a remote user.

[0087] Figure 10 - DMI & AP Coupling

[0088] Figures 10A-10C are embodiments of the vDMI 300 and AP 400 in various stages of coupling. Figure 10A illustrates the first stage of coupling wherein the DMI guides 301 are lined up with the DMI receptors 401. In this embodiment, the horizontal center point of the DMI guide is lined up directly above the horizontal center point of the DMI receptor. Another acceptable initial coupling position is if the DMI guide’s locking shank 306 is positioned above the circular opening of the frustoconical receptor 401 but the horizontal center point of the DMI guide 301 is not lined up directly above the horizontal center point of the DMI receptor.

[0089] The second stage of coupling is where the UAV 100 with DMI 300 lowers vertically, fully seating the DMI guide 301 within the DMI receptor 401. If, as in Figure 10A, the DMI guide 301 and DMI receptor 401 are in perfect alignment, the UAV 100 descends vertically until the DMI guides’ locking shanks 306 are fully seated in the DMI receptor’s cylindric well 413. If the DMI guides 301 are positioned over the circular opening of the frustoconical receptor, but the center points of the DMI guides 301 and DMI receptors 401 are not perfectly lined up, upon vertical descent, the DMI guide locking shanks 306 will slide along the DMI receptors’ frustoconical inner walls, ultimately lining DMI guides’ and the DMI receptors’ center points, at which point the DMI guides’ locking shanks 306 will descend into the DMI receptors’ cylindrical well 413 and fully seat.

[0090] Figure 10B illustrates the third stage of coupling, wherein the DMI guides 301 are fully seated within the DMI receptors 401, and the DMI guides locking shanks 306 are correctly positioned within the DMI receptors cylindric well 413. As seen in figure 10B, the DMI guided locking shank 306 is positioned such that the notch 305 is centered in the opening of the DMI receptor

[0091] SUBSTITUTE SHEET (RULE 26) cylindrical well 413. In certain embodiments, after the DMI guides 301 are fully seated within the DMI receptors 401, the UAV may further reduce upward thrust to maintain a fully docked position.

[0092] Figure 10C illustrates the fourth stage of coupling, wherein the DMI guides’ locking shanks 306 are held in place by the DMI locking wheel 412. After the DMI guides 301 are fully seated within the DMI receptors 401, either the UAV controller 200, SMI controller 502, or a series of sensor activates the servo motor 414, or other mechanical device capable of producing rotational force, and the DMI wheel 412 rotates such that the locking keys 415 on the DMI locking wheel 412 line up with the notches 305 of the DMI guides 301, through the opening of the DMI receptor cylindric well 413.

[0093] When the DMI locking wheel 412 is controlled by a series of sensors, during installation of an AP 400, the DMI locking wheel 412 is triggered to unlock, when a sensor indicates the SMI guide 402 is fully seated within the SMI receptor 501, and the SMI locking mechanism 507 has been activated and moved into the locked position. During uninstallation of an AP 400, the DMI locking wheel 412 may be triggered to lock when sensors indicate the DMI guides 301 are fully seated within the DMI receptors 401, and the SMI locking mechanism 507 has just been activated and moved into the unlocked position.

[0094] Figure 11 - hzDMI & AP Coupling

[0095] Figures 11 A-l ID are embodiments of the hzDMI and AP in various stages of coupling. Figure 11 A illustrates the first stage of coupling wherein the DMI guides 301 are lined up with the DMI receptors 401. In this embodiment, the center axis of the DMI guides 301 are directly in line with the center axis of the DMI receptors 401. It is also an acceptable initial coupling position for the DMI guides 301 to be positioned in line with the circular opening of the frustoconical receptor 401 but without center axis of the DMI guide 301 being directly lined up with the center axis of the DMI receptor 401.

[0096] The second stage of coupling is wherein the UAV 100 with hzDMI travels laterally seating the DMI guides 301 within the DMI receptors 401. While lateral movement of the UAV may result in the UAV no longer being perpendicular with the AP or SMI, the ball or hinge joint on the hzDMI allows the UAV to tilt while the hzDMI remains in the proper docking position. The

[0097] SUBSTITUTE SHEET (RULE 26) counterweight 706 should be positioned along the counterbalance track 704 such that the DMI receptors 301 are in a plane parallel to the plane of the DMI receptors 401.

