Flying elevator

Abstract

A flying elevator is characterized by comprising (100) a ducted propeller arrangement. And (200) a flying elevator telescopic car body. And (300) supplying power to the transfer platform truck. And (400) an intelligent control system. And (500) final assembly of the structure. The mechanisms and the systems are combined through final assembly. Therefore, a set of economical and practical elevator type intelligent low-altitude aircraft is formed. The technical problem that a conventional low-altitude aircraft cannot be connected for a long time to continuously work and cannot be increased in capacity due to limitation of self-loading power or electric power is solved. The elevator is widely applied to high-rise buildings, high-altitude construction sites, disaster areas and scenic areas and serves as a temporary elevator or a short-distance aircraft. And the emergency operation and rescue work of personnel transfer and material transportation can be continuously carried out by a single machine for a long time. The flying elevator has the beneficial effects that 1, the flying elevator flies with lines, and electric power is continuously provided by using the mains supply or a vehicle-mounted power generation device, so that the flying elevator can continuously run for a long time; 2, off-line flight: driving the flight elevator to run by utilizing a reserve battery in an area which is not suitable for line-carried flight; and emergency operation and rescue work in different environments are facilitated. And 3, a multi-set mechanical structure design, a power supply device and a control system. And flight safety and operation convenience are guaranteed.

Description

Technical Field

[0001] This invention relates to a low-altitude aircraft, and more particularly to an elevator-type intelligent low-altitude aircraft. Background Technology

[0002] The development of the low-altitude economy is still in its initial stage. However, it is progressing rapidly, supported by national policies and supported by continuous research and development investment from enterprises and institutions.

[0003] However, truly mature products that have achieved large-scale operation are still rare, especially heavy-duty electric aircraft. Most are still in the research and development or test flight stage. Due to limitations in current energy storage technology, heavy-duty electric aircraft capable of long-duration, continuous flight are still scarce.

[0004] This invention aims to supplement the intelligent products needed for the development of the low-altitude economy, filling a market gap. It proposes a low-cost, long-term, continuous-operation flying elevator to meet future market demands. Summary of the Invention

[0005] Technical issues: To address the technical challenges of conventional low-altitude aircraft, which are limited by their own power or electricity, preventing continuous long-term operation and increased payload capacity, the market demands a low-altitude aircraft that can be widely used in high-rise buildings, high-altitude construction sites, disaster areas, and scenic spots as a temporary elevator or short-range aircraft for long-term continuous personnel transfer and material transport in emergency operations and rescue work. This invention proposes an economical and practical technical solution: a flying elevator. Technical solution

[0006] A flying elevator.

[0007] 1. A flying elevator characterized by: (100) a ducted propeller device; (200) a telescopic flying elevator cabin; (300) a power transfer platform vehicle; (400) an intelligent control system; and (500) final assembly. These mechanisms and systems are assembled to form an economical and practical elevator-type intelligent low-altitude flying vehicle. This solves the technical problem that conventional low-altitude flying vehicles are limited by their own power or electricity, making it impossible to operate continuously for a long time and increase their load capacity. It is widely used in high-rise buildings, high-altitude construction sites, disaster areas, and scenic spots as a temporary elevator or short-distance flying vehicle, enabling long-term continuous personnel transfer, material transportation, emergency operations, and rescue work.

[0008] 2. The flying elevator according to claim 1 is characterized by: a (100) ducted propeller assembly component in the mechanism (as shown in the attached diagram). Figure 1(As shown): (101) Built-in motor rotating folding wing module. (102) Folding wing module connecting rod. (103) Built-in motor ducted propeller forward and reverse steering module. (104) Duct connecting clamp. (105) Built-in motor ducted propeller side steering module. (106) Tubular duct. (107) Tubular duct and built-in motor shaft module connector. (108) Propeller built-in motor shaft module. (109) Multi-bladed double-layer propeller. Connection method: (101) The built-in motor rotating folding wing module is installed on the (212) ducted propeller device mounting base. It is fixed by tightening screws and nuts. (102) The folding wing module connecting rod is installed between (101) the built-in motor rotating folding wing module and (103) the built-in motor ducted propeller forward and reverse steering module. (104) The duct connecting clamp is installed on the (103) built-in motor duct propeller forward and reverse steering module (103). Two sets of (105) built-in motor duct propeller side steering modules are respectively installed on the inner ends of the (104) duct connecting clamp. (106) The tubular duct is installed on the inner side of the two sets of (105) built-in motor duct propeller side steering modules. Each module is locked and fixed by corresponding fasteners. (107) The tubular duct and built-in motor shaft module connector is welded to connect the (106) tubular duct to the (108) propeller built-in motor shaft module. (109) The multi-bladed double-layer propeller is installed on both ends of the (108) propeller built-in motor shaft module shell. It is fixed by riveting.

