Window configured for parking drone and method for stopping drone

Abstract

Provided in the embodiments of the present application are a window configured for parking a drone and a method for stopping a drone. The window comprises a window frame, a window sash and stop members, wherein the lower end of the window sash is hinged to the window frame; the window sash can rotate inwards relative to the window frame to a closed position where the window frame is closed, and can rotate outwards relative to the window frame to a parking position parallel to a horizontal plane; and the stop members are arranged on an outer side of the window frame and are configured to prevent, when the window sash rotates relative to the window frame to the parking position, the window sash from continuing to rotate. In the window in the embodiments of the present application, when the window sash is opened, a drone can be directly parked on the window sash, such that a user can retrieve first-aid supplies from the drone through the window, thereby shortening the delivery time for medical supplies.

Description

Window for docking a drone and method for parking a drone Technical Field

[0001] The present invention relates to the technical field of drone parking, and in particular to a window for docking a drone and a method for parking a drone. Background Art

[0002] Remote monitoring of cardiovascular and cerebrovascular patients using a remote emergency care system can significantly reduce mortality from cardiovascular and cerebrovascular diseases. For remote emergency care systems that use drones to deliver emergency supplies, enabling drones to quickly deliver supplies to patients and shortening delivery times is crucial for improving patient treatment outcomes.

[0003] Summary of the Invention

[0004] The embodiment of the present application provides a window for docking a drone, which is helpful in shortening the time it takes for the drone to deliver supplies. The embodiment of the present application also provides a method for parking a drone.

[0005] In a first aspect, an embodiment of the present application provides a window for docking a drone, comprising: a window frame; a window sash, the lower end of which is hinged to the window frame; the window sash being capable of rotating inward relative to the window frame to a closed position that closes the window frame and rotating outward relative to the window frame to a park position parallel to a horizontal plane; and a stop member disposed on the outside of the window frame, for preventing the window sash from continuing to rotate when the window sash rotates to the park position relative to the window frame.

[0006] In a second aspect, an embodiment of the present application provides a method for parking a drone, which uses the window of the first aspect of the present application to perform parking. The method includes: receiving a pairing request message sent by the drone, the pairing request message including identity information; establishing a connection with the drone based on the identity information to receive a window opening instruction from the drone; when the window opening instruction from the drone is received, controlling the window sash to rotate outward relative to the window frame to a parking position parallel to the horizontal plane; when the window sash rotates to the parking position, sending a landing permission instruction to the drone.

[0007] The window of the embodiment of the present application allows the drone to dock directly on the window sash when the window sash is opened, so that the user can remove emergency supplies from the drone through the window, thereby shortening the delivery time of medical supplies. Because the embodiment of the present application uses a flexible belt to open and close the window sash, when the drone is docked on the window sash, if the drone's positioning accuracy is not high, the drone may come into contact with the flexible belt. Compared with the rigid contact of the drone with a rigid material such as a telescopic rod, the embodiment of the present application can reduce the probability of damage to the drone by providing a flexible belt. BRIEF DESCRIPTION OF THE DRAWINGS

[0008] Other objects and advantages of the present invention will become apparent from the following description of the present invention with reference to the accompanying drawings, which will help to provide a comprehensive understanding of the present invention.

[0009] FIG1 is a schematic structural diagram of a window according to one embodiment of the present invention, wherein the window sash is in a closed position;

[0010] FIG2 is a schematic structural diagram of the window shown in FIG1 as viewed from the outside;

[0011] FIG3 is a side view of the window shown in FIG1 ;

[0012] FIG4 is a front view of the window shown in FIG1 ;

[0013] FIG5 is a schematic structural diagram of the window shown in FIG1 , wherein the window sash is in the parked position;

[0014] FIG6 is a partial enlarged view of the window shown in FIG5;

[0015] FIG7 is a top view of the window shown in FIG5;

[0016] FIG8 is a schematic structural diagram of the window shown in FIG5 as viewed from the outside;

[0017] FIG9 is a side view of the window shown in FIG5;

[0018] FIG10 is a schematic structural diagram of a window according to another embodiment of the present invention, wherein the window sash is in a closed position;

[0019] FIG11 is a schematic structural diagram of the window shown in FIG10 observed from the outside;

[0020] FIG12 is a side view of the window shown in FIG10;

[0021] FIG13 is a schematic structural diagram of the window shown in FIG10 , wherein the window sash is in the parked position;

[0022] FIG14 is a side view of the window shown in FIG10;

[0023] FIG15 is a schematic structural diagram of the window shown in FIG13 viewed from the outside below;

[0024] FIG16 is a schematic structural diagram of the damping member in FIG15;

[0025] FIG17 is a schematic structural diagram of a locking mating portion according to an embodiment of the present application;

[0026] FIG18 is a cross-sectional view of the locking engagement portion shown in FIG17 ;

[0027] Figure 19 is a schematic diagram of the interaction between the window processor and the drone, remote monitoring and emergency system, and monitoring equipment according to an embodiment of the present application.

