Airborne ophthalmology and otorhinolaryngology hospital
By installing quick-release partitions and purification fan units in the cabin of a regular passenger aircraft, a Class I clean surgical environment is created, solving the problem that rotorcraft helicopters cannot create a clean surgical environment. This enables airborne medical services for complex ENT surgeries and expands the coverage.
Patent Information
- Application Number
- CN202511662708.8
- Authority / Receiving Office
- CN · China
- Patent Type
- Applications(China)
- Current Assignee / Owner
- Filing Date
- 2025-11-13
- Publication Date
- 2026-01-02
AI Technical Summary
Existing technologies cannot create a clean surgical environment inside the cabin of a rotorcraft helicopter, which limits the implementation of complex ENT surgeries. Furthermore, rotorcraft helicopters have limited range and cannot cover remote areas, while ordinary passenger planes lack high-quality airport facilities, resulting in insufficient medical service capabilities.
Quick-release partitions and purification fan units are installed in the cabin of a regular passenger aircraft to separate the front cabin treatment area, the middle cabin operating area, and the rear cabin equipment area. Ground air conditioning units and purification fan units are used to create a Class I clean operating environment, and cascade control of clean airflow is achieved to form a three-zone medical environment.
The ability to quickly build and dismantle an airborne ENT hospital, meeting Class I clean operating room standards, enabling complex ENT surgeries, expanding medical service coverage, without damaging cabin facilities, and applicable to different aircraft models and configurations.
Smart Images
Figure CN121247068A_ABST
Abstract
Description
TECHNICAL FIELD
[0001] The present application relates to an airborne five-senses hospital. BACKGROUND
[0002] The five-senses department (ophthalmology, otolaryngology) is a department or specialized hospital for treating the five senses (vision, hearing, taste, smell, and touch) of the human body. From the forehead to the neck, the organs of the human body involved are many diseases. Many people do not understand it well and do not pay much attention to it. It is mistakenly believed that five-senses diseases are small diseases, such as eye discomfort, rhinitis, itchy ears, swollen tonsils, and other common diseases. In fact, large fatal tumors such as nasopharyngeal carcinoma and laryngeal carcinoma, and small diseases that affect the quality of life of many people, such as cataract eye disease, allergic rhinitis, hay fever, otitis media, tinnitus, snoring, and chronic pharyngitis, all belong to the scope of the five-senses department. With the improvement of the quality of life, people pay more and more attention to the discomfort caused by the eyes, ears, nose, throat, and other parts. At the same time, the five-senses department is a front-line department of doctors and patients, and is one of the medical departments with the highest risk of infection. Some high-difficulty five-senses surgeries must be performed in a Class I clean operating room that meets the requirements of the national standard "Hospital Clean Operating Department Building Technical Specification" GB 50333. However, there are not many five-senses doctors, especially experienced doctors, in third- and fourth-tier city hospitals, not to mention remote areas. There is no five-senses department I-class clean operating room. If these top five-senses medical clinical teams can serve in these areas, not only can they treat patients, but also can provide opportunities for local medical staff to observe, share knowledge, and train on the spot, and cultivate local five-senses medical professionals who are most needed. Leave a "five-senses hospital that cannot be left behind" in the local area.
[0003] In order to serve less developed areas, there are already train hospitals and vehicle-mounted hospitals, and in order to make medical services available in more remote or more remote areas, there have also been attempts to carry out simple ophthalmic clinical treatment on helicopters, but the cabin space of the rotor helicopter is narrow and cannot build a clean operating environment, and cannot perform high-difficulty five-senses surgery, so the medical service capacity is limited. Secondly, the rotor helicopter has weak endurance and can only cover an area within a radius of 200 km, which cannot meet the needs of remote areas. Only large fixed-wing jet aircraft, such as transport aircraft, can solve the above problems, but they require high-quality airports that are difficult to provide in remote areas.
