Balanced power lift rescue capsule

Abstract

The utility model discloses a balanced power lifting rescue cabin belongs to rescue equipment technical field, including unmanned aerial vehicle body, rescue cabin, electromagnetic suction subassembly and fixed component, and the bottom of unmanned aerial vehicle body is provided with containing bin, and the rescue cabin is set up inside containing bin, and the electromagnetic suction subassembly is set up between containing bin and rescue cabin, and the fixed component is set up in the inside of the top wall of containing bin. The problem that the existing technology is difficult to provide timely rescue due to the influence of large -scale rescue unmanned aerial vehicle to the landing environment is solved. The utility model as an innovative rescue equipment fills the blank of traditional rescue mode in quick response, complex environment operation etc. has broad market prospect.

Description

Technical Field

[0001] This utility model relates to the field of rescue equipment technology, specifically to a balanced power lifting rescue cabin. Background Technology

[0002] In emergency rescue scenarios, traditional rescue methods are often limited by geographical environment and transportation conditions, resulting in slow response times and limited rescue coverage. For example, in remote mountainous areas, severely affected cities, and densely populated areas, ground rescue vehicles have difficulty reaching the scene quickly. While large rescue drones can solve the transportation problem to some extent, their large size presents shortcomings in terms of precise landing, site constraints, and on-site operational space. For patients with sudden cardiovascular and cerebrovascular diseases or severe trauma, every second of delay can lead to worsening of their condition or even death. In natural disasters such as earthquakes, floods, landslides, traffic accident scenes, and densely populated urban areas, affected people urgently need rapid medical assistance and material support, but existing rescue methods are insufficient to meet the needs for efficient and precise rescue.

[0003] Therefore, how to provide a balanced power lifting rescue cabin to overcome the shortcomings of existing technologies is a technical problem that urgently needs to be solved by those skilled in the art. Utility Model Content

[0004] Therefore, this utility model provides a balanced power lifting rescue cabin to solve the problem in the prior art that large rescue drones are greatly affected by the take-off and landing environment, making it difficult to provide timely rescue.

[0005] To achieve the above objectives, this utility model provides the following technical solution:

[0006] This utility model discloses a balanced power lifting rescue cabin, comprising:

[0007] The drone itself has a storage compartment at the bottom;

[0008] The rescue capsule is located inside the containment chamber;

[0009] An electromagnetic suction assembly is disposed between the containment chamber and the rescue chamber;

[0010] A fixing component is disposed inside the top wall of the receiving compartment.

[0011] Furthermore, the rescue capsule includes:

[0012] The cabin is a hollow structure, and the side walls of the cabin are hinged with cabin doors.

[0013] Several powered turbofans are located at the bottom of the hull;

[0014] The power battery is located inside the side wall of the cabin and is used to power the turbofan.

[0015] Furthermore, the electromagnetic attraction component includes:

[0016] An electromagnet is installed on the top wall of the container.

[0017] A ferromagnetic connector is installed on the top of the cabin, and the ferromagnetic connector corresponds to the position of the electromagnet.

[0018] Furthermore, the fixing component includes:

[0019] A sliding groove is formed inside the top wall of the receiving chamber, and the sliding groove is connected to the receiving chamber;

[0020] A servo motor is installed in the sliding groove, and a gear is installed at the output end of the servo motor;

[0021] The first tooth groove is slidably connected in the sliding groove, and one end of the first fixing rod is connected to the side wall of the first tooth groove. The other end of the first fixing rod extends into the receiving chamber along the sliding groove.

[0022] The second tooth groove is slidably connected in the sliding groove. One end of the second fixing rod is connected to the side wall of the second tooth groove, and the other end of the second fixing rod extends into the receiving chamber along the sliding groove.

[0023] The first tooth groove and the second tooth groove are slidably connected and mesh with the gear respectively;

[0024] Fixing holes are symmetrically arranged and opened on the outer side wall of the cabin. The fixing holes are engaged with the first fixing rod and the second fixing rod.

[0025] Furthermore, the ferromagnetic connector is made of low-carbon steel.

[0026] Furthermore, the rescue cabin is equipped with a stretcher bed and an AED (Automated External Defibrillator).

[0027] This utility model has the following advantages:

[0028] This invention, by setting up a drone body and a rescue cabin, can avoid the problem of slow rescue response speed caused by factors such as geographical environment and traffic conditions in traditional ground rescue methods. It can also respond and provide rescue in locations where the drone body cannot land by releasing the rescue cabin.