[0028] It should be noted that the drawings are not necessarily drawn to scale, but are merely shown in a schematic manner that does not affect the reader's understanding.

[0029] Description of reference numerals:

[0030] 10. Window frame; 11. Upper first crossbar; 12. Lower first crossbar; 13. First sidebar;

[0031] 20. Window sash; 21. Frame; 211. Upper second crossbar; 212. Lower second crossbar; 213. Second sidebar; 22. Glass panel; 221. First positioning mark; 222. Second positioning mark; 223. Third positioning mark; 224. Fourth positioning mark;

[0032] 30. hinge; 31. rotating shaft;

[0033] 40. Stopper;

[0034] 50. Flexible belt; 51. End fitting; 52. First connecting member;

[0035] 60. Retractable assembly; 61. Retractable wheel; 62. Rotating shaft; 63. Synchronous belt; 64. Drive motor; 65. Bearing; 66. Second connecting member; 67. Second synchronous pulley;

[0036] 71. Locking portion; 72. Locking mating portion; 721. Lock seat; 722. Lock seat slide; 723. Lock; 7231. Lock hole; 7232. Lock slot; 724. Return spring; 725. Pull pin; 726. Return spring;

[0037] 80, damping element; 81, coil spring seat; 811, slot; 82, coil spring; 821, external connector; 822, internal connector;

[0038] 91. handle; 92. counterweight; 93. connector; 94. processor;

[0039] 200. Remote monitoring and emergency system; 300. Drone; 400. Monitoring equipment. DETAILED DESCRIPTION

[0040] To make the objectives, technical solutions, and advantages of the present invention more clear, the technical solutions of the present invention will be clearly and completely described below in conjunction with the accompanying drawings of the embodiments of the present invention. Obviously, the described embodiment is only one embodiment of the present invention, not all embodiments. Based on the described embodiment of the present invention, all other embodiments obtained by ordinary technicians in this field without creative work are within the scope of protection of the present invention.

[0041] It should be noted that, unless otherwise defined, the technical or scientific terms used in this application should have the common meanings understood by persons having ordinary skills in the field to which the invention belongs.

[0042] In the description of the embodiments of the present invention, “a plurality of” means at least two, such as two, three, etc., unless otherwise clearly and specifically defined.

[0043] As previously mentioned, for remote monitoring and emergency systems that use drones for emergency supplies delivery, enabling drones to quickly deliver supplies to patients and shorten delivery times is crucial for improving patient treatment outcomes. The inventors of this application discovered that modifying a user's windows so that they can be used as a landing point for drones when open can significantly shorten the delivery time.

[0044] Therefore, an embodiment of the present invention provides a window for docking a drone, thereby shortening the time it takes for the drone to deliver supplies.

[0045] Referring to Figures 1 to 5, the window of the embodiment of the present invention includes: a window frame 10, and a window sash 20. The window frame 10 is usually installed on a wall. The lower end of the window sash 20 is hinged to the window frame 10. The window sash 20 can be rotated inwardly relative to the window frame 10 to a closed position to close the window frame 10; and can be rotated outwardly relative to the window frame 10 to a parking position parallel to the horizontal plane to allow a drone to dock. It is easy to understand that in the embodiment of the present application, when the window sash 20 is in the parking position, the window sash 20 is located outdoors. "Inward rotation" in the embodiment of the present application can be understood as rotation toward the room; "outward rotation" can be understood as rotation toward the outside.

[0046] In some embodiments, the window further comprises a stopper 40 disposed on the exterior of the window frame 10, configured to prevent the window sash 20 from further downward rotation from its rest position. In such an embodiment, the stopper 40 can bear at least some of the weight of the window sash 20, providing support for the window sash 20. The window of this embodiment of the present invention has a simple structure and is suitable for installation in a user's home. When a user opens the window sash 20, a drone can dock directly on it, allowing the user to access drone-delivered supplies through the window, thereby shortening delivery time.

