A tethered flying flashlight

Abstract

The application discloses a tethered flying flashlight, which comprises a quick-release mechanism, a flying mechanism, a storage mechanism and a tethering mechanism. The quick-release mechanism comprises a quick-release shell and a first light-emitting device. The flying mechanism is detachably connected to the quick-release shell. The flying mechanism comprises a base device, a second light-emitting device and a flying device. The flying mechanism is arranged on the base device, and the second light-emitting device is arranged on the flying device. The flying mechanism is detachably stored in the storage mechanism. The tethering mechanism comprises a power supply box and a line wheel assembly. The line wheel assembly is installed in the power supply box, and the line wheel assembly is detachably connected to the flying mechanism. The tethered flying flashlight can provide illumination as a common flashlight in daily use. When high-altitude wide-area illumination is needed, the flying mechanism can be quickly detached, the flying device is unfolded, the second light-emitting device is used for illumination in the air, and the tethering mechanism is used for flexible deployment and quick winding, so that the flying mechanism can obtain continuous and stable power supply in a flying working state.

Description

Technical Field

[0001] This application relates to the field of lighting technology, and in particular to a tethered flying flashlight. Background Technology

[0002] Existing handheld lighting devices, such as ordinary flashlights, have a limited illumination range primarily due to the height and angle at which the user holds them, making it difficult to meet the lighting needs of large-area, high-altitude scenarios. In complex environments such as field searches, nighttime construction, or emergency rescue, traditional flashlights suffer from insufficient lighting efficiency and flexibility. To address this, some drone-based lighting products have entered the market; however, these devices are mostly independent structures, large in size, complex to operate, and have limited battery life, making them unable to hover stably for extended periods. Furthermore, existing lighting drones are typically not integrated with handheld devices, requiring separate operation and resulting in low carrying and deployment efficiency. In addition, most devices lack precise positioning and altitude control capabilities, making them unsuitable for applications requiring continuous, fixed-point lighting. Utility Model Content

[0003] This application aims to address at least one of the technical problems existing in the prior art. This application provides a tethered flying flashlight that integrates a portable flashlight with a high-altitude lighting drone, providing continuous power supply, precise positioning, and stable hovering illumination, thereby improving the flexibility and efficiency of lighting in complex environments.

[0004] The tethered flying flashlight according to an embodiment of this application includes: A quick-release mechanism, comprising a quick-release housing and a first light-emitting device, wherein the first light-emitting device is disposed within the quick-release housing; A flight mechanism, wherein the flight mechanism is detachably connected to the quick-release housing; A storage mechanism, wherein the flight mechanism can be detachably stored in the storage mechanism; A mooring mechanism, the mooring mechanism comprising a power supply box and a reel assembly, the reel assembly being disposed within the power supply box; The flight mechanism includes a base device, a second light-emitting device, and a flight device. The flight device is foldably mounted on the base device, the second light-emitting device is mounted on the flight device, and the reel assembly is detachably connected to the flight mechanism.

[0005] The tethered flying flashlight according to the embodiments of this application has at least the following beneficial effects: The tethered flying flashlight of this application includes a quick-release mechanism, a flying mechanism, a storage mechanism, and a tethering mechanism. The quick-release mechanism includes a quick-release housing and a first light-emitting device, which provides ground illumination. The quick-release housing serves as the head structure of the flashlight. The flying mechanism is detachably connected to the quick-release housing and includes a base device, a second light-emitting device, and the flying device itself. The base device is located below the flying mechanism, supporting it and engaging with the quick-release housing. The flying device has a foldable structure, allowing it to be compressed in its ground-operated state. The second light-emitting device is located on the flying device, providing high-altitude illumination during flight. The flying mechanism is detachably stored in the storage mechanism, which houses the flying mechanism and provides space protection. The tethering mechanism includes a power supply housing and a reel assembly. The reel assembly is installed inside the power supply housing and is detachably connected to the flying mechanism, supplying power to the flying mechanism.