[0009] 3. The flying elevator according to claim 1 is characterized by: (200) the flying elevator telescopic cabin component (as shown in the attached diagram). Figure 2(As shown): (201) Main compartment. (202) Sub-compartment. (203) Sub-compartment slide rail device. (204) Sub-compartment telescopic electric push rod. (205) Vacuum adsorption fixing module. (206) Vacuum adsorption fixing module slide rail device. (207) Vacuum adsorption fixing module electric push rod. (208) Main compartment bridging door cover. (209) Main compartment bridging door cover electric roller device. (210) Main compartment landing foot. (211) Sub-compartment telescopic moving wheel. (212) Duct propeller device mounting base. Connection method: (202) The sub-compartment is fitted inside the (201) main compartment. It is connected through the (203) sub-compartment slide rail device. (203) The auxiliary compartment slide rail device is installed on both sides of the (201) main compartment. (202) The auxiliary compartment is installed on the (203) auxiliary compartment slide rail device. (204) The auxiliary compartment telescopic electric push rod is installed between the (201) main compartment and the top of the (203) auxiliary compartment slide rail device. (205) The vacuum adsorption fixing module is installed on the (206) vacuum adsorption fixing module slide rail device. (207) The vacuum adsorption fixing module electric push rod is installed between the (201) main compartment and the top of the (206) vacuum adsorption fixing module slide rail device. (208) The main compartment bridging door cover is installed at the outer opening of the (201) main compartment, and the bottom is connected by a rotating hinge. Two sets of (209) main compartment bridging door cover electric roller devices are installed between the (201) main compartment and the (208) main compartment bridging door cover on each side. Four sets (210) of main body landing feet are installed at the four corners of the bottom of the (201) main body. (211) The auxiliary body telescopic moving wheels are located at both ends of the bottom of the (202) auxiliary body opening. Various mechanisms are riveted or locked with corresponding fasteners, and eight sets (212) of duct propeller device mounting seats are welded to the top of the (201) main body and the top of the (202) auxiliary body respectively.

[0010] 4. The flying elevator according to claim 1 is characterized by: a power supply transfer platform vehicle component (300) in the mechanism (as shown in the attached diagram). Figure 3 (301) Transfer electric vehicle. (302) Electric vehicle operator's cab. (303) Flying elevator cable winding device. (304) Flying elevator landing platform automatic leveling device. (305) Flying elevator landing platform. (306) Cable winding device cable stretching dynamic detection module.

[0011] Connection method: (302) The electric vehicle operator's cab is located at the front end of the (301) transfer electric vehicle. (303) The flying elevator cable winding device is located at the rear end of the (301) transfer electric vehicle carriage. (304) The flying elevator landing platform automatic leveling device is located above the (301) transfer electric vehicle carriage. (305) The flying elevator landing platform is located above the (304) flying elevator landing platform automatic leveling device. (306) The cable winding device cable stretching dynamic detection module is located at the rear end of the (303) flying elevator cable winding device. Installation and fixation are carried out according to the designed workstations using corresponding fasteners for locking or welding.

[0012] 5. The flying elevator according to claim 1 is characterized by: a (400) intelligent control system component in the mechanism (as shown in the attached diagram). Figure 4 (401) Overall control system. (402) Flight control device. (403) Ground control device. (404) Unmanned driving system. (405) Heading and attitude balance system. (406) Sensor ranging and visual monitoring system. (407) Offline dual-power battery for flight. (408) Offline dual-power battery automatic switcher for flight. (409) Vehicle-mounted dual-power aluminum-air battery power station. (410) Vehicle-mounted dual-power aluminum-air battery power station automatic switcher. (411) Mains power interface. (412) Automatic interface for flight elevator with wired flight cable. (413) Power control system. (414) Power detection system. (415) Power detection system.