[0004] Therefore, in view of the above problems, an airborne five-senses hospital suitable for different types of ordinary passenger aircraft is proposed. SUMMARY
[0005] The purpose of the present application is to overcome the existing defects and provide an airborne five-senses hospital suitable for different types of ordinary passenger aircraft, achieving the purpose of an airborne hospital.
[0006] In order to achieve the above object, the present application provides the following technical scheme: the airborne five sense organs hospital comprises a cabin, a front partition plate and a rear partition plate are arranged inside the cabin to separate a front cabin diagnosis and treatment area, a middle cabin operation area and a rear cabin equipment area; a horizontal laminar flow purification fan unit is arranged on one side of the rear cabin equipment area close to the rear partition plate, an air supply opening of the horizontal laminar flow purification fan unit is communicated with the middle cabin operation area, and the horizontal laminar flow purification fan unit is used for conveying clean one-way airflow to the middle cabin operating room; an external connecting assembly matched with a cabin door is connected to a left rear cabin door of the rear cabin equipment area, and the external connecting assembly is used for connecting a ground airplane air conditioning unit; a safety passage is arranged on one side of the middle cabin operation area and the rear cabin equipment area, the middle cabin operation area is communicated with the safety passage through an operation area door, the rear cabin equipment area is communicated with the safety passage through a first rear door, a right rear cabin door is communicated with the rear cabin equipment area through a second rear door, a front cabin side door of the front cabin diagnosis and treatment area is communicated with the safety passage, the front cabin side door of the front cabin diagnosis and treatment area is a normally closed safety door, and three doors in front of the operation area door are formed; the front part of the middle cabin operating room is communicated with the front cabin diagnosis and treatment area through an operation area front door.
[0007] Preferably, the horizontal laminar flow purification fan unit comprises a fan box, an efficient low-noise fan is arranged in the fan box; the fan box is connected with a filter box, an efficient filter is arranged in the filter box, and an air supply opening of the filter box is embeddedly connected to the rear partition plate, with an outlet facing the middle cabin operating room; and the air supply opening of the filter box is a air supply hole plate.
[0008] Preferably, the external connecting assembly matched with the cabin door comprises an air supply static pressure box and an external round pipe, the external round pipe is connected to the left rear cabin door of the rear cabin equipment area, one end of the external round pipe is communicated with the ground airplane air conditioning unit, and the other end of the external round pipe penetrates through the left rear cabin door and is communicated with the air supply static pressure box arranged on the inner side of the rear door of the cabin.
[0009] Preferably, the front partition plate is composed of the operation area front door, a side perforated partition plate and the front cabin side door; and the outer wall of the front cabin side door and the side perforated partition plate is connected with the inner wall of the cabin.
[0010] Preferably, the rear partition plate is a solid wall plate.
[0011] Preferably, the present application further comprises a quick dismounting and non-damage connecting assembly for connecting the front partition plate and the rear partition plate with the inner wall of the cabin.
[0012] Preferably, the quick dismounting and non-damage connecting assembly comprises an angle code, one side of the angle code is connected with the front partition plate or the rear partition plate, and the other side of the angle code is connected with the inner wall of the cabin; a soft rubber sealing strip is arranged between the side wall of the front partition plate or the rear partition plate and the inner wall of the cabin; and the lower end of the front partition plate or the rear partition plate is connected with the original reserved ground groove of the cabin through a ground rail.
[0013] Compared with the prior art, the beneficial effects of the present application are that the present application sets up the five-senses department hospital in the cabin of the ordinary passenger plane of different types, realizes the purpose of the airborne hospital, and facilitates the treatment of patients in different regions; the whole five-senses department hospital which can be quickly and non-destructively disassembled and assembled is quickly constructed or disassembled on the aircraft by using the plate wall and the purification air conditioning unit, and is equipped with the I-class clean operating room reaching the national standard Hospital Clean Operating Department Building Technical Specification GB 50333. After the aircraft lands and stops at the designated parking apron, the airborne five-senses department hospital can be quickly built in one night, and the medical service can be provided the next day. After the task is completed, the airborne five-senses department hospital can be quickly disassembled, and the cabin is not damaged or changed, which meets the airworthiness requirements and continues to perform the flight task.