[0047] The inventors of this application further discovered that if a rigid telescopic rod is used to open and close the window sash relative to the window frame, when a drone is docked on the window sash, if the drone's positioning accuracy is not high, the drone may come into contact with the rigid telescopic rod during the docking process, thereby causing damage to the drone.

[0048] Therefore, to reduce the probability of damage to drones, in some embodiments, the window further includes: at least one flexible strap 50 and a retractable assembly 60. Each flexible strap 50 is connected to the window sash 20. The retractable assembly 60 is used to retract and extend each flexible strap 50. When the retractable assembly 60 retracts each flexible strap 50, the window sash 20 can rotate relative to the window frame 10 to a closed position, sealing the window frame 10. When the retractable assembly 60 releases each flexible strap 50, the window sash 20 can rotate outward relative to the window frame 10 to a parking position parallel to the horizontal plane, allowing the drone to dock.

[0049] When the drone is docked on the window sash 20, if the drone's positioning accuracy is not high, the drone may come into contact with the flexible belt 50. Compared with the rigid contact between the drone and rigid materials such as telescopic rods, the embodiment of the present invention uses the flexible belt 50 to realize the opening and closing of the window sash 20 relative to the window frame 10, which can reduce the probability of damage to the drone.

[0050] In a further embodiment, when the window has a stopper 40, the retracting assembly 60 can be further configured to continue releasing the flexible straps 50 when the window sash 20 is in the parked position by releasing the flexible straps 50, so that the flexible straps 50 are in a relaxed state. Referring to Figures 5, 8, and 9, in such an embodiment, since the flexible straps 50 are in a relaxed state rather than a tensioned state, on the one hand, if the landing point of the drone on the window sash 20 deviates due to inaccurate positioning, even if the drone contacts the flexible straps 50, the relaxed flexible straps 50 are less likely to cause damage to the drone. On the other hand, since the flexible straps 50 are in a relaxed state, they can sag under the action of gravity, thereby "making way" for the flying drone, minimizing obstruction to the drone and allowing the drone to fly from the side of the window sash 20 to directly above the window sash 20 at a lower position, thereby improving the accuracy of the drone's landing.

[0051] In some embodiments, the window sash 20 includes a frame 21 and a glass plate 22 mounted on the inner side of the frame 21. In such an embodiment, when the window for docking a drone is installed in a user's home, the window also has the ventilation and light transmission functions of an ordinary window without causing too much adverse impact on the ventilation and light transmission of the house.

[0052] The flexible band 50 can be connected to the frame 21 via a first connector 52. To facilitate installation, an end fitting 51 can be provided at the end of the flexible band 50. The end fitting 51 is connected to the frame 21 via the first connector 52. The flexible band 50 can be hinged to the first connector 52, so that when the window sash 20 rotates at different angles relative to the window frame 10, the flexible band 50 near the end fitting 51 is less susceptible to wear.

[0053] The window frame 10 may have a rectangular structure. The window frame 10 may include an upper first crossbar 11, a lower first crossbar 12, and two first side bars 13 connected to the upper first crossbar 11 and the lower first crossbar 12 on the same side. The two first side bars 13 are respectively a left first side bar and a right first side bar. A stopper 40 may be formed on the lower first crossbar 12.

[0054] Accordingly, the frame 21 may also have a rectangular shape. The frame 21 may include an upper second crossbar 211, a lower second crossbar 212, and two second side bars 213 connected to the upper second crossbar 211 and the lower second crossbar 212 on the same side. The lower second crossbar 212 is hinged to the lower first crossbar 12. For example, the lower second crossbar 212 is hinged to the lower first crossbar 12 via a hinge 30. The hinge 30 may be a rotating shaft 31.

[0055] In some embodiments, the number of flexible straps 50 may be one. In some embodiments, the number of flexible straps 50 may be two, each of which is connected to the upper portions of the two second side bars 213 via two first connectors 52. Compared to connecting the flexible strap 50 to the upper first crossbar 11 via the first connector 52, connecting the flexible strap 50 to the upper portions of the second side bars 213 via the first connector 52 prevents the flexible strap 50 from extending along the entire length of the glass panel 22 when the window sash 20 is in the parked position, thereby reducing the adverse impact of the flexible strap 50 on the drone landing.