[0013] Connection method: (401) The central control system and (403) the ground control device are respectively installed in the (302) electric vehicle operating room. (409) The vehicle-mounted dual-power aluminum-air battery power station, (410) the vehicle-mounted dual-power aluminum-air battery power station automatic power switch and (411) the mains power interface are installed in the 301 transfer electric vehicle compartment. (402) The flight control device, (407) the offline flight dual-power battery and (408) the offline flight dual-power battery automatic switch are respectively installed on the top of the (201) flight elevator main body. (412) The flight elevator wired flight cable automatic interface is installed at the bottom of the (201) flight elevator main body. Other ranging and vision hardware are installed on the outside of the (200) flight elevator body. (401) serves as the central control system and interfaces with all branch modules of the present invention. (409) provides power for all devices and modules of the present invention. (408) provides power for all devices and modules on the flight elevator during offline flight. Each control system and sensing system interfaces with its respective equipment and devices, and is connected via remote control modules, wires, cables, and hoses.

[0014] 6. The flying elevator according to claim 1 is characterized by: (500) final assembly. Components (as shown in the attached document) Figure 5 (100) Ducted propeller assembly. (200) Telescopic flying elevator cabin. (300) Power supply transfer platform vehicle.

[0015] Connection method: Eight sets of (100) ducted propeller units are installed above the (200) telescopic flight elevator cabin. The (200) telescopic flight elevator cabin rests above the (300) power supply transfer platform vehicle. When flying with the power cord connected, the power supply from the (300) power supply transfer platform vehicle to the flight elevator is supplied via cable. When offline flight is required, the control system automatically disconnects the power supply cable from the flight elevator.

[0016] Working principle: The telescopic elevator cabin and power supply transfer platform are effectively combined through a ducted propeller system. Eight ducted propellers provide power to the elevator, enabling it to perform the necessary movements for lifting, moving up, down, left, right, turning, and hovering. The telescopic elevator cabin is powered by electric push rods, allowing it to extend and retract to change its spatial dimensions. The vacuum adsorption fixing module, powered by electric push rods and vacuum suction cups, secures the elevator cabin to the wall. The main cabin's bridging door is opened and closed by an electric reel that winds a chain. During cable-driven flight, the cable winding device uses an electric drum to wind and unwind the power cable. When the elevator needs to land on the power supply transfer platform, the platform leveling device, guided by a leveling instrument, uses electric push rods at the four corners of the platform to level it, ensuring a safe landing. The power transfer platform vehicle is equipped with an onboard dual-power aluminum-air battery power station, or connects to the mains power supply via an interface, to provide continuous power for the flying elevator during long-term operation. When the elevator is offline, the dual-power battery provides power for offline operation. Separate power switching devices ensure uninterrupted power supply. Various control and monitoring systems provide intelligent implementation guarantees for the normal and safe operation of the flying elevator.

[0017] The beneficial effects of this invention are: 1. The flying elevator operates continuously for extended periods by using mains power or onboard generators to provide a constant supply of electricity.

[0018] 2. Offline flight: The flying elevator is powered by reserve batteries in areas where tethered flight is not feasible. This is beneficial for emergency operations and rescue work in various environments.

[0019] 3. The cargo space is retractable. When air transport is needed, the cargo compartment can be extended to increase cargo space and transport longer items. For example, it can be used to transport long items that cannot fit in a conventional elevator in a high-rise building. When not in use, the cargo compartment can be retracted for easy transfer to a vehicle.

[0020] 4. The main structure of the container is equipped with a vacuum wall-gripping stabilizer to secure the container. This facilitates personnel getting on and off the elevator and loading and unloading goods.

[0021] 5. The ducted propeller is equipped with a rotating and retractable fin function. It unfolds during flight to increase propulsion. When not in flight, it retracts above the cabin for easy transport by vehicle.

[0022] 6. Targeted environmental application design. Avoids many unnecessary reserve functions and adaptive designs, significantly and effectively reducing product manufacturing costs and facilitating product popularization, promotion, and application.