[0014] The present application sets up the five-senses department hospital in the cabin of the ordinary passenger plane of different types, realizes the purpose of the airborne hospital, and facilitates the treatment of patients in different regions; the whole five-senses department hospital which can be quickly and non-destructively disassembled and assembled is quickly constructed or disassembled on the aircraft by using the plate wall and the purification air conditioning unit, and is equipped with the I-class clean operating room reaching the national standard Hospital Clean Operating Department Building Technical Specification GB 50333. After the aircraft lands and stops at the designated parking apron, the airborne five-senses department hospital can be quickly built in one night, and the medical service can be provided the next day. After the task is completed, the airborne five-senses department hospital can be quickly disassembled, and the cabin is not damaged or changed, which meets the airworthiness requirements and continues to perform the flight task. BRIEF DESCRIPTION OF DRAWINGS
[0015] The accompanying drawings are included to provide a further understanding of the present application, and constitute a part of the specification, illustrate the present application and explain the principles of the present application, and do not constitute a limitation of the present application. In the drawings: Figure 1 It is a schematic diagram of the plane layout of the airborne five-senses department hospital of the present application; Figure 2 It is a schematic diagram of the reverse plane layout of the airborne five-senses department hospital of the present application; Figure 3 It is a schematic diagram of the horizontal laminar flow purification air blower unit of the present application; Figure 4The schematic diagram of the air inlet and outlet operation of the horizontal laminar flow purification fan unit of the present application; Figure 5 The schematic diagram of the installation of the high-efficiency fan of the present application; Figure 6 The schematic diagram of the installation position of the air supply static pressure box of the present application; Figure 7 The schematic diagram of the installation of the front partition plate of the present application (with a luggage compartment); Figure 8 The schematic diagram of the installation of the front partition plate of the present application Figure 2 (without a luggage compartment); Figure 9 The schematic diagram of the installation of the rear partition plate of the present application (with a luggage compartment); Figure 10 The schematic diagram of the installation of the rear partition plate of the present application Figure 2 (without a luggage compartment); Figure 11 The detail view of the connecting assembly of the present application; Figure 12 The schematic diagram of the third door of the present application; Figure 13 The schematic diagram of the first door of the present application.
[0016] In the figure: 1, cabin; 2, front partition plate; 3, rear partition plate; 4, front cabin diagnosis and treatment area; 5, middle cabin operation area; 6, rear cabin equipment area; 7, safety passage; 8, operation area door; 9, first rear door; 10, operation area front door; 11, fan box; 12, high-efficiency low-noise fan; 13, filter box; 14, high-efficiency filter; 15, air supply hole plate; 16, air supply static pressure box; 17, externally connected circular pipe; 18, side perforated partition plate; 19, front cabin side door; 20, corner brace; 21, soft rubber sealing strip; 22, ground groove; 23, ground rail; 25, left rear cabin door; 26, front cabin door; 27, right rear cabin door; 28, second rear door. DETAILED DESCRIPTION
[0017] The technical solutions in the embodiments of the present application will be described clearly and completely below with reference to the accompanying drawings in the embodiments of the present application. Obviously, the described embodiments are only a part of the embodiments of the present application, rather than all the embodiments of the present application. Based on the embodiments in the present application, all the other embodiments obtained by those skilled in the art without creative labor fall within the protection scope of the present application.
