Aircraft fire rescue real fire training device
By designing a splicable aircraft fire rescue real fire training device, the problem of lack of fire training devices suitable for different types of aircraft in the prior art is solved, real simulation training of various aircraft fire situations is achieved, and firefighters' response capabilities and safety are improved.
Patent Information
- Application Number
- CN202421316650.2
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2024-06-11
- Publication Date
- 2025-05-06
- Estimated Expiration
- 2034-06-11
AI Technical Summary
The prior art lacks fire-fighting training devices that are adapted to different types of aircraft, and cannot effectively simulate and deal with fire training in various aircraft.
An aircraft fire rescue real fire training device was designed, and a chamber structure was formed by splicing multiple boxes with each other, simulation modules, fire point modules, monitoring modules and emergency modules were set up to simulate the internal equipment and fire conditions of the aircraft, and equipped with video monitoring, temperature monitoring and combustible gas monitoring functions.
Real fire simulation training for different types of aircraft has been achieved, the response ability and safety of firefighters have been improved, and the effectiveness and safety of training have been ensured.
Smart Images
Figure CN222838512U_ABST
Abstract
Description
Technical Field
[0001] The utility model belongs to the technical field of aircraft fire fighting real fire training, and more specifically, relates to an aircraft fire fighting and rescue real fire training device. Background Art
[0002] Firefighting training with real fire is an important firefighting training method, which aims to enhance the firefighting commanders and fighters' ability to deal with various types of aircraft fire emergencies and protect the lives and property of the people.
[0003] Firefighters can train by simulating different types of aircraft fires in simulated venues to improve their abilities in fire fighting, firefighting, and personnel management.
[0004] Civil aviation firefighting also requires firefighting training to improve aircraft fire handling capabilities, but there are many types of aircraft, the structural layout of each type of aircraft is different, and the types of internal sudden fires are also different. Therefore, a device that can adapt to different fire training for various types of aircraft is needed. Utility Model Content
[0005] The purpose of the utility model is to provide an aircraft fire rescue real fire training device in view of the deficiencies in the prior art, so as to solve the problem that the prior art lacks fire training devices suitable for different types of aircraft.
[0006] In order to achieve the above-mentioned purpose, the utility model provides an aircraft fire rescue real fire training device, comprising:
[0007] A plurality of boxes, each box being provided with at least one hatch, and the boxes being able to be spliced together to form a communicating chamber structure;
[0008] A simulation module, which is disposed in the box and is used to simulate various equipment of the aircraft;
[0009] A fire point module, which is arranged on the box and the simulation module and is used to simulate the fire of each device of the aircraft individually or in conjunction with each other;
[0010] A monitoring module and an emergency module, wherein the monitoring module and the emergency module are arranged in the box, and the monitoring module includes a video monitoring unit, a temperature monitoring unit and a combustible gas monitoring unit.
[0011] Optionally, the chamber structure comprises:
[0012] A rear cargo hold box and a front cargo hold box, wherein the rear cargo hold box and the front cargo hold box are connected end to end;
[0013] A cabin box and a cockpit box, wherein the cabin box and the cockpit box are connected end to end and are in communication with each other;
[0014] The passenger cabin box is located above the rear cargo compartment box, and a first ladder is provided between the passenger cabin box and the rear cargo compartment box;
[0015] The cockpit box is located above the front cargo compartment box, and a second ladder is provided between the cockpit box and the front cargo compartment box.
[0016] Optionally, the rear cargo compartment box includes:
[0017] The head, middle and tail parts are connected in sequence, the head of the rear cargo hold box is close to the front cargo hold box, the head of the rear cargo hold box is provided with an air path room, and the middle part of the rear cargo hold box is provided with a fixed cargo cage and a movable cargo cage.
[0018] Optionally, the front cargo compartment box includes:
[0019] The head, middle and tail parts are connected in sequence, the tail part of the front cargo hold box is close to the rear cargo hold box, the tail part of the front cargo hold box is provided with a PLC control room, and the middle part of the front cargo hold box is provided with fixed shelves and / or mobile shelves.
[0020] Optionally, the cabin box includes:
[0021] The head, middle and tail parts are connected in sequence, the head part of the cabin box is provided with an isolation door connected with the cockpit box, the middle part of the cabin box is provided with a first seat, and the tail part of the cabin box is provided with a dining preparation area.
[0022] Optionally, the cockpit box includes:
[0023] The head, middle and tail parts are connected in sequence, the head part of the cockpit box is provided with a cab, the tail part of the cockpit box is provided with an isolation door connected with the cockpit box, and the middle part of the cockpit box is provided with a second seat and the second ladder.