[0023] 7. Vehicle-mounted transfer. This ensures the safe and long-term power supply to the flying elevator while avoiding the hassle of applying for various unnecessary flight routes.

[0024] 8. Multiple sets of mechanical structure design and power supply devices, as well as control systems, ensure flight safety and ease of operation. Attached Figure Description

[0025] To more clearly illustrate the technical solutions in the embodiments of the present invention or the prior art, the drawings used in the embodiments will be briefly introduced below. Obviously, the drawings described below are only some embodiments of the present invention. For those skilled in the art, other drawings can be obtained based on these drawings without creative effort.

[0026] Schematic diagram of mechanism and component names: Figure 1 (100) Ducted propeller assembly 101. Built-in motor rotating folding wing module.

[0027] 102. Folding Module Connecting Rod.

[0028] 103. Built-in motor ducted propeller forward and reverse steering module.

[0029] 104. Folding connection clamp.

[0030] 105. Built-in motor ducted propeller side steering module.

[0031] 106. Tubular duct.

[0032] 107. Connector between tubular channel and built-in motor shaft module.

[0033] 108. Propeller with built-in motor shaft module.

[0034] 109. Multi-bladed double-layer propeller.

[0035] Figure 2 , (200) Flying elevator telescopic cabin.

[0036] 201. Main compartment.

[0037] 202. Secondary compartment.

[0038] 203. Sub-body slide rail device.

[0039] 204. Electric push rod for telescopic movement of the auxiliary compartment.

[0040] 205. Vacuum adsorption fixation module.

[0041] 206. Vacuum adsorption fixing module slide rail device.

[0042] 207. Electric push rod for vacuum adsorption fixing module.

[0043] 208. Main compartment with bridging door cover.

[0044] 209. Main compartment bridging door cover electric roller device.

[0045] 210. Main compartment landing feet.

[0046] 211. Telescopic casters for the auxiliary compartment.

[0047] 212. Mounting base for ducted propeller assembly.

[0048] (Note 203, 204, 206, 207, 209 are installed on the inside of the compartment).

[0049] Figure 3 , (300) Power supply transfer platform vehicle.

[0050] 301. Transfer of electric vehicles.

[0051] 302. Electric vehicle operator's cab.

[0052] 303. Flying elevator cable winding device.

[0053] 304. Automatic leveling device for the landing platform of the flying elevator.

[0054] 305. Flying elevator landing platform.

[0055] 306. Cable winding device, dynamic detection module for cable stretching.

[0056] Figure 4 , (400) Intelligent control system.

[0057] 401. Central control system.

[0058] 402. Flight control device.

[0059] 403. Ground control device.

[0060] 404. Autonomous driving system.

[0061] 405. Heading and attitude balance system.

[0062] 406. Sensor-based distance vision monitoring system.

[0063] 407. Offline flight dual-power battery.

[0064] 408. Offline flight dual-power battery automatic switcher.

[0065] 409. Vehicle-mounted dual-power aluminum-air battery power station.

[0066] 410. Vehicle-mounted dual-power aluminum-air battery power station automatic power switch.

[0067] 411. Mains power interface.

[0068] 412. Automatic interface for flight elevator with cable.

[0069] 413. Power control system.

[0070] 414. Power detection system.

[0071] 415. Power detection system.

[0072] Figure 5 , (500) assembly.

[0073] 100. Ducted propeller assembly.

[0074] 200. Telescopic flying elevator cabin.

[0075] 300. Power supply transfer platform vehicle. Detailed Implementation

[0076] Obviously, the described embodiments are only some embodiments of the present invention, and not all embodiments. All other embodiments obtained by those skilled in the art based on the embodiments of the present invention are also part of the present invention. The accompanying drawings of the embodiments of the present invention clearly and completely illustrate the technical solutions of the embodiments of the present invention.