[0018] As Figures 1-13As shown, the airborne five-organ hospital includes a cabin 1, a front partition 2 and a rear partition 3 are arranged inside the cabin 1 to separate a front cabin diagnosis and treatment area 4, a middle cabin operation area 5 and a rear cabin equipment area 6 which are quickly and non-destructively installed and removed; a horizontal laminar flow purification fan group is arranged on one side of the rear cabin equipment area 6 close to the rear partition 3, and the air supply port of the horizontal laminar flow purification fan group is connected to the middle cabin operation area 5, which is used to deliver clean one-way airflow to the middle cabin operation area 5; an external connecting assembly adapted to the cabin door is connected to the left rear cabin door 25 of the rear cabin equipment area 6, which is used to connect the ground airplane air conditioning unit; a safety passage 7 is arranged on one side of the middle cabin operation area 5 and the rear cabin equipment area 6, the middle cabin operation area 5 is connected to the safety passage 7 through an operation area door 8, and the rear cabin equipment area 6 is connected to the safety passage 7 through a first rear door 9; the right rear cabin door 27 is connected to the rear cabin equipment area 6 through a second rear door 28, and the front part of the middle cabin operation area 5 is connected to the front cabin diagnosis and treatment area 4 through an operation area front door 10.
[0019] The airborne five-organ hospital includes a cabin, a front partition and a rear partition are arranged inside the cabin to separate a front cabin diagnosis and treatment area, a middle cabin operation room and a rear cabin equipment area; a horizontal laminar flow purification fan group is arranged on one side of the rear cabin equipment area close to the rear partition, and the air supply port of the horizontal laminar flow purification fan group is connected to the middle cabin operation area, which is used to deliver clean one-way airflow to the middle cabin operation area; an external connecting assembly adapted to the cabin door is connected to the cabin rear door of the rear cabin equipment area, which is used to connect the ground airplane air conditioning unit; a safety passage is arranged on one side of the middle cabin operation area and the rear cabin equipment area, the middle cabin operation area is connected to the safety passage through an operation room door, and the rear cabin equipment area is connected to the safety passage through a first rear door and a front door, forming an operation area front room. The present application can provide an airborne five-organ hospital and a high-level clean operation area for all different types of cabins with different configurations, and the clean airflow is used to achieve the purpose of medical environment control of the three areas of the airborne hospital Specifically, the front partition 2 and the rear partition 3 are arranged inside the cabin 1 to isolate the front cabin diagnosis and treatment area 4, the middle cabin operation area 5 and the rear cabin equipment area 6; the most basic function of the five-organ hospital is met. The layout of the three areas is independent and can be connected. The middle cabin operation area 5 and the rear cabin equipment area 6 are provided with a through safety passage 7, and the first rear door 9 of the safety passage 7 is used for the entry and exit of medical staff after changing clothes, and the front cabin side door 19 is normally closed, which together with the operation area door 8 constitutes a three-door front room with the operation area door as the priority.
[0020] Specifically, the rear cabin equipment area 6 is provided with a hand washing and changing room, a medical equipment cabinet, a changing cabinet, a medicine cabinet and an isolation transformer, the middle cabin is an operation area, and the front cabin is provided with an outpatient, examination and operation waiting area. The front cabin and the rear cabin can also be reversed according to the type of the airplane and the clinical requirements, forming a reverse cascade airflow as Figure 2 shown.
[0021] Specifically, the middle cabin operation area 5 can be provided with a single operating bed or two operating beds. The operating area can adopt horizontal laminar flow or vertical laminar flow. The operating bed in the operating room is inclined to one side and located at the center of the horizontal laminar flow, and the head of the operating bed is located in a first working surface with a horizontal laminar flow of not more than 3m. The special microscope for ophthalmology and other equipment can be arranged in the middle of the cabin with higher height.
[0022] Specifically, the medical staff enters the cabin buffer room through the right rear cabin door 27, changes shoes, and then enters the rear cabin equipment area 6 through the second rear door to change clothes, wash hands, and the like. The first rear door 9 of the rear cabin equipment area 6 serves as the entrance and exit of the medical staff after changing clothes, and enters the operating room through the operating area door 8 of the safety channel 7. When the operation is performed, the doors of the front cabin need to be interlocked, and the operating area door 8 has priority. That is, only when the operating area door is closed, the other two doors can be opened. When the operating area door is opened, the other two doors must be closed. One door (front cabin side door 19) leading to the operating room through the safety channel 7 is always closed. The other door (front cabin side door 19) provided on the orifice plate wall of the front cabin serves as the entrance and exit of the patient, and realizes the separation of doctors and patients. The horizontal laminar flow purification air supply unit is arranged on the rear side of the assembly type partition plate close to the rear cabin. The front cabin door 26 of the cabin is always open, which is convenient for doctors and patients to enter and exit, and also facilitates air flow removal. The opening degree of the front cabin door is adjusted to adjust the pressure difference with the operating area.