[0056] Referring to Figure 6, in some embodiments, the retracting assembly 60 may include: a rotating shaft 62 and two retracting wheels 61. The axial ends of the rotating shaft 62 are rotatably provided on the two first side rods 13 of the window frame 10. One end of each flexible belt 50 away from the first connecting member 52 is wound around a retracting wheel 61. The two retracting wheels 61 are respectively coaxially connected to the rotating shaft 62 to rotate together with the rotating shaft 62. The two retracting wheels 61 are driven by the rotating shaft 62 to rotate forward and reverse, thereby realizing the release and retraction of the flexible belt 50. Since the two retracting wheels 61 are connected to the same rotating shaft 62, it is possible to ensure that the two retracting wheels 61 can synchronously retract and retract the two flexible belts 50.

[0057] 4 , in some embodiments, when the window sash 20 is in the closed position, the projections of the two retracting and extending wheels 61 within the plane of the glass sheet 22 are located within the projections of the two first side bars 13 within the same plane. In such embodiments, the retracting and extending wheels 61 do not affect the lighting of the glass sheet 22.

[0058] Referring to Figure 6 , in some embodiments, the retractable assembly 60 further includes a drive motor 64, a first synchronous pulley (not shown), a second synchronous pulley 67, and a synchronous belt 63. The drive motor 64 is mounted on the upper first crossbar 11. The first synchronous pulley is driven to rotate by the drive motor 64. The rotating shaft of the first synchronous pulley can be mounted on the upper first crossbar 11 via a bearing and a mounting member.

[0059] A second synchronous pulley 67 is mounted on the middle portion of the rotating shaft 62. A synchronous belt 63 engages with the first and second synchronous pulleys 67, so that the first synchronous pulley drives the second synchronous pulley 67 to rotate. In this embodiment, by providing the synchronous pulleys and synchronous belt 63, the two retractable and retractable pulleys 61 can be synchronously rotated using only a single motor, thus conserving space within the retractable and retractable assembly 60.

[0060] The retractable assembly 60 further includes a cover for housing the first synchronous pulley, the second synchronous pulley 67 and the synchronous belt 63 .

[0061] The retractable assembly 60 also includes: two second connecting members 66 and two bearings 65. The two second connecting members 66 are respectively connected to the upper part of the two first side rods 13. The upper part here can be understood as a position close to the upper first cross bar 11. The two bearings 65 are respectively arranged on the two second connecting members 66. The axial ends of the rotating shaft 62 are respectively connected to the two bearings 65. In such an embodiment, the retractable wheel 61 is fixedly connected to the rotating shaft 62, so that it is only necessary to connect the two ends of the rotating shaft 62 to the two first side rods 13 of the window frame 10, fix the drive motor 64 to the upper first cross bar 11 of the window frame 10, and realize the rotation transmission of the two through the synchronous belt 63, which not only rationally utilizes the space for layout, but also minimizes the impact on the field of view of the window, and also facilitates the installation of the retractable assembly 60.

[0062] 5 , in some embodiments, a locking portion 71 is provided on the window frame 10, and a locking mating portion 72 is provided on the window sash 20. When the window sash 20 is in the closed position, the locking mating portion 72 cooperates with the locking portion 71 to lock the window sash 20 to the window frame 10. In some embodiments, the locking portion 71 can be an electric lock.

[0063] A sealing strip may also be formed on the periphery of the window sash 20 to improve the sealing effect of the window frame 10 when the window sash 20 is in a closed state.

[0064] Referring to FIG. 7 , in some embodiments, the window sash 20 is formed with at least one positioning mark for positioning the drone. When the window sash 20 is in the parked position, the drone can be positioned according to the at least one positioning mark to dock on the window sash 20. The positioning mark formed on the window sash 20 in the embodiment of the present application facilitates the smooth landing of the drone on the window sash 20.

[0065] Each positioning mark can be formed on the glass plate 22. The positioning marks formed on the glass plate 22 include a first positioning mark 221, a second positioning mark 222, a third positioning mark 223, and a fourth positioning mark 224. The first positioning mark 221, the fourth positioning mark 224, the second positioning mark 222, and the third positioning mark 223 are symmetrically arranged on both sides of the glass plate 22.

[0066] The first positioning mark 221 and the second positioning mark 222 are respectively set at the upper corners of the glass plate 22, and the third positioning mark 223 and the fourth positioning mark 224 are respectively set at the two sides of the glass plate 22. The first positioning mark 221, the second positioning mark 222, the third positioning mark 223 and the fourth positioning mark 224 jointly define a rectangular area A. This rectangular area A is the area where the drone can land after being positioned according to the positioning marks. The glass plate 22 can be divided into an upper half (i.e., the side away from the hinge 30) and a lower half (i.e., the side close to the hinge 30) along the height direction of the window sash 20. The rectangular area A is located in the upper half of the glass plate 22 so that the drone is as far away from the window frame 10 as possible during landing to avoid collision with the window frame 10.