[0077] The working principle of this invention is as follows: 1. The (100) ducted propeller assembly components in the mechanism (as shown in the attached document) Figure 1(As shown): (101) Built-in motor rotating folding wing module. (102) Folding wing module connecting rod. (103) Built-in motor ducted propeller forward and reverse steering module. (104) Duct connecting clamp. (105) Built-in motor ducted propeller side steering module. (106) Tubular duct. (107) Tubular duct and built-in motor shaft module connector. (108) Propeller built-in motor shaft module. (109) Multi-bladed double-layer propeller. Connection method: (101) The built-in motor rotating folding wing module is installed on the (212) ducted propeller device mounting base. It is fixed by tightening screws and nuts. (102) The folding wing module connecting rod is installed between (101) the built-in motor rotating folding wing module and (103) the built-in motor ducted propeller forward and reverse steering module. (104) The duct connecting clamp is installed on the (103) built-in motor duct propeller forward and reverse steering module (103). Two sets of (105) built-in motor duct propeller side steering modules are respectively installed on the inner ends of the (104) duct connecting clamp. (106) The tubular duct is installed on the inner side of the two sets of (105) built-in motor duct propeller side steering modules. Each module is locked and fixed by corresponding fasteners. (107) The tubular duct and built-in motor shaft module connector is welded to connect the (106) tubular duct to the (108) propeller built-in motor shaft module. (109) The multi-bladed double-layer propeller is installed on both ends of the (108) propeller built-in motor shaft module shell. It is fixed by riveting.

[0078] 2. The (200) telescopic cabin component of the flight elevator in the mechanism (as shown in the attached document) Figure 2 (As shown): (201) Main compartment. (202) Sub-compartment. (203) Sub-compartment slide rail device. (204) Sub-compartment telescopic electric push rod. (205) Vacuum adsorption fixing module. (206) Vacuum adsorption fixing module slide rail device. (207) Vacuum adsorption fixing module electric push rod. (208) Main compartment bridging door cover. (209) Main compartment bridging door cover electric roller device. (210) Main compartment landing foot. (211) Sub-compartment telescopic moving wheel. (212) Duct propeller device mounting base.

[0079] Connection method: (202) The auxiliary compartment is fitted inside the (201) main compartment. It is connected by the (203) auxiliary compartment slide rail device. The (203) auxiliary compartment slide rail device is installed on both sides of the (201) main compartment, the (202) auxiliary compartment is installed on the (203) auxiliary compartment slide rail device, and the (204) auxiliary compartment telescopic electric push rod is installed between the (201) main compartment and the top of the (203) auxiliary compartment slide rail device. (205) The vacuum adsorption fixing module is installed on the (206) vacuum adsorption fixing module slide rail device. (207) The vacuum adsorption fixing module electric push rod is installed between the (201) main compartment and the top of the (206) vacuum adsorption fixing module slide rail device. (208) The main compartment bridging door cover is installed at the outer opening of the (201) main compartment, and the bottom is connected by a rotating hinge. Two sets of (209) main body bridging door cover electric roller devices are installed between the two sides of the (201) main body and the (208) main body bridging door cover. Four sets of (210) main body landing feet are installed at the four corners of the bottom of the (201) main body. (211) Auxiliary body telescopic moving wheels are located at both ends of the bottom of the (202) auxiliary body exterior opening. Various mechanisms are riveted or locked with corresponding fasteners, and eight sets of (212) duct propeller device mounting seats are welded to the top of the (201) main body and the top of the (202) auxiliary body respectively.

[0080] 3. The (300) power supply transfer platform vehicle components in the organization (as shown in the attached document) Figure 3 (301) Transfer electric vehicle. (302) Electric vehicle operator's cab. (303) Flying elevator cable winding device. (304) Flying elevator landing platform automatic leveling device. (305) Flying elevator landing platform. (306) Cable winding device cable stretching dynamic detection module.

[0081] Connection method: (302) The electric vehicle operator's cab is located at the front end of the (301) transfer electric vehicle. (303) The flying elevator cable winding device is located at the rear end of the (301) transfer electric vehicle carriage. (304) The flying elevator landing platform automatic leveling device is located above the (301) transfer electric vehicle carriage. (305) The flying elevator landing platform is located above the (304) flying elevator landing platform automatic leveling device. (306) The cable winding device cable stretching dynamic detection module is located at the rear end of the (303) flying elevator cable winding device. Installation and fixation are carried out according to the designed workstations using corresponding fasteners for locking or welding.