[0023] The horizontal laminar flow purification air supply unit includes a fan box 11, and a high-efficiency low-noise fan 12 is arranged in the fan box 11. The fan box 11 is connected with a filter box 13, a high-efficiency filter 14 is arranged in the filter box 13, the filter box 13 is embeddedly connected with the rear partition plate 3 at the air supply port, the outlet of the filter box 13 faces the middle cabin operation area 5, and the air supply port of the filter box 13 is an air supply orifice plate 15. The horizontal laminar flow can be formed in the operating area in the operating room, and the requirements of the I-class clean operating room in the national standard “Hospital Clean Operating Department Building Technical Specification” GB 50333 are met. The size of the purification air supply unit is adjusted in height or width according to the service model on the premise of meeting the requirements of the I-class clean operating area.
[0024] The external assembly matched with the cabin door includes an air supply static pressure box 16 and an external round pipe 17. The external round pipe 17 is connected to the left rear cabin door 25 of the rear cabin equipment area 6, one end is connected to the ground airplane air conditioning unit, and the other end penetrates through the left rear cabin door 25 and is connected to the special-shaped air supply static pressure box 16 arranged on the inner side of the left rear cabin door 25.
[0025] Specifically, the outer circular pipe 17 is connected to the ground plane air conditioning unit, and the air supply amount of the ground plane air conditioning unit is less than the air inlet amount of the horizontal laminar flow unit. The air flow is sent into the rear cabin equipment area 6 through the high-efficiency air supply port provided in the air supply static pressure box 16. After being sucked by the horizontal laminar flow purification air supply unit, the air flow is sent into the middle cabin operation area 5, and the horizontal laminar flow is generated in the operation area, so that a highly sterile and dust-free I-class operation environment is formed in the operation area. The air conditioning clean air flow is pressed out of the aircraft through the normally open front cabin front door 26. The original air conditioning system of the aircraft is no longer used, and the air conditioning air flow can enter from the front cabin and be discharged from the rear cabin according to the type and clinical requirements.
[0026] Specifically, the outer circular pipe 17 is connected to the ground plane air conditioning unit, and the air supply amount of the ground plane air conditioning unit is less than the air inlet amount of the horizontal laminar flow unit. The air flow is sent into the rear cabin equipment area 6 through the high-efficiency air supply port provided in the air supply static pressure box 16. After being sucked by the horizontal laminar flow purification air supply unit, the air flow is sent into the middle cabin operation area 5, and the horizontal laminar flow is generated in the operation area, so that a highly sterile and dust-free I-class operation environment is formed in the operation area. The air conditioning clean air flow is pressed out of the aircraft through the normally open front cabin front door 26. The original air conditioning system of the aircraft is no longer used, and the air conditioning air flow can enter from the front cabin and be discharged from the rear cabin according to the type and clinical requirements.
[0027] The front partition plate 2 is composed of the operation area front door 10, the side perforated partition plate 18 and the front cabin side door 19. The outer wall of the front cabin side door 19 and the side perforated partition plate 18 is connected to the inner wall of the cabin 1. The rear partition plate 3 is a solid wall plate.