[0067] The line connecting the connection points of the two flexible straps 50 and the corresponding first connectors 52 is located in the middle region of rectangular area A. Rectangular area A can be divided into an upper third, a middle third, and a lower third along the height of the window sash 20, with the middle third constituting the middle region of rectangular area A. This arrangement not only helps reduce the torque required to rotate the window sash 20 from the parked position to the closed position (i.e., reduces the torque required to retract the flexible straps 50), but also minimizes the impact of the flexible straps 50 on drone landing. Specifically, after the flexible straps 50 are relaxed by the retractable assembly 60, the flexible straps 50 on either side of rectangular area A droop downward toward the corresponding second side rods 213, minimizing the vertical impact of the flexible straps 50 on drone landing and enhancing drone landing safety. Thus, by rationally arranging the retractable assembly 60, positioning markers, and first connectors 52 on the window frame 10 and window sash 20, the embodiments of the present application can improve drone landing safety at a low cost and with a relatively simple installation method.

[0068] In some embodiments, referring to Figures 10 to 15 , the window may further include a damping member 80 for providing damping to the window sash 20 during its rotation from the closed position to the rest position relative to the window frame 10. In such an embodiment, the window may not be provided with the flexible band 50 and the retractable assembly 60. Instead, the window may be capable of rotating from the closed position relative to the window frame 10 to the rest position under the action of gravity. During this rotation, the damping member 80 provides rotational damping, thereby enabling the window sash 20 to slowly rotate from the closed position to the rest position relative to the window frame 10.

[0069] In such an embodiment, since there is no need to provide the window sash 20 with a telescopic rod or a flexible belt 50 , the probability of damage to the drone can be further reduced, facilitating the landing of the drone.

[0070] In some embodiments, the damper 80 can be a coil spring damper 80, which is disposed at the junction of the lower first crossbar 12 and the first sidebar 13. One end of the rotating shaft 31 is connected to the coil spring damper 80, so that the rotating shaft 31 is damped by the coil spring during rotation. Because the coil spring damper 80 is disposed at the junction of the lower first crossbar 12 and the first sidebar 13, the coil spring damper 80 can provide a damping effect without affecting the landing of the drone.

[0071] Referring to Figure 16 , the coil spring damper 80 includes a coil spring seat 81 and a coil spring 82 disposed within the coil spring seat 81. The coil spring seat 81 has a retaining groove 811. An outer joint 821 of the coil spring 82, located radially outward, extends radially outward to engage with the retaining groove 811. The rotating shaft 31 also has a retaining groove. An inner joint 822 of the coil spring 82, located radially inward, extends radially inward to engage with the retaining groove of the rotating shaft 31.

[0072] When the window sash 20 is in the closed position, the plane on which the window sash 20 lies extends outwardly and tilted upward from bottom to top. Referring to Figure 12 , there is an angle α between the plane on which the window sash 20 lies and the vertical plane. In this embodiment, the center of gravity of the window sash 20 is unstable when in the closed position. Without the locking engagement portion 72 and the locking portion 71 securing the window sash 20 to the window frame 10, the window sash 20 can rotate outward to the rest position under its own weight.

[0073] The outer surface of the window frame 10 extends outwardly from bottom to top, and the inner surface of the window frame 10 (i.e., the side facing the room) is substantially located in a vertical plane. When the window sash 20 is in the closed position, the window sash 20 is substantially flush with the outer surface of the window frame 10, or slightly protrudes from the outer surface of the window frame 10.

[0074] 12 , the window may further include a counterweight 92 disposed above the window sash 20 to enable the window sash 20 to rotate from a closed position relative to the window frame 10 to a parked position under the action of gravity. The counterweight 92 may be disposed on the upper second crossbar 211 via a connector 93 .

[0075] In some embodiments, the locking portion 71 may be an electromagnetic lock. The electromagnetic lock includes an electromagnetic generator, a return spring, and a lock tongue. The locking mating portion 72 is provided with a lock hole. When the electromagnetic lock is powered on, the electromagnetic generator generates magnetism, attracting the lock tongue, which then withdraws from the lock hole, releasing the lock between the window sash 20 and the window frame 10. After the window sash 20 is closed, the electromagnetic lock is powered off, and the lock tongue, activated by the return spring, ejects and retracts into the lock hole, locking the window sash 20 and the window frame 10.