[0082] 4. Components of the (400) intelligent control system in the mechanism (as shown in the appendix) Figure 4(401) Overall control system. (402) Flight control device. (403) Ground control device. (404) Unmanned driving system. (405) Heading and attitude balance system. (406) Sensor ranging and visual monitoring system. (407) Offline dual-power battery for flight. (408) Offline dual-power battery automatic switcher for flight. (409) Vehicle-mounted dual-power aluminum-air battery power station. (410) Vehicle-mounted dual-power aluminum-air battery power station automatic switcher. (411) Mains power interface. (412) Automatic interface for flight elevator with wired flight cable. (413) Power control system. (414) Power detection system. (415) Power detection system.

[0083] Connection method: (401) The central control system and (403) the ground control device are respectively installed in the (302) electric vehicle operating room. (409) The vehicle-mounted dual-power aluminum-air battery power station, (410) the vehicle-mounted dual-power aluminum-air battery power station automatic power switch and (411) the mains power interface are installed in the 301 transfer electric vehicle compartment. (402) The flight control device, (407) the offline flight dual-power battery and (408) the offline flight dual-power battery automatic switch are respectively installed on the top of the (201) flight elevator main body. (412) The flight elevator wired flight cable automatic interface is installed at the bottom of the (201) flight elevator main body. Other ranging and vision hardware are installed on the outside of the (200) flight elevator body. (401) serves as the central control system and interfaces with all branch modules of the present invention. (409) provides power for all devices and modules of the present invention. (408) provides power for all devices and modules on the flight elevator during offline flight. Each control system and sensing system interfaces with its respective equipment and devices, and is connected via remote control modules, wires, cables, and hoses.

[0084] 5. (500) Final Assembly. Components (as shown in the attached document) Figure 5 (100) Ducted propeller assembly. (200) Telescopic flying elevator cabin. (300) Power supply transfer platform vehicle.

[0085] Connection method: Eight sets of (100) ducted propeller units are installed above the (200) telescopic flight elevator cabin. The (200) telescopic flight elevator cabin rests above the (300) power supply transfer platform vehicle. When flying with the power cord connected, the power supply from the (300) power supply transfer platform vehicle to the flight elevator is supplied via cable. When offline flight is required, the control system automatically disconnects the power supply cable from the flight elevator.

[0086] The telescopic elevator cabin and power supply transfer platform are effectively combined through a ducted propeller system. Eight ducted propellers provide power to the elevator, enabling it to perform the necessary movements for lifting, moving up, down, left, right, turning, and hovering. The telescopic elevator cabin is powered by electric push rods, allowing it to extend and retract to change its spatial dimensions. The vacuum adsorption fixing module, powered by electric push rods and vacuum suction cups, secures the elevator cabin to the wall. The main cabin's bridging door is opened and closed by an electric reel that winds a chain. During cable-driven flight, the cable winding device uses an electric drum to wind and unwind the power cable. When the elevator needs to land on the power supply transfer platform, the platform leveling device, guided by a leveling instrument, uses electric push rods at the four corners of the platform to level it, ensuring a safe landing. The power transfer platform vehicle is equipped with an onboard dual-power aluminum-air battery power station, or connects to the mains power supply via an interface, to provide continuous power for the flying elevator during long-term operation. When the elevator is offline, the dual-power battery provides power for offline operation. Separate power switching devices ensure uninterrupted power supply. Various control and monitoring systems provide intelligent implementation guarantees for the normal and safe operation of the flying elevator.

[0087] The beneficial effects of this invention are: 1. The flying elevator operates continuously for extended periods by using mains power or onboard generators to provide a constant supply of electricity.

[0088] 2. Offline flight: The flying elevator is powered by reserve batteries in areas where tethered flight is not feasible. This is beneficial for emergency operations and rescue work in various environments.

[0089] 3. The cargo space is retractable. When air transport is needed, the cargo compartment can be extended to increase cargo space and transport longer items. For example, it can be used to transport long items that cannot fit in a conventional elevator in a high-rise building. When not in use, the cargo compartment can be retracted for easy transfer to a vehicle.

[0090] 4. The main structure of the container is equipped with a vacuum wall-gripping stabilizer to secure the container. This facilitates personnel getting on and off the elevator and loading and unloading goods.