[0098] If, as in Figure 11 A, the DMI guides 301 and DMI receptors 401 are in perfect alignment, the UAV 100 moves laterally until the DMI guides’ locking shanks 306 are fully seated in the DMI receptor’s cylindric well 413. If the DMI guides 301 are positioned next to the circular opening of the frustoconical receptor, but the center axis’ of the DMI guides 301 and DMI receptors 401 are not perfectly lined up, upon lateral movement, the DMI guide locking shanks 306 will slide along the DMI receptors’ frustoconical inner walls, ultimately lining DMI guides’ and the DMI receptors’ center points, at which point the DMI guides’ locking shanks 306 will move into the DMI receptors’ cylindrical well 413 and fully seat.

[0099] Figure 11B illustrates the third stage of coupling, wherein the DMI guides 301 are fully seated within the DMI receptors 401, and the DMI guides locking shanks 306 are correctly positioned within the DMI receptors cylindric well 413. As seen in figure 11B, the DMI guided locking shank is positioned such that the notch is centered in the opening of the DMI receptor cylindrical well. In certain embodiments, after the DMI guides 301 are fully seated within the DMI receptors 401, the UAV 100 may increase lateral thrust to maintain a fully docked position.

[0100] After the DMI guides 301 are fully seated within the DMI receptors 401, either the UAV controller 200, SMI controller 502, or a sensor activates the servo motor 414, or other mechanical device capable of producing rotational force, and the DMI locking wheel 412 rotates such that the locking keys 415 on the DMI locking wheel 412 line up with the notches 305 of the DMI guides 301, through the opening of the DMI receptor cylindric well 413.

[0101] If the AP is being removed, once the DMI locking shanks 306 are secured, the UAV controller 200, SMI controller 502, or a series of sensors will trigger the SMI locking mechanism 507 to disengage, unlocking the AP 400 from the SMI 500.

[0102] When the DMI locking wheel is controlled by a series of sensors, during installation of an AP, the DMI locking wheel is triggered to unlock, when a sensor indicates the SMI guide is fully seated within the SMI receptor, and the SMI locking wheel has been activated and moved into

[0103] SUBSTITUTE SHEET (RULE 26) the locked position. During uninstallation of an AP, the hzDMI locking wheel may be triggered to lock when sensors indicate the DMI guides are fully seated within the DMI receptors, and the SMI locking wheel has just been activated and moved into the unlock position.

[0104] Figure 11C shows an embodiment of the UAV and hzDMI where the AP 400 being removed from the SMI, and the counterweight 1101 is set to balance the hzDMI without the AP. The connector rod with ball joint 702 allows the hzDMI and AP combination to tilt, recentering the payload center of gravity beneath the UAV 100.

[0105] Figure 1 ID shows an embodiment of the UAV and hzDMI where the AP 400 was installed onto the SMI 500, and the hzDMI has disengaged from the AP 400. Because the counterweight 1102 was set to balance the hzDMI with the AP, when the AP is disengaged, connector rod with ball joint 702 allows the hzDMI will tilt recentering the hzDMFs center of gravity beneath the UAV 100.

[0106] Figure 12 - SMI & AP Coupling

[0107] Figures 12A-12C are embodiments of the AP 400 and SMI 500 in various stages of coupling. Figure 12A illustrates the first stage of coupling wherein a single SMI guide 402 is lined up with an SMI receptor 501. It is anticipated the SMI 500 and AP 400 might have multiple SMI guides 402 and SMI receptors 501, that each line up with one another. In this embodiment, the center axis of the SMI guides 402 are directly in line with the center axis of the SMI receptors 501. It is also an acceptable position if the SMI guide’s locking shank 410 is positioned over the circular opening of the frustoconical receptor but the center axis of the SMI guide 402 is not lined up directly above the center axis of the SMI receptor 501.

[0108] The second stage of coupling whereby the UAV 100 with DMI 300 and AP 400 descends vertically seating the SMI guide 402 within the SMI receptor 501. If, as in Figure 12A, the SMI guide 402 and SMI receptor 501 are in perfect alignment, the UAV 100 descends vertically until the SMI guides’ locking shank 410 is fully seated in the SMI receptor’s cylindric well. In an embodiment where the SMI guides 402 are positioned over to the circular opening of the frustoconical receptor, but the center axis’ of the SMI guides 402 and SMI receptors 501 are

[0109] SUBSTITUTE SHEET (RULE 26) not perfectly lined up, upon vertical descent, the SMI guide locking shanks 410 will slide along the SMI receptors’ frustoconical inner walls, ultimately lining SMI guides’ and the SMI receptors’ center points, at which point the SMI guides’ locking shanks 410 will descend into the SMI receptors’ cylindrical well and fully seat.