[0076] 17 and 18 , in some embodiments, the locking fitting portion 72 includes a lock seat 721 , a lock 723 , a pull pin 725 , a return spring 724 , and a return spring 726 .

[0077] The latch seat 721 is provided with a latch seat slot 722, and the latch 723 is slidably disposed in the latch seat slot 722. A lock hole 7231 is formed at one end of the latch 723 for engaging with the lock tongue of the locking portion 71; a return spring 724 is provided at the other end of the latch 723 for providing a force to the latch 723 to move toward the lock tongue. The latch 723 forms a latch slot 7232, and the latch seat 721 also forms a slot, through which a pull pin 725 can pass through the latch slot 7232 and enter the slot to secure the latch 723 in the latch seat slot 722. The pull pin 725 includes a head at each end and a connecting portion connecting the two ends. The connecting portion of the pull pin 725 is sleeved with a return spring 726 for providing a force to the pull pin 725 to engage with the slot.

[0078] Under normal circumstances, when the electromagnetic lock is powered on, the electromagnetic generator generates magnetism, attracting the lock tongue, which withdraws from the lock hole 7231, and the window sash 20 can automatically open. After the window sash 20 is closed, the electromagnetic lock is powered off, and the lock tongue pops out under the action of the return spring and inserts into the lock hole 7231, locking the window sash 20.

[0079] Under abnormal circumstances (e.g., a power outage), the pin 725 can be manually removed from the slot to activate the catch 723. Pulling the catch 723 in the opposite direction of the lock tongue (while the return spring 724 is compressed) disengages the catch 723 from the lock tongue, automatically opening the window sash 20. When the pin 725 and catch 723 are released, the return spring 724 resets the catch 723, and the pin 725 resets its socket under the action of the return spring 726.

[0080] When the window sash 20 needs to be closed, the pin 725 is manually pulled out of the slot to activate the lock catch 723. The lock catch 723 is then pulled in the opposite direction of the lock tongue (the return spring 724 is compressed at this time), causing the lock catch 723 to give way to the lock tongue. When the window sash 20 is completely closed, the pin 725 and lock catch 723 are released. The lock catch 723 extends under the action of the return spring 724 to engage with the lock tongue, and the pin 725 is inserted into the slot, locking the window sash 20.

[0081] 19 , in some embodiments, the window may further include: a processor 94 for receiving a window opening instruction from the drone 300 , and controlling the locking mating portion 72 and the locking portion 71 to unlock after receiving the window opening instruction.

[0082] The processor 94 is further configured to: receive a pairing request message sent by the drone 300 , the pairing request message including identity information; establish a connection with the drone 300 according to the identity information to receive a window opening instruction from the drone 300 .

[0083] In an embodiment of the present application, after pairing with a drone 300, the drone 300 can send a window opening command. The processor 94 energizes the electromagnetic lock according to the window opening command, causing the lock tongue to automatically leave the keyhole, achieving the purpose of automatically opening the window. In embodiments where the window does not have a flexible band 50 and a retractable assembly 60, the window sash 20 can be provided with a handle 91. When the lock tongue automatically leaves the keyhole, the window sash 20 automatically rotates outward to a parked position; the drone 300 then lands on the window sash 20 based on the positioning marker. After the drone 300 completes its mission, when the window needs to be closed, the user can manually close the window sash 20 using the handle 91.

[0084] In an embodiment where the window includes a flexible band 50 and a retractable assembly 60, the electromagnetic lock is powered on, the lock tongue automatically leaves the lock hole, and the drive motor 64 is activated, loosening the flexible band 50. The window sash 20 slowly opens under the action of gravity. After opening to the parking position, the drive motor 64 rotates a specified number of times and then automatically stops. The drone 300 lands on the window sash 20 according to the positioning marker. After completing its mission, the drone 300 flies away and issues a window closing command. Upon receiving the window closing command, the processor 94 activates the drive motor 64, retracting the flexible band 50 and slowly closing the window sash 20. The drive motor 64 rotates a specified number of times and then automatically stops. The processor 94 then de-energizes the electromagnetic lock, locking the window sash 20.

[0085] In some cases, when the drone 300 has a limited load capacity or emergency supplies are not located in the same location, the remote monitoring and emergency system 200 requires multiple drones 300 to deliver them separately. This can cause the drones 300 to arrive at their destinations at the same time. In this case, after the processor 94 establishes pairings with each drone 300 and the window sash 20 is opened, the drones 300 may interfere with each other and fail to land on the window sash 20, thereby extending the delivery time of the emergency supplies.