[0091] 5. The ducted propeller is equipped with a rotating and retractable fin function. It unfolds during flight to increase propulsion. When not in flight, it retracts above the cabin for easy transport by vehicle.

[0092] 6. Targeted environmental application design. Avoids many unnecessary reserve functions and adaptive designs, significantly and effectively reducing product manufacturing costs and facilitating product popularization, promotion, and application.

[0093] 7. Vehicle-mounted transfer. This ensures the safe and long-term power supply to the flying elevator while avoiding the hassle of applying for various unnecessary flight routes.

[0094] 8. Multiple sets of mechanical structure design and power supply devices, as well as control systems, ensure flight safety and ease of operation.

Claims

1. A flying elevator characterized by: (100) Ducted propeller unit. (200) Telescopic flying elevator cabin. (300) Power supply transfer platform vehicle. (400) Intelligent control system. (500) Final assembly. These mechanisms and systems are assembled to form an economical and practical elevator-type intelligent low-altitude aircraft. This solves the technical problem that conventional low-altitude aircraft are limited by their own power or electricity, making it impossible to operate continuously for a long time and increase their load capacity. It is widely used in high-rise buildings, high-altitude construction sites, disaster areas, and scenic spots as a temporary elevator or short-distance aircraft, enabling long-term continuous personnel transfer, material transportation, emergency operations, and rescue work.

2. The flying elevator according to claim 1 is characterized by the following components in the (100) ducted propeller device (as shown in Figure 1): (101) Built-in motor rotating folding wing module; (102) Folding wing module connecting rod; (103) Built-in motor ducted propeller forward and reverse steering module; (104) Duct connecting clamp; (105) Built-in motor ducted propeller side steering module; (106) Tubular duct; (107) Tubular duct and built-in motor shaft module connector; (108) Propeller built-in motor shaft module; (109) Multi-bladed double-layer propeller. Connection method: The (101) built-in motor rotating folding wing module is installed on the (212) ducted propeller device mounting base. It is fixed by tightening screws and nuts. (102) The folding wing module connecting rod is installed between the (101) built-in motor rotating folding wing module and the (103) built-in motor ducted propeller forward and reverse steering module. (104) The duct connecting clamp is installed on the (103) built-in motor ducted propeller forward and reverse steering module (103). Two sets of (105) built-in motor ducted propeller side steering modules are respectively installed on the inner ends of the (104) duct connecting clamp. (106) The tubular duct is installed inside the two sets of (105) built-in motor ducted propeller side steering modules. Each module is locked and fixed by corresponding fasteners. (107) The tubular duct and the built-in motor shaft module connecting piece are connected by welding to the (106) tubular duct and the (108) propeller built-in motor shaft module. (109) The multi-bladed double-layer propeller is installed on both ends of the (108) propeller built-in motor shaft module shell. It is fixed by riveting.

3. The flying elevator according to claim 1 is characterized by the following components in the mechanism: (200) the telescopic cabin of the flying elevator (as shown in Figure 2): (201) main cabin; (202) auxiliary cabin; (203) auxiliary cabin slide rail device; (204) auxiliary cabin telescopic electric push rod; (205) vacuum adsorption fixing module; (206) vacuum adsorption fixing module slide rail device; (207) vacuum adsorption fixing module electric push rod; (208) main cabin bridging door cover; (209) main cabin bridging door cover electric roller device; (210) main cabin landing foot; (211) auxiliary cabin telescopic moving wheel; (212) duct propeller device mounting base. Connection method: (202) the auxiliary cabin is fitted inside the (201) main cabin. It is connected by the (203) auxiliary cabin slide rail device. (203) The auxiliary compartment slide rail device is installed on both sides of the (201) main compartment. (202) The auxiliary compartment is installed on the (203) auxiliary compartment slide rail device. (204) The auxiliary compartment telescopic electric push rod is installed between the (201) main compartment and the top of the (203) auxiliary compartment slide rail device. (205) The vacuum adsorption fixing module is installed on the (206) vacuum adsorption fixing module slide rail device. (207) The vacuum adsorption fixing module electric push rod is installed between the (201) main compartment and the top of the (206) vacuum adsorption fixing module slide rail device. (208) The main compartment bridging door cover is installed at the outer opening of the (201) main compartment, and the bottom is connected by a rotating hinge. Two sets of (209) main compartment bridging door cover electric roller devices are installed between the (201) main compartment and the (208) main compartment bridging door cover on each side. Four sets (210) of main body landing feet are installed at the four corners of the bottom of the (201) main body. (211) The auxiliary body telescopic moving wheels are located at both ends of the bottom of the (202) auxiliary body opening. Various mechanisms are riveted or locked with corresponding fasteners, and eight sets (212) of duct propeller device mounting seats are welded to the top of the (201) main body and the top of the (202) auxiliary body respectively.