[0006] The tethered flying flashlight of this application can provide illumination as a regular flashlight during daily use. When high-altitude wide-area illumination is required, the flying mechanism can be quickly disassembled, the flying device deployed, and the flight function activated, allowing the second light-emitting device to provide illumination in the air, thus increasing the illumination range and making it suitable for lighting needs in various complex scenarios. Flexible deployment and rapid retraction are achieved through the use of the power supply box and reel assembly, ensuring a continuous and stable power supply for the flying mechanism during flight operations.

[0007] According to some embodiments of this application, the flight device includes a fuselage fixing component, an arm assembly, and a rotor. The arm assembly is foldably disposed on the fuselage fixing component, the rotor is disposed on the arm assembly, and the second light-emitting device is disposed on the arm assembly.

[0008] According to some embodiments of this application, the arm assembly includes an arm component, a support component, and a drive component. The arm component is foldably mounted on the fuselage fixing component. The drive component and the support component are both fixedly connected to the arm component, and the rotor is connected to the drive component.

[0009] According to some embodiments of this application, the flight mechanism further includes a laser component, a flight control electronic speed controller (ESC), and a positioning component. The laser component and the ESC are disposed within the base device, and the positioning component is disposed on the flight device.

[0010] According to some embodiments of this application, the tethering mechanism further includes a power supply component, which includes a first power supply and a step-down module. Both the first power supply and the step-down module are disposed in the power supply box. The first power supply is connected to the step-down module, and the step-down module is connected to the reel assembly.

[0011] According to some embodiments of this application, the tethering mechanism further includes a third light-emitting device, which is connected to the step-down module.

[0012] According to some embodiments of this application, the quick-release housing is provided with at least two quick-release buttons, the base device is provided with at least two locking parts, and the quick-release buttons are detachably connected to the locking parts.

[0013] According to some embodiments of this application, the first light-emitting device includes a first fixing component, a light-emitting component, and a lens assembly. The first fixing component is disposed in the quick-release housing, the light-emitting component is fixedly disposed on the first fixing component, and the lens assembly is disposed on the quick-release housing.

[0014] According to some embodiments of this application, the storage mechanism includes a lower housing, a battery assembly, and a control component, wherein the battery assembly is disposed within the lower housing, and the control component is connected to the battery assembly.

[0015] According to some embodiments of this application, the battery assembly includes a second power source, a charging component, and a charging base. The charging base is disposed at the bottom end of the lower housing, the charging component is disposed on the charging base, the second power source is connected to the charging component, and the control component is disposed on the charging base. Attached Figure Description

[0016] The present application will be further described below with reference to the accompanying drawings and embodiments, wherein: Figure 1 This is a schematic diagram of the flight working state of a tethered flying flashlight according to an embodiment of this application; Figure 2 An exploded view of the quick-release mechanism of a tethered flying flashlight according to an embodiment of this application; Figure 3 This is an exploded schematic diagram of the flight mechanism of a tethered flying flashlight according to an embodiment of this application; Figure 4 An exploded view of the storage mechanism of a tethered flying flashlight according to an embodiment of this application; Figure 5 This is a schematic diagram of the tethering mechanism of a tethered flying flashlight according to an embodiment of this application; Figure 6 This is an exploded schematic diagram of the tethering mechanism of a tethered flying flashlight according to an embodiment of this application.