[0029] By setting up electromagnetic attraction and fixing components, the rescue cabin and the drone body can be locked and released in seconds. Electromagnetic attraction provides instantaneous connection, while the double-tooth groove driven fixing rod system forms a mechanical interlock through locking holes to ensure zero displacement during transportation. When released, the electromagnet is de-energized and demagnetized, and the fixing rod retracts synchronously to achieve precise deployment. Attached Figure Description

[0030] To more clearly illustrate the embodiments of this utility model or the technical solutions in the prior art, the drawings used in the description of the embodiments or the prior art will be briefly introduced below. Obviously, the drawings in the following description are merely exemplary, and those skilled in the art can derive other embodiments based on the provided drawings without creative effort.

[0031] The structures, proportions, sizes, etc. illustrated in this specification are only for the purpose of assisting those skilled in the art in understanding and reading the content disclosed herein, and are not intended to limit the implementation conditions of this utility model. Therefore, they have no substantial technical significance. Any modifications to the structure, changes in the proportions, or adjustments to the size, without affecting the effects and objectives that this utility model can produce, should still fall within the scope of the technical content disclosed in this utility model.

[0032] Figure 1 A three-dimensional view of the balanced power lifting rescue cabin provided for this utility model;

[0033] Figure 2 Cross-sectional view of the balanced power lifting rescue cabin provided by this utility model;

[0034] Figure 3 Provided by this utility model Figure 2 Enlarged view of the A-structure;

[0035] Figure 4 A perspective view of the fixing component provided by this utility model;

[0036] Figure 5 A three-dimensional view of the rescue cabin provided for this utility model;

[0037] Figure 6 A cross-sectional view of the rescue cabin provided for this utility model.

[0038] In the diagram: 1. UAV body; 2. Storage compartment; 3. Rescue compartment; 31. Cabin; 32. Door; 33. Power turbofan; 34. Power battery; 35. Stretcher bed; 36. AED defibrillator; 41. Electromagnet; 42. Ferromagnetic connector; 51. Sliding groove; 53. Servo motor; 54. Gear; 55. First tooth groove; 56. First fixing rod; 57. Second tooth groove; 58. Second fixing rod; 59. Fixing hole. Detailed Implementation

[0039] The following specific embodiments illustrate the implementation of this utility model. Those skilled in the art can easily understand other advantages and effects of this utility model from the content disclosed in this specification. Obviously, the described embodiments are only some, not all, of the embodiments of this utility model. Based on the embodiments of this utility model, all other embodiments obtained by those skilled in the art without creative effort are within the protection scope of this utility model.

[0040] Please refer to Figures 1-6 The present invention discloses a balanced power lifting rescue cabin, which consists of four parts, as follows: Figure 1 , Figure 2 As shown, the device includes a drone body 1, a rescue cabin 3, an electromagnetic suction component, and a fixing component. The drone body 1 has a receiving compartment 2 at its bottom. The rescue cabin 3 is located inside the receiving compartment 2. The electromagnetic suction component is located between the receiving compartment 2 and the rescue cabin 3. The fixing component is located inside the top wall of the receiving compartment 2.

[0041] In this embodiment, the drone body 1 and the rescue capsule 3 are detachable and operate independently. The drone body 1 carries the rescue capsule 3 for movement. The rescue capsule 3 is released in situations where the drone body 1 cannot land accurately, such as at a car accident scene or in a densely populated urban area. Due to its small size, the rescue capsule 3 can respond quickly and provide rescue. The rescue capsule 3 measures 2m * 1.5m * 1.5m. The drone body 1 is too large to land in densely populated residential areas, while the rescue capsule 3, being small, can land in a parking space or even a small open space in front of a building entrance.

[0042] By configuring the drone body 1 and the rescue capsule 3, the problem of slow rescue response speed caused by geographical environment and traffic conditions in traditional ground rescue methods can be avoided. Furthermore, the rescue capsule 3 can be deployed to respond and carry out rescue operations in locations where the drone body 1 cannot land. Electromagnetic attraction and fixing components enable second-level locking and releasing between the rescue capsule 3 and the drone body 1. Electromagnetic attraction provides instantaneous connection, while the double-tooth-driven fixing rod system forms a mechanical interlock through the locking hole 59, ensuring zero displacement during transportation. During release, the electromagnet 41 is de-energized and demagnetized, retracting synchronously with the fixing rod for precise deployment.