4. The flying elevator according to claim 1 is characterized by: (300) a power supply transfer platform vehicle component (as shown in Figure 3) of the mechanism; (301) a transfer electric vehicle; (302) an electric vehicle operator's cab; (303) a flying elevator cable winding device; (304) a flying elevator landing platform automatic leveling device; (305) a flying elevator landing platform; and (306) a cable winding device cable stretching dynamic detection module. Connection method: (302) The electric vehicle operator's cab is located at the front end of (301) the transfer electric vehicle; (303) the flying elevator cable winding device is located at the rear end of (301) the transfer electric vehicle's cargo box; (304) the flying elevator landing platform automatic leveling device is located above (301) the transfer electric vehicle's cargo box; (305) the flying elevator landing platform is located above (304) the flying elevator landing platform automatic leveling device; and (306) the cable winding device cable stretching dynamic detection module is located at the rear end of (303) the flying elevator cable winding device. Install and fix the components according to the designed workstations by locking or welding them with the appropriate fasteners.

5. The flying elevator according to claim 1 is characterized by the following components in the mechanism: (400) intelligent control system (as shown in Figure 4): (401) central control system; (402) flight control device; (403) ground control device; (404) unmanned driving system; (405) heading and attitude balance system; (406) sensor ranging and visual monitoring system; (407) offline dual-power battery for flight; (408) offline dual-power battery automatic switcher for flight; (409) vehicle-mounted dual-power aluminum-air battery power station; (410) vehicle-mounted dual-power aluminum-air battery power station automatic switcher; (411) mains power interface; (412) automatic interface for the flying elevator with wired flight cable; (413) power control system; (414) power detection system; (415) power detection system. Connection method: (401) central control system and (403) ground control device are respectively installed in the (302) electric vehicle operating room. (409) The vehicle-mounted dual-power aluminum-air battery power station, (410) the vehicle-mounted dual-power aluminum-air battery power station automatic power switch, and (411) the mains power interface are installed inside the 301 transfer electric vehicle compartment. (402) The flight control device, (407) the offline flight dual-power battery, and (408) the offline flight dual-power battery automatic switch are all installed on the top of the (201) flight elevator main body. (412) The flight elevator wired flight cable automatic interface is installed at the bottom of the (201) flight elevator main body. Other ranging and vision hardware are installed on the outside of the (200) flight elevator body. (401) serves as the main control system and interfaces with all branch modules of the present invention. (409) provides power for all devices and modules of the present invention. (408) provides power for all devices and modules on the flight elevator during offline flight. Each control system and sensing system interfaces with its respective equipment and devices, and is connected through remote control modules, wires, cables, and hoses.

6. The flying elevator according to claim 1 is characterized by: (300) a power supply transfer platform vehicle component (as shown in Figure 3) of the mechanism; (301) a transfer electric vehicle; (302) an electric vehicle operator's cab; (303) a flying elevator cable winding device; (304) a flying elevator landing platform automatic leveling device; (305) a flying elevator landing platform; and (306) a cable winding device cable stretching dynamic detection module. Connection method: (302) The electric vehicle operator's cab is located at the front end of (301) the transfer electric vehicle; (303) the flying elevator cable winding device is located at the rear end of (301) the transfer electric vehicle's cargo box; (304) the flying elevator landing platform automatic leveling device is located above (301) the transfer electric vehicle's cargo box; (305) the flying elevator landing platform is located above (304) the flying elevator landing platform automatic leveling device; and (306) the cable winding device cable stretching dynamic detection module is located at the rear end of (303) the flying elevator cable winding device. Install and fix the components according to the designed workstations by locking or welding them with the appropriate fasteners.

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