[0017] Figure label: Flight mechanism 1; outboard light panel 111; outboard light cover 112; long strip light panel 113; inner cover of the lampshade 114; light panel cover 115; base component 121; snap-fit ​​part 122; 6P interface 131; fuselage fixing component 132; arm component 133; support component 134; locking pressure plate 135; drive component 136; rotor 137; laser component 14; flight control ESC 15; first shock absorber ball 151; GPS positioning component 161; GPS outer cover 162; partition cover 163; second shock absorber ball 164; cable protection sleeve 17; conductive sheet 18; power supply light panel interface 19. Quick-release mechanism 2; First fixing component 21; Light-emitting component 22; Quick-release housing 23; Lens assembly 24; Lens sheet 241; Lens fixing component 242; Quick-release button 25; EVA plug 26; Storage mechanism 3; lower shell 31; second power supply 321; conductive plate 322; charging plate 323; charging interface 324; charging bottom shell 325; control component 33; plug 34; 4. Mooring mechanism; 411. Upper cover of the box; 412. Lower shell of the box; 413. Partition; 42. Wire wheel assembly; 43. First power supply; 44. Step-down module; 45. Third light-emitting device. Detailed Implementation

[0018] The embodiments of this application are described in detail below. Examples of these embodiments are shown in the accompanying drawings, wherein the same or similar reference numerals denote the same or similar elements or elements having the same or similar functions throughout. The embodiments described below with reference to the accompanying drawings are exemplary and are only used to explain this application, and should not be construed as limiting this application.

[0019] In the description of this application, it should be understood that the use of terms such as "center," "middle," "longitudinal," "transverse," "length," "width," "thickness," "upper," "lower," "front," "rear," "left," "right," "vertical," "horizontal," "top," "bottom," "inner," "outer," "axial," "radial," and "circumferential" to indicate orientation or positional relationships is based on the orientation or positional relationships shown in the accompanying drawings and is only for the convenience of describing this application and simplifying the description, and does not indicate or imply that the device or element referred to must have a specific orientation, or be constructed and operated in a specific orientation, and therefore should not be construed as a limitation of this application. Furthermore, features defined as "first" or "second" may explicitly or implicitly include one or more of that feature. In the description of this application, unless otherwise stated, "a plurality of" means two or more.

[0020] In the description of this application, it should be noted that, unless otherwise expressly specified and limited, the terms "installation," "connection," and "linking" should be interpreted broadly. For example, they can refer to a fixed connection, a detachable connection, or an integral connection; they can refer to a mechanical connection or an electrical connection; they can refer to a direct connection or an indirect connection through an intermediate medium; and they can refer to the internal connection between two components. Those skilled in the art can understand the specific meaning of the above terms in this application based on the specific circumstances.

[0021] The following reference Figures 1 to 6 Describes the tethered flying flashlight in the embodiments of this application.

[0022] according to Figures 1 to 6 As shown, an embodiment of this application of a tethered flying flashlight includes a quick-release mechanism 2, a flying mechanism 1, a storage mechanism 3, and a tethering mechanism 4. The quick-release mechanism 2 includes a quick-release housing 23 and a first light-emitting device. The quick-release housing 23 is the head of the flashlight, and the first light-emitting device is disposed within the quick-release housing 23, providing handheld illumination when in ground operation. The flying mechanism 1 is detachably connected to the quick-release housing 23. The flying mechanism 1 includes a base device, a flying device, and a second light-emitting device. The base device is disposed at the bottom of the flying mechanism 1 and supports the flying device. The flying mechanism 1 is detachably connected to the quick-release housing 23 via the base device. The flying device has a foldable structure and is foldably mounted on the base device. The second light-emitting device is disposed on the flying device and provides aerial illumination during flight operation. The storage mechanism 3 is used to store the flying mechanism 1. The storage mechanism 3 is a hollow housing, and the flying mechanism 1 can be stored within the hollow housing. The flying mechanism 1 is detachably connected to the storage mechanism 3. The tethering mechanism 4 includes a power supply box and a reel assembly 42. The power supply box is used to provide power. The reel assembly 42 is installed in the power supply box. The reel assembly 42 is detachably connected to the flight mechanism 1 and supplies power to the flight mechanism 1.

[0023] When in ground operation mode, the flying device folds inward to reduce its size and is stored in the storage mechanism 3. The quick-release mechanism 2, the flying mechanism 1 and the storage mechanism 3 are connected in sequence. It is used as a regular flashlight, and the first light-emitting device provides portable handheld lighting.