[0043] like Figure 5 , Figure 6As shown, the rescue cabin 3 includes a cabin body 31, a power turbofan 33, and a power battery 34. The cabin body 31 has a hollow structure, and a door 32 is hinged to the side wall of the cabin body 31. Several power turbofans 33 are arranged at the bottom of the cabin body 31, and the power battery 34 is arranged inside the side wall of the cabin body 31. The power battery 34 is used to supply power to the power turbofans 33.

[0044] In this embodiment, the rescue capsule uses multiple sets of power batteries 34 and multiple sets of power turbofans 33 as power sources, enabling it to achieve smooth vertical take-off and landing, similar to a residential elevator, with a maximum take-off height of 150 meters. This vertical take-off and landing method is not restricted by terrain conditions and can quickly take off and land in narrow spaces and complex terrains, compressing the golden treatment time to the "platinum ten minutes" and winning valuable time for rescue.

[0045] The main body of the drone 1 provides the primary power, while the bottom of the rescue cabin 3 is equipped with multiple sets of power turbofans 33 and power batteries 34. If the main body of the drone 1 malfunctions during operation, the rescue cabin 3 can provide lifting force to make the whole thing land smoothly and slowly. If the rescue cabin 3 malfunctions, the main body of the drone 1 can provide hoisting force to make the whole thing land in a balanced manner. The two complement each other to achieve the maximum safety effect and greatly improve the reliability of the rescue process.

[0046] Perfectly balanced combination and separation design: The Balanced Power Rescue Pod 3 combines with a high-altitude unmanned helicopter or a tandem unmanned helicopter through electromagnetic attraction, finding the best balance between weight, size, stability, and controllability. This ensures that the Balanced Power Rescue Pod 3 is safe and reliable during takeoff, combination with the drone, and separation and landing, and can operate stably even in complex weather conditions.

[0047] Preferably, the rescue capsule 3 is equipped with a lidar positioning and sensing system. This system helps the rescue capsule 3 achieve precise positioning with the containment capsule 2, ensuring that the rescue capsule 3 can accurately enter the containment capsule 2. Simultaneously, it can monitor and avoid obstacles such as trees and power lines at the landing site. The lidar positioning and sensing system can be a system manufactured by Shenzhen Leishen Intelligent Systems Co., Ltd., or other 3D SLAM laser vision recognition solutions.

[0048] Preferably, a wireless charging component can be installed between the housing 2 and the rescue cabin 3 so that the two can replenish each other's energy.

[0049] Preferably, rescue capsule 3 can be equipped with a thermal imager and a life detector.

[0050] like Figure 2 , Figure 3As shown, the electromagnetic attraction assembly includes an electromagnet 41 and a ferromagnetic connector 42. The electromagnet 41 is installed on the top wall of the receiving chamber 2, and the ferromagnetic connector 42 is installed on the top of the chamber 31. The ferromagnetic connector 42 is positioned opposite to the electromagnet 41.

[0051] In this embodiment, the bitmap showing the arrangement of the electromagnet 41 and the ferromagnetic connector 42 is as follows: Figure 2 , Figure 3 As shown, when the rescue cabin 3 and the containment cabin 2 are docked, the electromagnet 41 will generate magnetic force and magnetically connect with the ferromagnetic connector 42; when released, the electromagnet 41 will be de-energized and demagnetized, and released synchronously with the fixing component to achieve precise deployment.

[0052] like Figure 2 , Figure 3 , Figure 4 As shown, the fixing assembly includes a sliding groove 51, a servo motor 53, a first toothed groove 55, a second toothed groove 57, and a fixing hole 59. The sliding groove 51 is formed inside the top wall of the receiving chamber 2 and is connected to the receiving chamber 2. The servo motor 53 is installed in the sliding groove 51, and a gear 54 is installed at the output end of the servo motor 53. The first toothed groove 55 is slidably connected in the sliding groove 51, and one end of a first fixing rod 56 is connected to the side wall of the first toothed groove 55. The other end of the first fixing rod 56 is connected along... The sliding groove 51 extends into the receiving chamber 2. The second toothed groove 57 is slidably connected in the sliding groove 51. One end of the second fixing rod 58 is connected to the side wall of the second toothed groove 57. The other end of the second fixing rod 58 extends into the receiving chamber 2 along the sliding groove 51. The first toothed groove 55 and the second toothed groove 57 are slidably connected and mesh with the gear 54 respectively. The fixing holes 59 are symmetrically arranged and opened on the outer side wall of the chamber 31. The fixing holes 59 form a snap-fit ​​connection with the first fixing rod 56 and the second fixing rod 58.