[0110] Figure 12B illustrates the third stage of coupling, wherein the SMI guides 402 are fully seated within the SMI receptors 501 , and the SMI guides locking shanks 410 are correctly positioned within the SMI receptors cylindric well. As seen in figure 12B, the SMI guided locking shank is positioned such that the notch is centered in the opening of the DMI receptor cylindrical well. In certain embodiments, after the SMI guides 402 are fully seated within the SMI receptors 501, the UAV 100 may reduce upward thrust to maintain a fully docked position.

[0111] Figure 12C illustrates the fourth stage of coupling, wherein the SMI guide’s locking shanks is held in place by the SMI locking mechanism 507. After the SMI guide 402 is fully seated within the SMI receptor 501, either the UAV controller 200, SMI controller 502 or a series of sensors activates the servo motor 507, or other mechanical device capable of producing rotational force, and the locking key 506 rotates into the notch 409 of the SMI guide 402, through the opening of the SMI receptor cylindric well.

[0112] When the SMI locking mechanism 507 is controlled by a series of sensors, during installation of an AP 400, the SMI locking mechanism 507 is triggered, when a sensor indicates the SMI guide 402 has just become fully seated within the SMI receptor 501. During uninstallation of an AP 400, the SMI locking mechanism 501 may be triggered to unlock when sensors indicate the DMI locking wheel 412 has been fully activated and the DMI 300 is locked onto the AP 400

[0113] Figure 13 - Claw Drone Mounted Interface

[0114] Figure 13 A is an embodiment of a claw drone mounted interface. The cDMI consists of a UAV mounting plate 701, connector rod 702, and a claw grappler 1301.

[0115] It is envisioned that the connector rod 702 could be secured to both the UAV mounting plate 701 and grappler claw 1301 with a threaded connection or a locking pin. The UAV mounting plate 701 is attached to the underside of the drone, and is secured by fasteners, such as (but not

[0116] SUBSTITUTE SHEET (RULE 26) limited to) bolts, screws, or locking pins, that extend from the drone fuselage 101, through the UAV mounting plate 701, and are secured by locking nuts or locking pins. In another embodiment, the UAV mounting plate 701 is secured to the drone by two interlocking brackets, respectively attached to the top surface of the UAV mounting plate and the lower surface of the drone.

[0117] The cDMI, as described in Figure 13 A, has two grapple arms 1303 that are attached to a grappler pivot point 1302. It is anticipated that the grapple arm pivot point 1302 could be pins, rods, ball joints, hinges or other such means of securing the grapple arms 1303 while allowing the grapple arms 1303 to pivot outwards relative to a central vertical axis between the grapple arms 1303. The shape of the grapple arms 1303 should match the contours of the claw adapted payload (cAP) it is intended to carry. While the embodiment in figure 13B, shows that the surface of the grapple arms 1303 are tapered, it is anticipated that the width and taper of the arms can vary. The end of the grapple arms contains a hook 1304 which is capable of seating on the grapple rim of the cAP. In certain embodiments, the grapple arms 1303 are held in a closed position with a tensioning coil, tensioning spring, or other such method as known in the art. It is anticipated that the claw grappler could have more than two hooked arms, as described above.

[0118] Figure 14 - Claw Adapted Payload

[0119] Figure 14 is an embodiment of a claw adapted payload (cAP). The cAP has a frustoconical protrusion 1401, with a hollow interior, connected to a mounting plate 1405 with a riser 1404, to create a gap between the mounting plate and the frustoconical protrusion, sufficient in size to allow the grapple hooks 1304 to catch the interior rim 1406 of the frustoconical protrusion 1401. The lower rim of the frustoconical protrusion is tapered towards the mounting plate. Inside the frustoconical protrusion, and surrounding the riser, is a cAP locking / unlocking rings 1403. The payload can either be located at the top of the frustoconical cone 1402, or inside of the frustoconical protrusion 1401.