[0024] In flight operation mode, the flight mechanism 1 is removed from the storage mechanism 3, and the flight device unfolds outward to achieve flight, providing aerial illumination through the second light-emitting device. In flight operation mode, the flight mechanism 1 continuously receives power supply through the reel assembly 42 connected to the power supply box.

[0025] The tethered flying flashlight of this application achieves quick-release connection, folding storage, and functional integration in its structure. In daily use, it can be used as a regular flashlight, conveniently portable and easily placed in a pocket or backpack for ordinary flashlight illumination. When high-altitude lighting is required, the operator can quickly release the flying mechanism 1 via the quick-release mechanism 2, unfold the flying device, and take off, using a second light-emitting device to provide aerial illumination. The tethered flying flashlight effectively combines the portability of a flashlight with the wide-area lighting capabilities of a drone. With the power supply system of the tethering mechanism 4, it can achieve long-term hovering illumination, avoiding interruption of lighting missions due to battery depletion, overcoming the problem of insufficient battery life in traditional flying lighting equipment, and improving the device's endurance and practicality. The tethered flying flashlight of this application has advantages such as compact structure, convenient operation, diverse functions, and wide applicability, and is particularly suitable for complex application environments such as night patrols, field operations, and emergency search and rescue.

[0026] In some embodiments, the second light-emitting device includes a marker light panel 111, a marker light cover 112, a strip light panel 113, an inner cover 114, and a light panel cover 115. The marker light panel 111 is disposed on the outer side or edge of the flight device, and the marker light cover 112 fixes the marker light panel 111. The marker light panel 111 is used as a visual warning light or flight positioning reference. The strip light panel 113, the inner cover 114, and the light panel cover 115 are sequentially fixedly installed on the flight device. The strip light panel 113 is used for main aerial illumination.

[0027] according to Figures 1 to 6 As shown, in one embodiment of this application, the flight device specifically includes a fuselage fixing component 132, an arm assembly, and rotors 137. The fuselage fixing component 132 is located at the center of the flight device, serving as a support for the flight device. The arm assembly has a foldable structure and is foldably mounted on the fuselage fixing component 132. In ground operation, it can be folded inwards, and in flight operation, it can be unfolded outwards to a preset angle. Rotors 137 are mounted at the ends of the arm assembly. Each rotor 137 rotates to generate lift during flight operation, enabling hovering, takeoff, and directional control. A second light-emitting device is specifically mounted on the arm assembly, providing illumination. The flight device has a compact structure; the foldable arm assembly significantly reduces the storage volume, facilitating its inclusion in the storage mechanism 3. When unfolded, the arm assembly is securely positioned, improving flight stability.

[0028] In some embodiments, the second light-emitting device is integrated with the arm assembly, unifying the lighting and flight functions.

[0029] according to Figures 1 to 6As shown, in one embodiment of this application, the arm assembly includes an arm component 133, a support component 134, and a drive component 136. The support component 134 is disposed on the underside of the arm component 133 and is used to support the flight mechanism 1 during landing. It effectively distributes the weight of the aircraft, preventing the arm component 133 from directly contacting the ground and deforming or wearing down, thus improving the structural integrity and service life of the flight mechanism 1. The drive component 136 is fixedly mounted on the upper surface of the end of the arm component 133 and is used to drive the rotor 137 to rotate. The rotor 137 is mounted on the output shaft of the drive component 136 and rotates at high speed under the drive of the drive component 136, providing the upward thrust required for takeoff. While ensuring flight power output, the support component 134 enhances the load-bearing capacity of the flight mechanism 1 in ground conditions, reducing the risk of structural fatigue. This is particularly suitable for portable tethered flight lighting equipment with frequent takeoffs and landings and reusability requirements.

[0030] In some embodiments, the drive component 136 is configured as a motor drive component 136.