[0053] In this embodiment, the specific shape of the sliding groove 51 is as follows: Figure 2 The sliding groove 51 has a wider middle section to accommodate the movement of the first toothed groove 55 and the second toothed groove 57. There is space at both ends of the sliding groove 51 to provide space for the movement of the first fixed rod 56 and the second fixed rod 58. When the servo motor 53 starts, it drives the gear 54 to rotate, causing the first toothed groove 55 and the second toothed groove 57 to move in opposite directions, thereby engaging the first fixed rod 56 and the second fixed rod 58 with the fixing hole 59 to lock or unlock the rescue chamber 3.

[0054] Preferably, the ferromagnetic connector 42 is made of low-carbon steel. The low-carbon steel ferromagnetic connector 42, in conjunction with the electromagnet 41, maintains stable attraction force within a temperature range of -40℃ to 80℃, and has a remanent magnetization of <0.1T, ensuring reliable connection and rapid separation in extremely cold / high temperature environments. Meanwhile, the power turbofan 33 adopts an IP67 protection rating design, adapting to operation in rainy and snowy weather.

[0055] like Figure 6 As shown, rescue capsule 3 is equipped with a stretcher bed 35 and an AED defibrillator 36. The stretcher bed 35 and the AED defibrillator 36 can provide emergency assistance to the injured. In addition, rescue capsule 3 is equipped with a full range of emergency medical equipment and medicines, such as electrocardiogram monitors, oxygen bags, and first aid kits, forming a fully functional small air ambulance station to provide comprehensive and professional medical support for patients during transport.

[0056] Regarding the application scenarios of this utility model:

[0057] Pre-hospital emergency care: Upon receiving an emergency call for help related to sudden cardiovascular or cerebrovascular diseases, severe trauma, or accidents, the drone body 1 and rescue capsule 3 combine and deploy rapidly. Upon arrival at the scene, rescue capsule 3 descends vertically, allowing professional medical personnel to provide on-site emergency treatment to the patient, either inside or outside the capsule. This includes wound dressing, CPR, and ECG monitoring to stabilize the patient's condition. Subsequently, rescue capsule 3 takes off and reassembles with drone body 1, transporting the patient to a nearby hospital with treatment capabilities as quickly as possible, significantly shortening the time between the onset of symptoms and receiving professional treatment.

[0058] Inter-hospital transport: For critically ill patients requiring transfer to other hospitals for higher-level treatment: The drone itself (1) and the rescue capsule (3) can establish a safe and rapid lifeline between different hospitals. During the transport, continuous medical monitoring equipment monitors the patient's vital signs in real time, and medical staff can take timely treatment measures as needed to ensure the patient's safety during transport and create favorable conditions for subsequent treatment.

[0059] Emergency Rescue: In the event of natural disasters such as earthquakes, floods, and landslides, as well as public health emergencies and major accidents, the low-altitude rescue capsule 3 can undertake a variety of critical tasks. For example, utilizing its flexible flight capabilities, it can penetrate deep into disaster areas to conduct search and rescue operations, quickly locating trapped individuals using onboard thermal imagers, life detectors, and other equipment; transport medical supplies, providing urgently needed medicines and medical equipment to disaster victims and rescue personnel in a timely manner; and transfer the injured and sick from dangerous areas to safe medical treatment points, effectively alleviating the pressure on medical rescue in disaster areas.

[0060] In practical applications, upon receiving an emergency rescue mission, the dispatch center quickly plans the flight route and notifies relevant medical personnel to prepare. The UAV body 1, carrying the rescue capsule 3, rapidly flies to the rescue site. Upon reaching the designated area, the UAV hovers, the rescue capsule 3 completes electromagnetic separation, and lands smoothly and vertically. Medical personnel immediately begin treatment of the patient. After treatment, the rescue capsule 3 smoothly ascends and reconnects with the UAV body 1 via an electromagnetic attraction component, transferring the patient to the target hospital according to the planned route. Throughout the process, rescue personnel maintain close contact with the command center via a real-time communication system to ensure the smooth operation of the rescue mission. Simultaneously, regular maintenance is performed on the rescue capsule 3 and the UAV body 1, checking the performance of the power battery 34, the operation of the power turbofan 33, and the status of medical equipment to ensure the equipment can operate normally in critical moments.