[0120] The cap locking rings are two rings 1403, that have the same spacing as the gap in between the frustoconical protrusion 1401 and the mounting plate 1405. The rings 1403 move in tandem up or down the riser 1404 either lock the grapple hooks 1304 in place or push the grapple hooks down to the tapered face of the lower rim, such that the grapple hooks are ejected from the

[0121] SUBSTITUTE SHEET (RULE 26) lower rim. It is envisioned that the locking rings 1403 could be driven up or down using a servo, step or other mechanical motor, with the necessary gearing as understood in the art. It is also anticipated that the locking rings 1403 could be threaded to the riser 1404, but held rotationally stationary with pins, and the rotation of the riser by a servo, step or other mechanical motor would cause the locking rings to raise or lower. The locking rings could be activated by the UAV controller 200, SMI controller 502, or a series of sensors that activates a servo or other motor.

[0122] When the locking rings 1403 are controlled by a series of sensors, during installation of a cAP, the locking rings are triggered to unlock, when a sensor indicates the SMI guide 402 is fully seated within the SMI receptor 501, and the SMI locking mechanism 507 has been activated and moved into the locked position 506. During uninstallation of an cAP, the locking rings 1403 may be triggered to raise (lock) when sensors indicate the grapple hooks 1304 are fully seated on the frustoconical protrusion rim 1406 and the SMI locking mechanism 507 has just been activated and moved into the unlock position.

[0123] At least one SMI guide 402 is attached to the underside of the cAP bottom plate. The SMI guide 402 is composed of a frustoconical guide 408, notch 409, and a locking shank 410. In the embodiment of this disclosure wherein there is only one SMI guide 402, it is centered at the middle of the bottom plate. In certain embodiments where in the AP has more than one SMI guide 402, they are positioned equidistant from one another, along a circular pattern, such that the center of gravity for the cAP is at the center of the bottom plate 1405. In certain embodiments, the bottom of the SMI guide locking shank 410 has a metal contact point 411 which is connected to a wire that connects to a contact in the bottom inner surface of the cylindric well of a SMI receptor.

[0124] Fig. 15 - cDMI and cAP various stages of coupling.

[0125] Figures. 15(A-D) show the cDMI and cAP in various stages of coupling. Figure 15A shows the first stage of coupling between the cAP and the cDMI, wherein the claw grappler 1301 is positioned directly over the cAP. The UAV 100 descends vertically onto the cAP, and the grapple arms 1304 begin to pivot outwards and slide down the frustoconical protrusion 1401, of the cAP. Figure 15D shows the position when the grapple arms 1304 are fully seated onto the cAP, but the locking rings 1403 have yet to be engaged.

[0126] SUBSTITUTE SHEET (RULE 26) The locking rings are activated by the UAV controller 200, SMI controller 502, or a series of sensors on the mounting plate 1405 that interact with the grapple arms 1303. When the locking rings 1403 engage, they rise upwards; the bottom ring pushes the grapple arms 1303 up, until the grapple hooks 1304 are seated into the frustoconical protrusion rim 1406. Figure 15B shows the locking rings 1403 in an engaged position, holding the grapple hooks in place.

[0127] Figure 15C is an embodiment of the cAP, wherein the locking rings are driven up and down with a servo motor 1502 that turns a threaded screw 1502. The exterior or the cAP is dashed out in Figure 15C to show an embodiment of the inner workings of the cAP.

[0128] Figure 15 D shows the unlocking of the cAP from the cDMI. As the locking rings 1403 are lowered, the upper rings angled surface pushes the grapple arms down, until the frustoconical protrusion rim 1406, is removed, and the cDMI grapple arms 1303 pivot outwards until they slide free from the cAP.

[0129] SUBSTITUTE SHEET (RULE 26)

Claims

CLAIMS:

1. A system comprising: an aerial drone with a drone mounted interface that is attached to the aerial drone; a first controller that is capable of changing the altitude and the orientation of the aerial drone; an adapted payload that is capable of locking onto both the drone mounted interface and the surface mounted interface; a surface mounted interface that is attached directly to a stationary object; and sensors on the drone mounted interface, adapted payload, and surface mounted interface which engage the locking and unlocking mechanisms.2 The system of claim 1, wherein there is a second controller that is integrated with the surface mounted interface, which controls the locking mechanism between the surface mounted interface to the adapted payload and the locking mechanism between the drone mounted interface to the adapted payload.3 The system of claim 1, wherein the first controller and second controller communicate to facilitate assisted or automatic docking of the adapted payload to the surface mounted interface.4 The system of claim 1, wherein drone beacon sensors are added to the drone mounted interface, the adapted payload, and the surface mounted interface to facilitate assisted or automatic docking.