[0028] The quick dismounting and mounting connecting assembly is used for connecting the front partition plate 2 and the rear partition plate 3 with the inner wall of the cabin 1. The quick dismounting and mounting connecting assembly comprises an angle code 20, one side of the angle code 20 is connected with the front partition plate 2 or the rear partition plate 3, and the other side of the angle code 20 is connected with the inner wall of the cabin 1; a soft rubber sealing strip 21 is arranged between the side wall of the front partition plate 2 or the rear partition plate 3 and the inner wall of the cabin 1; the lower end of the front partition plate 2 or the rear partition plate 3 is connected with the original reserved ground groove 22 of the cabin 1 through a ground rail 23.
[0029] When the passenger plane is ready for flight, the front partition plate 2 and the rear partition plate 3 can be quickly dismounted through the quick dismounting and mounting connecting assembly, without changing any facilities and equipment of the original plane and without causing any damage to the cabin; after the flight reaches the designated position, the front partition plate 2 and the rear partition plate 3 can be quickly mounted to construct the five-sense organ hospital.
[0030] Specifically, the front partition plate 2 and the rear partition plate 3 meet the A-class flame-retardant requirement in GB 8624-2012 “Classification of Building Materials and Products Based on Combustion Performance”. The wall and the equipment are connected and fixed through the original fixed guide rail of the U-shaped ground groove and the cabin ground, the wall surface is fixed and stabilized by the two vertically intersecting wall surfaces, the angle code is fixed to the top of the cabin wall by the double-sided adhesive tape, and the wall plates are sealed by gluing.
[0031] Specifically, the front partition plate 2 and the rear partition plate 3 can be applied to the occasions where the cabin retains the luggage compartment and the occasions where the luggage compartment is removed, such as the occasions shown in Figs. Figure 7 、 8 , 9, 10; and are suitable for different types of passenger planes.
[0032] The cabin-mounted five-sense organ hospital is divided into a front cabin diagnosis and treatment area 4, a middle cabin operation area 5 and a rear cabin equipment area 6 by arranging the front partition plate 2 and the rear partition plate 3; a horizontal laminar flow purification air blower set is arranged on one side of the rear cabin equipment area 6 close to the rear partition plate 3, an air supply opening of the horizontal laminar flow purification air blower set is communicated with the middle cabin operation area 5, and the horizontal laminar flow purification air blower set is used for conveying clean one-way airflow to the middle cabin operation area 5; an external connecting assembly matched with the rear cabin door is connected to the left rear cabin door 25 of the rear cabin equipment area 6, and is used for connecting a ground plane air conditioning unit; the rear cabin equipment area 6 is provided with a hand washing basin, a changing cabinet, a medical equipment cabinet and an isolation transformer; the front cabin diagnosis and treatment area 4 is provided with an outpatient, examination and operation waiting area. An interface on the outside of the rear cabin door plate is connected to the ground plane air conditioning unit, and clean air is sent into the rear cabin through a high-efficiency air supply opening in a static pressure box. After being sucked by the horizontal laminar flow purification air blower set, the air is sent into the operation area, horizontal laminar flow is generated in the operation area, and a first-class operation environment with high sterility and dustlessness is formed in the operation area. The air flows into the front cabin through the perforated wall of the front cabin. Since a non-woven fabric filter layer is filled in the middle of the hole plate to form a damping layer, the pressure in the operation room is higher than that in the front cabin. The air conditioning airflow is pressed out of the plane through the always-open front cabin door, so that the clean airflow penetrates through the three cabin rooms of the cabin to form a three-zone clean and sterile medical environment with orderly positive airflow series.
[0033] The five-senses department hospital is arranged in the cabin, the purpose of the airborne hospital is realized, and treatment of patients in different regions is facilitated; the whole five-senses department hospital is quickly constructed or removed on the aircraft by using the quickly detachable plate wall and the purification air conditioning equipment, and the five-senses department hospital reaches the I-class clean operating room in the national standard "Hospital Clean Operating Department Building Technical Specification" GB 50333. After the aircraft lands, the aircraft is parked in the designated parking lot, and the airborne five-senses department hospital is quickly constructed in one night. The medical service can be provided the next day. After the medical service is completed, the airborne five-senses department hospital also needs to be quickly removed, and the original appearance of the aircraft is restored, and any slight damage to the original aircraft body caused by fixing or removing is avoided. The application can also be used for other aircraft, other airborne specialist hospitals and other types of operations.