[0086] To address this situation, in some embodiments, the identification information of the drone 300 includes information about the emergency supplies it carries, and different landing priorities correspond to different emergency supplies. In some embodiments, the remote monitoring and emergency system 200 is in communication with the patient's monitoring device 400 and is able to obtain the patient's monitoring data from the monitoring device 400. When the remote monitoring and emergency system 200 dispatches two drones 300, each carrying emergency medicine and emergency equipment, the remote monitoring and emergency system 200 can determine the landing priority of the drone 300 carrying emergency medicine and the drone 300 carrying emergency equipment based on the patient's monitoring data when dispatching the drones 300. As can be easily understood, the drone 300 with the higher priority will land first.

[0087] The processor 94 is further configured to, upon receiving pairing requests from two or more drones 300 within a preset time interval, send a landing permission command to the drone 300 with the highest priority, and send a queue waiting command to the remaining drones 300, based on their landing priorities. A drone 300 that receives a landing permission command can then prepare to land, while a drone 300 that receives a queue waiting command can choose to hover or maneuver. This embodiment of the present application can determine the drone 300 that should land first based on the landing priority corresponding to the emergency supply information. This prevents interference between multiple drones 300 and delays in receiving emergency supplies, while also prioritizing the receipt of supplies most urgently needed by patients, thereby improving treatment outcomes.

[0088] In some embodiments, the preset time interval may be, for example, 1-2 minutes.

[0089] In some embodiments, the processor 94 is further configured to: after the currently landing drone 300 takes off, send a landing permission instruction to the drone 300 with the highest priority among the drones 300 waiting in line according to the landing priority.

[0090] In some embodiments, after receiving the takeoff information sent by the currently landing drone 300, the processor 94 determines that the currently landing drone 300 has taken off and can send a landing permission instruction to the drone 300 of the next priority.

[0091] The present invention also provides a method for stopping a drone 300 using a window according to the present invention. The method comprises: receiving a pairing request message from the drone 300, the pairing request message including identification information; establishing a connection with the drone 300 based on the identification information to receive a window opening command from the drone 300; upon receiving the window opening command from the drone 300, controlling the window sash 20 to rotate outward relative to the window frame 10 to a parking position parallel to the horizontal plane; and, when the window sash 20 rotates to the parking position, sending a landing permission command to the drone 300.

[0092] In some embodiments, the shutdown method further includes: when pairing request information is received from two or more drones 300 within a preset time interval, sending a landing permission instruction to the drone 300 with the highest priority according to the landing priority, and sending a queue waiting instruction to the other drones 300.

[0093] In some embodiments, the shutdown method further includes: after the currently landing drone 300 takes off, sending a landing permission instruction to the drone 300 with the highest priority among the drones 300 waiting in the queue according to the landing priority.

[0094] Regarding the embodiments of the present invention, it should also be noted that, in the absence of conflict, the embodiments of the present invention and the features therein may be combined with each other to obtain new embodiments.

[0095] The above are only specific embodiments of the present invention, but the protection scope of the present invention is not limited thereto. The protection scope of the present invention shall be based on the protection scope of the claims.

Claims

1. A window for docking a drone, comprising: window frame; A window sash, the lower end of which is hinged to the window frame, and the window sash can be rotated inwardly relative to the window frame to a closed position for closing the window frame and can be rotated outwardly relative to the window frame to a parking position parallel to a horizontal plane; as well as A stopper is arranged on the outer side of the window frame and is used to prevent the window sash from continuing to rotate when the window sash rotates to the stop position relative to the window frame.

2. The window according to claim 1, further comprising: at least one flexible band, each of said flexible bands being connected to said window sash; and a retracting and unfolding assembly, for retracting and unfolding the at least one flexible belt, When the retractable assembly retracts the at least one flexible belt, it can drive the window sash to rotate relative to the window frame to a closed position that closes the window frame; when the retractable assembly releases the at least one flexible belt, the window sash can rotate outward relative to the window frame to a parking position parallel to the horizontal plane to allow the drone to dock.

3. The window according to claim 2, wherein: The retracting and releasing assembly is configured to, when the window sash is in the parking position by releasing the at least one flexible band, continue to release the at least one flexible band so that the at least one flexible band can be in a relaxed state.

4. The window according to claim 2, wherein: The window sash comprises a frame and a glass plate installed inside the frame. Wherein, the flexible belt is connected to the frame through a first connecting member.