5. The system of claim 1, wherein the second controller is capable of communicating diagnostic information to the first controller while the adapted payload is locked onto both the drone mounted interface and the surface mounted interface.

6. The system of claim 1, wherein the adapted payload receives power through the surface mounted interface.SUBSTITUTE SHEET (RULE 26)7. The system of claim 1, wherein the adapted payload transfers data to the surface mounted interface.

8. A system which allows docking and coupling between a surface mounted interface and an adapted payload comprising; one, two, three, four, five, or six drone mount guides which are attached to the bottom of the adapted payload; one, two, three, four, five, or six drone mount receptors which are attached to the top side of the surface mounted interface, with an integrated locking mechanism that is operated by a motor; and a controller which operates the server motor that locks or unlocks the drone mount receptor.

9. A system which allows docking and coupling between a drone mount interface and an adapted payload comprising; one, two, three, four, five, or six drone mount guides which are attached to the bottom of the drone mounted interface; one, two, three, four, five, or six drone mount receptors with integrated locking mechanisms, which are operated by a motor, and are integrated into enclosure of an adapted payload; and a controller which operates the server motors that locks or unlocks the drone mount receptors.

10. A system which allows docking and coupling between a horizontal drone mount interface and an adapted payload comprising; one, two, three, four, five, or six drone mount guides which are attached to the backplate of the horizontal drone mounted interface; one, two, three, four, five, or six drone mount receptors with integrated locking mechanisms, which are operated by a motor, and are integrated into enclosure of an adapted payload; and a controller which operates the server motors that locks or unlocks the drone mount receptors.SUBSTITUTE SHEET (RULE 26)11. A system which allows docking and coupling between a drone mount interface and an horizontal adapted payload comprising; one, two, three, four, five, or six drone mount guides which are attached to the bottom of the drone mounted interface; one, two, three, four, five, or six drone mount receptors with integrated locking mechanisms, which are operated by a motor, and are integrated into enclosure of an horizontal adapted payload; and a controller which operates the server motors that locks or unlocks the drone mount receptors.

12. A system which allows docking and coupling between a claw drone mount interface and a claw adapted payload comprising; two, three, or four, five, or six grapple arms which are attached to a pivot point of a claw drone mounted interface; a claw adapted payload with a frustoconical protrusion and AND integrated locking ring mechanism, which is operated by a motor; and a controller which operates the server motors that locks or unlocks the drone mount receptors.

13. A method for installing an adapted payload on a surface mounted interface using an aerial drone with a drone mounted interface attached to the aerial drone comprising: locking the adapted payload to the drone mounted interface, which is attached to an aerial drone; flying the aerial drone with the attached drone mounted interface and locked adapted payload to the surface mount interface using the first controller; docking the adapted payload with surface mounted interface; using the second controller to lock the adapted payload to the surface mounted interface; and unlocking the drone mounted interface from the adapted payload.

14. The method of claim 13 further comprising: the first controller and second controller communicating to facilitate assisted or automatic docking of the adapted payload to the surface mounted interface.SUBSTITUTE SHEET (RULE 26)15. The method of claim 13 further comprising: drone beacon sensors are added to the drone mounted interface, the adapted payload, and the surface mounted interface to facilitate assisted or automatic docking.

16. A method for uninstalling an adapted payload from a surface mounted interface using an aerial drone with a drone mounted interface attached to the aerial drone comprising: flying the aerial drone with an attached drone mounted interface to the adapted payload which is locked onto the surface mounted interface using the first controller; docking the drone mounted interface with adapted payload which is locked onto the surface mounted interface; locking the adapted payload to the drone mounted interface which is attached to an aerial drone; and using the second controller to unlock the adapted payload from the surface mounted interface.

17. The method of claim 16 further comprising: the first controller and second controller communicating to facilitate assisted or automatic docking of the drone mounted interface with the adapted payload.

18. The method of claim 16 further comprising: drone beacon sensors are added to the drone mounted interface, the adapted payload, and the surface mounted interface to facilitate assisted or automatic docking.SUBSTITUTE SHEET (RULE 26)

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