[0061] Regarding the market prospects of this utility model:

[0062] This application, as an innovative rescue and relief device, fills the gaps in traditional rescue and relief methods in terms of rapid response and operation in complex environments, and has broad market prospects. In the field of medical rescue, it can provide medical institutions and emergency centers with efficient rescue methods, improve the success rate of rescue, and reduce patient mortality and disability rates; in emergency management departments, it can serve as an important piece of equipment for responding to natural disasters and emergencies, enhancing emergency rescue capabilities and protecting life and property; in the insurance industry, it helps reduce high rescue and relief costs and claims amounts, and improves the quality of insurance services. It is estimated that in the next few years, the global market demand for drone-based balanced rescue and relief capsules will double.

[0063] Regarding the potential for development of this utility model:

[0064] Technological Upgrades: With the continuous advancement of battery technology, sensing technology, radar technology, and 5G network technology, the driving range and power performance of this application can be further improved; by introducing more advanced sensor technologies and artificial intelligence algorithms, autonomous obstacle avoidance and intelligent navigation can be achieved, as well as intelligent diagnosis and treatment suggestions for patients' conditions, thereby improving the accuracy and intelligence of rescue operations.

[0065] Application Expansion: In addition to the existing medical emergency and rescue fields, the product can be expanded to special scenarios such as maritime rescue, forest fire rescue, and polar rescue. Customized design and functional optimization can be carried out to meet the needs of different scenarios, thereby expanding the application scope of the product.

[0066] Industry Collaboration: Strengthen cooperation with drone manufacturers, medical equipment manufacturers, research institutions, etc., to form a complete industrial chain ecosystem, jointly promote the development and application of low-altitude flight balance rescue capsule technology, and promote industrial upgrading and innovative development.

[0067] Although the present invention has been described in detail above with general descriptions and specific embodiments, some modifications or improvements can be made to it, which will be obvious to those skilled in the art. Therefore, all such modifications or improvements made without departing from the spirit of the present invention fall within the scope of protection claimed by the present invention.

Claims

1. A balanced-powered lifting rescue cabin, characterized in that, include: The drone body (1) has a storage compartment (2) at the bottom; A rescue compartment (3) is located inside the containment compartment (2); An electromagnetic suction assembly is disposed between the receiving chamber (2) and the rescue chamber (3); A fixing component is disposed inside the top wall of the receiving chamber (2).

2. The balanced power lifting rescue cabin as described in claim 1, characterized in that, The rescue capsule (3) includes: The cabin (31) is a hollow structure, and a cabin door (32) is hinged to the side wall of the cabin (31); Several turbofans (33) are installed at the bottom of the cabin (31); A power battery (34) is disposed inside the side wall of the cabin (31) and is used to power the power turbofan (33).

3. The balanced power lifting rescue cabin as described in claim 2, characterized in that, The electromagnetic attraction component includes: An electromagnet (41) is installed on the top wall of the receiving chamber (2); A ferromagnetic connector (42) is installed on the top of the cabin (31), and the ferromagnetic connector (42) is positioned opposite to the electromagnet (41).

4. The balanced power lifting rescue cabin as described in claim 2, characterized in that, The fixing component includes: A sliding groove (51) is formed inside the top wall of the receiving chamber (2), and the sliding groove (51) is connected to the receiving chamber (2); A servo motor (53) is installed in the sliding groove (51), and a gear (54) is installed at the output end of the servo motor (53); The first tooth groove (55) is slidably connected in the sliding groove (51). One end of the first fixing rod (56) is connected to the side wall of the first tooth groove (55), and the other end of the first fixing rod (56) extends into the receiving chamber (2) along the sliding groove (51). The second tooth groove (57) is slidably connected in the sliding groove (51). One end of the second fixing rod (58) is connected to the side wall of the second tooth groove (57). The other end of the second fixing rod (58) extends into the receiving chamber (2) along the sliding groove (51). The first tooth groove (55) and the second tooth groove (57) are slidably connected and mesh with the gear (54) respectively; Fixing holes (59) are symmetrically arranged and opened on the outer side wall of the cabin (31). The fixing holes (59) are engaged with the first fixing rod (56) and the second fixing rod (58).

5. The balanced power lifting rescue cabin as described in claim 3, characterized in that, The ferromagnetic connector (42) is made of low-carbon steel.

6. The balanced power lifting rescue cabin as described in claim 2, characterized in that, The rescue cabin (3) is equipped with a stretcher bed (35) and an AED defibrillator (36).

Images