[0031] In some embodiments, the arm assembly further includes a locking plate 135, which, during flight preparation, causes the arm component 133 to rotate and extend outward to a horizontal position. The locking plate 135 locks and fixes the arm component 133, thereby improving stability and safety during flight.

[0032] In some embodiments, during flight operation, the arm component 133 is connected to the base component 121 via a 6P interface 131.

[0033] according to Figures 1 to 6 As shown, in one embodiment of this application, the flight mechanism 1 includes a laser component 14, a flight control electronic speed controller (ESC) 15, and a positioning component. The laser component 14 is installed within the base device and provides point-to-point pressure indication and laser ranging functions during flight operation, suitable for special application scenarios such as nighttime positioning and path guidance. The ESC 15 module is integrated within the base device and can control the rotor speed 137, attitude angle, and flight mode switching in real time, ensuring stable and reliable flight attitude. The positioning component is installed on the flight device and provides real-time coordinate information and altitude data, enabling the flight mechanism 1 to automatically hover, fly precisely, and prevent loss. By integrating the laser component 14, the ESC 15, and the positioning component into the flight mechanism 1, the tethered flying flashlight not only possesses conventional lighting and flight functions but also further achieves real-time control of flight attitude, high-precision positioning, and environmental awareness capabilities. The laser module enhances the device's indication and guidance capabilities at night or in harsh environments, while the ESC-15 flight control system improves the aircraft's stability and response speed, adapting to multiple flight modes. The positioning module effectively prevents the device from drifting or losing control, making it particularly suitable for applications requiring long-term stable hovering or fixed-point lighting, such as field rescue, emergency command, and nighttime monitoring.

[0034] In some embodiments, the flight mechanism 1 further includes a first shock-absorbing ball 151, and the laser component 14, flight control ESC 15, the first shock-absorbing ball 151 and the fuselage fixing component 132 are sequentially mounted on the base component 121.

[0035] In some embodiments, the positioning component includes a GPS positioning part 161 and a GPS cover 162. The GPS cover 162 is fixedly mounted on the body fixing part 132, and the GPS positioning part 161 is installed inside the body fixing part 132. In some embodiments, the positioning component further includes a partition cover 163 and a shock-absorbing ball. The partition cover 163, the second shock-absorbing ball 164, the GPS part, and the GPS cover 162 are sequentially mounted on the body fixing part 132.

[0036] In some embodiments, the flight mechanism 1 further includes a cable sheath 17, a conductive sheet 18, and a power supply lamp board interface 19.

[0037] according to Figures 1 to 6 As shown, in one embodiment of this application, the tethering mechanism 4 includes a power supply component, which includes a first power supply 43 and a step-down module 44, both housed within a power supply enclosure. The first power supply 43 is connected to the step-down module 44, providing a stable power supply to the tethering mechanism 4. The step-down module 44 is connected to the reel assembly 42, enabling it to stably output a stable current conforming to the operating voltage to the flight mechanism 1. By integrating an independent power supply component into the tethering mechanism 4, the flight mechanism 1 no longer relies on an onboard battery but is continuously powered by a ground power source, thereby significantly improving flight endurance. The step-down module 44 ensures stable and safe output voltage, avoiding voltage fluctuations affecting the flight control ESC 15 and the second lighting device, making it particularly suitable for mission scenarios requiring long-term continuous lighting, such as emergency lighting and nighttime search.

[0038] according to Figures 1 to 6 As shown, in one embodiment of this application, the tethering mechanism 4 includes a third light-emitting device 45, which is disposed on the outer shell of the power supply box and installed on the side of the box for easy observation by the operator. By providing the third light-emitting device 45 on the tethered power supply box, additional lighting support can be provided to the ground operator during the operation of the flight mechanism 1, improving the safety and ease of use of operation at night or in low light conditions, and is particularly suitable for complex operation scenarios such as nighttime emergency response and search and rescue dispatch.