[0034] Finally, it should be noted that: the above is only the preferred embodiment of the present application, and is not intended to limit the present application, although the present application has been described in detail with reference to the foregoing embodiments, those skilled in the art can still modify the technical solutions recorded in the foregoing embodiments, or make equivalent replacement for some technical features. Any modification, equivalent replacement, improvement, etc. made within the spirit and principles of the present application shall be included in the protection scope of the present application.
Claims
1. An airborne multispecialty hospital, characterized in that, The utility model provides a kind of aircraft cabin, comprising cabin (1), front bulkhead (2) and rear bulkhead (3) are provided inside the cabin (1), and front cabin treatment area (4), middle cabin operating area (5) and rear cabin equipment area (6) are separated by quick non-destructive installation and removal;Horizontal laminar flow purification fan unit is arranged in the rear cabin equipment area (6) one side close to the rear bulkhead (3), and its air supply opening is connected with the middle cabin operating area (5), for conveying clean one-way airflow for the middle cabin operating area (5);The left rear cabin door (25) of the rear cabin equipment area (6) is connected with the external component matched with cabin door, for connecting ground aircraft air conditioning unit;Safety passage (7) is arranged in one side of the middle cabin operating area (5) and the rear cabin equipment area (6), and the middle cabin operating area (5) is connected with the safety passage (7) by operating area door (8), and the rear cabin equipment area (6) is connected with the safety passage (7) by first rear door (9);Right rear cabin door (27) is connected with the rear cabin equipment area (6) by second rear door (28), and the front part of the middle cabin operating room (5) is connected with the front cabin treatment area (4) by operating area front door (10).
2. The airborne quinary hospital according to claim 1, characterized in that, The horizontal laminar flow purification fan unit includes fan box (11), and high-efficiency low-noise fan (12) is arranged inside the fan box (11);The fan box (11) is connected with filter box (13), and high-efficiency filter (14) is arranged inside the filter box (13), and the air supply opening of the filter box (13) is embeddedly connected on the rear bulkhead (3), and the outlet is towards the middle cabin operating room (5), and the air supply opening of the filter box (13) is air supply hole plate (15).
3. The airborne quinary hospital according to claim 1, characterized in that, The external component matched with cabin door includes air supply static pressure box (16) and external round pipe (17), and the external round pipe (17) is connected on the left rear cabin door (25) of the rear cabin equipment area (6), one end is connected with ground aircraft air conditioning unit, and the other end penetrates rear cabin door (25) and is connected with air supply static pressure box (16) arranged on the inner side of left rear cabin door (25).
4. The airborne ophthalmology hospital of claim 1, wherein, The front bulkhead (2) is composed of operating room front door (10), side perforated bulkhead (18) and front cabin side door (19);The outer wall of the front cabin side door (19) and the side perforated bulkhead (18) is connected with the inner wall of the cabin (1).
5. The airborne ophthalmology hospital of claim 1, wherein, The rear bulkhead (3) is solid wallboard.
6. The airborne ophthalmology hospital of claim 1, wherein, It also includes quick disassembly and connection assembly for non-destructive connection of the front bulkhead (2) and the rear bulkhead (3) with the inner wall of the cabin (1).
7. The airborne ophthalmology hospital of claim 6, wherein, The quick disassembly and connection assembly includes corner code (20), one side of the corner code (20) is connected with the front bulkhead (2) or the rear bulkhead (3), and the other side is connected with the inner wall of the cabin (1);Soft rubber sealing strip (21) is arranged between the side wall of the front bulkhead (2) or the rear bulkhead (3) and the inner wall of the cabin (1);The lower end of the front bulkhead (2) or the rear bulkhead (3) is connected with the original reserved ground slot (22) of the cabin (1) through ground rail (23).