5. The window according to claim 4, wherein: The window frame comprises an upper first cross bar, a lower first cross bar and two first side bars respectively connected to the upper first cross bar and the lower first cross bar on the same side in a transverse direction; The frame comprises an upper second crossbar, a lower second crossbar and two second side bars respectively connected to the upper second crossbar and the lower second crossbar on the same side in the transverse direction, wherein the lower second crossbar is hinged to the lower first crossbar; The number of the flexible belts is two, and the two flexible belts are connected to the upper parts of the two second side rods through the two first connecting members respectively.

6. The window according to claim 5, wherein: The retractable assembly comprises: A rotating shaft, axial ends of which are rotatably disposed on the two first side rods of the window frame; and Two retractable wheels, one end of each flexible belt away from the first connecting member is wound around one of the retractable wheels, and the two retractable wheels are respectively coaxially connected to the rotating shaft to rotate together with the rotating shaft. Wherein, when the window sash is in the closed position, the projection contours of the two retracting and releasing wheels in the plane where the glass plate is located are respectively located within the projection contours of the two first side rods in the same plane.

7. The window according to claim 6, wherein: The retractable assembly also includes: A driving motor is arranged on the upper first crossbar; A first synchronous pulley, driven to rotate by the driving motor; A second synchronous pulley is sleeved on the middle part of the rotating shaft; and A synchronous belt is meshed with the first synchronous belt pulley and the second synchronous belt pulley, so that the first synchronous belt pulley drives the second synchronous belt pulley to rotate.

8. The window according to claim 6, wherein: The retractable assembly also includes: two second connecting members, respectively connected to the upper portions of the two first side rods; and Two bearings are respectively arranged on the two second connecting members, Wherein, the axial ends of the rotating shaft are respectively connected to the two bearings.

9. The window according to claim 1, further comprising: The damping member is used for providing damping to the window sash during the process of the window sash rotating from the closed position to the parking position relative to the window frame.

10. The window according to claim 1, wherein: When the window sash is in the closed position, the plane where the window sash is located extends obliquely outward from bottom to top.

11. The window according to claim 10, further comprising: A counterweight is arranged on the upper part of the window sash so that the window sash can rotate from the closed position to the parking position relative to the window frame under the action of gravity.

12. The window according to claim 1, wherein: The window sash is formed with at least one positioning mark for positioning the drone. When the window sash is in the parking position, the drone can be positioned according to the at least one positioning mark to dock on the window sash.

13. The window according to claim 1, wherein: The window frame is provided with a locking portion, and the window sash is provided with a locking matching portion. When the window sash is in a closed position, it can be locked with the window frame through the cooperation between the locking matching portion and the locking portion.

14. The window according to claim 13, further comprising: The processor is used to receive a window opening instruction of the drone, and control the locking matching part and the locking part to unlock after receiving the window opening instruction.

15. The window according to claim 14, wherein: The processor is further configured to: Receiving a pairing request message sent by the drone, wherein the pairing request message includes identity information; A connection is established with the drone according to the identity information to receive a window opening instruction from the drone.

16. The window according to claim 15, wherein: The drone carries first aid supplies, and the identity information also includes first aid supply information. Different first aid supply information corresponds to different landing priorities. The processor is also used to: when pairing request information of more than two drones is received within a preset time interval, send a landing permission instruction to the drone with the highest priority according to the landing priority, and send a queue waiting instruction to other drones.

17. The window according to claim 16, wherein the processor is further configured to: after the currently landing drone takes off, send a landing permission instruction to the drone with the highest priority among the drones waiting in line according to the landing priority.

18. A method for parking a drone, using the window according to any one of claims 1 to 17 for parking, the method comprising: Receiving a pairing request message sent by the drone, wherein the pairing request message includes identity information; Establishing a connection with the drone according to the identity information to receive a window opening instruction from the drone; When receiving a window opening command from the drone, controlling the window sash to rotate outward relative to the window frame to a parking position parallel to the horizontal plane; When the window sash rotates to the parking position, a landing permission instruction is sent to the drone.

19. The method according to claim 18, wherein: The drone carries emergency supplies, and the identification information also includes information about the emergency supplies carried. Different information about the emergency supplies carried corresponds to different landing priorities. The method further includes: when pairing request information of more than two drones is received within a preset time interval, according to the landing priority, sending a landing permission instruction to the drone with the highest priority, and sending a queue waiting instruction to other drones.

20. The method according to claim 19, further comprising: After the currently landing drone takes off, a landing permission instruction is sent to the drone with the highest priority among the drones waiting in line according to the landing priority.

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