[0039] In some embodiments, the power supply box is divided into a box top cover 411 and a box bottom shell 412. The box top cover 411 and the box bottom shell 412 are detachably connected. A partition 413 is also provided inside the box bottom shell 412. The first power supply 43, the step-down module 44 and the reel assembly 42 are all located on the lower side of the partition 413.

[0040] according to Figures 1 to 6 As shown, in one embodiment of this application, the quick-release housing 23 is provided with at least two quick-release buttons 25, and the base device is provided with at least two latching parts 122. The quick-release buttons 25 and the latching parts 122 correspond one-to-one, and the quick-release buttons 25 and the latching parts 122 are detachably connected.

[0041] In ground operation, the operator inserts the base device into the quick-release housing 23. The quick-release button 25 automatically engages upon contact with the latching part 122, locking the connection. For disassembly, pressing the two quick-release buttons 25 releases the base device, enabling quick release. This simple quick-release structure allows for rapid installation and release of the flight mechanism 1 simply by pressing the quick-release buttons 25, significantly improving mode switching efficiency. In scenarios such as emergency lighting and field inspections, operators can quickly deploy the UAV flight lighting module, enhancing response speed and operational convenience.

[0042] In some embodiments, the first fixing component 21 is provided with two EVA plugs 26.

[0043] according to Figures 1 to 6 As shown, in one embodiment of this application, it includes a first fixing component 21, a light-emitting component 22, and a lens assembly 24. The first fixing component 21 is disposed inside the front end of the quick-release housing 23 and is used to install the light-emitting component 22 to ensure the stability of the illumination. The light-emitting component 22 is fixed on the first fixing component 21. The lens assembly 24 is disposed at the very front end of the quick-release housing 23 and is used to regulate the light emitted by the light-emitting component 22 so that the output light has a suitable illumination distance and illumination angle.

[0044] In some embodiments, the lens assembly 24 includes a lens sheet 241 and a lens retainer 242, the lens retainer 242 securing the lens sheet 241 in the quick-release housing 23.

[0045] according to Figures 1 to 6 As shown, in one embodiment of this application, the storage mechanism 3 includes a lower housing 31, a battery assembly, and a control component 33. The battery assembly is disposed at the bottom end of the lower housing 31, and the control component 33 is disposed on the battery assembly. The control component 33 is used to control the opening and closing of the first light-emitting device when in ground-based working mode.

[0046] In some embodiments, both the lower housing 31 and the base component 121 are provided with threads, and the flight mechanism 1 and the storage unit are detachably connected by threads.

[0047] according to Figures 1 to 6As shown, in one embodiment of this application, the battery assembly includes a second power source 321, a charging component, and a charging base 325. The charging base 325 is disposed at the bottom end of the lower housing 31, providing an installation platform for the battery assembly. The charging component is disposed on the charging base 325, the second power source 321 is connected to the charging component, and the control component 33 is disposed on the charging base 325. By integrating charging, energy storage, and power supply into a single package, the tethered flying flashlight can be directly recharged through the charging interface 324 on the base, simplifying the operation process.

[0048] In some embodiments, the charging component includes a charging plate 323 and a charging interface 324, wherein the charging interface 324 may be configured as a USB-C interface or a magnetic interface.

[0049] In some embodiments, the power source includes a battery and two battery conductive plates 322, which are respectively disposed at both ends of the battery and are used to conduct electricity to the battery.

[0050] In some embodiments, a plug 34 is also provided on the charging base 325.

[0051] This application's tethered flying flashlight integrates a handheld flashlight and a flying device, employing a quick-release and folding storage structure to achieve flexible switching between ground-based flashlight lighting and high-altitude flight lighting, thus enhancing the tethered flying flashlight's adaptability to various scenarios. The tethering mechanism 4 provides a continuous and stable power supply to the flying device, effectively solving the problem of short battery life in traditional flight lighting equipment. The flying device is equipped with a GPS positioning component 161 and a laser component 14, enabling precise positioning and stable hovering, improving lighting accuracy and safety, and is particularly suitable for continuous lighting needs in complex environments such as emergency rescue, field operations, and night patrols.

[0052] In the description of this specification, the use of terms such as "an embodiment," "some examples," "some embodiments," "illustrative embodiment," "example," "specific example," or "some examples" indicates that a specific feature, structure, material, or characteristic described in connection with that embodiment or example is included in at least one embodiment or example of this application. In this specification, the illustrative expressions of the above terms do not necessarily refer to the same embodiment or example. Furthermore, the specific features, structures, materials, or characteristics described may be combined in any suitable manner in one or more embodiments or examples.

[0053] The embodiments of this application have been described in detail above with reference to the accompanying drawings. However, this application is not limited to the above embodiments. Within the scope of knowledge possessed by those skilled in the art, various changes can be made without departing from the spirit of this application.

Claims

1. A tethered flying flashlight, characterized in that: include A quick-release mechanism, comprising a quick-release housing and a first light-emitting device, wherein the first light-emitting device is disposed within the quick-release housing; A flight mechanism, wherein the flight mechanism is detachably connected to the quick-release housing; A storage mechanism, wherein the flight mechanism can be detachably stored in the storage mechanism; A mooring mechanism, the mooring mechanism comprising a power supply box and a reel assembly, the reel assembly being disposed within the power supply box; The flight mechanism includes a base device, a second light-emitting device, and a flight device. The flight device is foldably mounted on the base device, the second light-emitting device is mounted on the flight device, and the reel assembly is detachably connected to the flight mechanism.

2. The tethered flying flashlight according to claim 1, characterized in that: The flight device includes a fuselage fixing component, an arm assembly, and a rotor. The arm assembly is foldably mounted on the fuselage fixing component, the rotor is mounted on the arm assembly, and the second light-emitting device is mounted on the arm assembly.

3. The tethered flying flashlight according to claim 2, characterized in that: The arm assembly includes an arm component, a support component, and a drive component. The arm component is foldably mounted on the fuselage fixed component. The drive component and the support component are both fixedly connected to the arm component. The rotor is connected to the drive component.

4. The tethered flying flashlight according to claim 1, characterized in that: The flight mechanism also includes a laser component, a flight control electronic speed controller (ESC), and a positioning component. The laser component and the ESC are disposed within the base device, and the positioning component is disposed on the flight device.

5. The tethered flying flashlight according to claim 1, characterized in that: The mooring mechanism also includes a power supply component, which includes a first power supply and a step-down module. Both the first power supply and the step-down module are located inside the power supply box. The first power supply is connected to the step-down module, and the step-down module is connected to the reel assembly.

6. The tethered flying flashlight according to claim 5, characterized in that: The tethering mechanism also includes a third light-emitting device, which is connected to the step-down module.

7. The tethered flying flashlight according to claim 1, characterized in that: The quick-release housing is provided with at least two quick-release buttons, and the base device is provided with at least two locking parts. The quick-release buttons are detachably connected to the locking parts.

8. The tethered flying flashlight according to claim 1, characterized in that: The first light-emitting device includes a first fixing component, a light-emitting component, and a lens assembly. The first fixing component is disposed in the quick-release housing, the light-emitting component is fixedly disposed on the first fixing component, and the lens assembly is disposed on the quick-release housing.

9. The tethered flying flashlight according to claim 1, characterized in that: The storage mechanism includes a lower housing, a battery assembly, and a control component. The battery assembly is disposed inside the lower housing, and the control component is connected to the battery assembly.

10. The tethered flying flashlight according to claim 9, characterized in that: The battery assembly includes a second power source, a charging component, and a charging base. The charging base is disposed at the bottom end of the lower housing, the charging component is disposed on the charging base, the second power source is connected to the charging component, and the control component is disposed on the charging base.

Images