[0024] Optionally, the chamber structure is suspended in the air by a bracket, and each of the boxes is provided with a staircase connected to the ground.
[0025] Optionally, it also includes:
[0026] An aircraft engine, the aircraft engine being arranged on one side of the chamber structure through a bracket;
[0027] A bridge gallery, one end of which is connected to the chamber structure, and the other end of which is close to the aircraft engine, and the bridge gallery is used to simulate an aircraft wing.
[0028] Optionally, the fire point module is arranged on the inner wall of the box or on the simulation module, and includes:
[0029] Flashover fire unit, used to simulate deflagration fire;
[0030] Wall fire unit, used to simulate line fire or bulkhead fire;
[0031] Smoke point, which is used to produce smoke and open flames;
[0032] A burning point, the burning point being used for ignition with an open flame;
[0033] A ground flowing fire point is arranged on the periphery of the chamber structure.
[0034] Optionally, the emergency module includes emergency exhaust equipment, emergency lighting equipment and a gas management emergency shut-off device, the emergency exhaust equipment and the emergency lighting equipment are arranged inside the chamber structure, and the gas management emergency shut-off device is used to cut off the fuel of the fire point module.
[0035] The utility model provides an aircraft fire rescue real fire training device, which has the following beneficial effects:
[0036] The aircraft fire rescue real fire training device is built into a chamber structure by splicing multiple boxes together to simulate the layout structure of a real aircraft. The simulation module is used to simulate various equipment and facilities inside the aircraft. The ignition module is used to provide various fire flames or combustion simulation modules to simulate the actual fire state. A single form of fire or a composite form of fire can be selected according to the training content. The monitoring module monitors the fire scene, and the emergency module is used for emergency firefighting to avoid training accidents. At the same time, each box is equipped with a monitoring module and an emergency module to ensure the safety of personnel during single training and the ability to safely extinguish fires.
[0037] Other features and advantages of the present invention will be described in detail in the subsequent specific implementation section. BRIEF DESCRIPTION OF THE DRAWINGS
[0038] The above and other objects, features and advantages of the present invention will become more apparent through a more detailed description of exemplary embodiments of the present invention in conjunction with the accompanying drawings, wherein the same reference numerals generally represent the same components in the exemplary embodiments of the present invention.
[0039] Figure 1 A structural schematic diagram of an aircraft firefighting and rescue real fire training device according to an embodiment of the utility model is shown.
[0040] Figure 2A structural schematic diagram of an aircraft engine of an aircraft fire rescue real fire training device according to an embodiment of the utility model is shown.
[0041] Description of reference numerals:
[0042] 11. Cockpit box; 12. Passenger cabin box; 13. Rear cargo box; 14. Front cargo box; 15. Driver's cab; 16. Isolation door; 17. Food preparation area; 18. Gas room; 19. PLC control room;
[0043] 21. First seat; 22. Second seat; 23. Fixed shelf; 24. Aircraft engine; 25. Fixed cargo cage; 26. Mobile cargo cage;
[0044] 31. Flashover fire unit; 32. Wall fire unit; 33. Smoke point; 34. Burning point; 35. Ground flow fire point;
[0045] 51. EMB fan; 52. Exhaust fan. DETAILED DESCRIPTION
[0046] The preferred embodiments of the present invention will be described in more detail below. Although the preferred embodiments of the present invention are described below, it should be understood that the present invention can be implemented in various forms and should not be limited by the embodiments described herein. On the contrary, these embodiments are provided to make the present invention more thorough and complete, and to fully convey the scope of the present invention to those skilled in the art.
[0047] like Figure 1-2 As shown, an aircraft fire rescue real fire training device comprises:
[0048] Multiple boxes, each box is provided with at least one hatch, and the boxes can be spliced together to form a connected chamber structure;
[0049] A simulation module, which is arranged in the box and is used to simulate various equipment of the aircraft;
[0050] Fire point module, which is set on the box and the simulation module and is used to simulate the fire of each device of the aircraft individually or in conjunction with each other;
[0051] The monitoring module and the emergency module are arranged in the box, and the monitoring module includes a video monitoring unit, a temperature monitoring unit and a combustible gas monitoring unit.
[0052] Specifically, multiple boxes are spliced together to form a chamber structure to simulate the layout structure of a real aircraft. The simulation module is used to simulate various equipment and facilities inside the aircraft. The ignition module is used to provide various fire flames or combustion simulation modules to simulate the actual fire state. A single form of fire or a composite form of fire can be selected according to the training content. The monitoring module monitors the fire scene, and the emergency module is used for emergency firefighting to avoid training accidents. At the same time, each box is equipped with a monitoring module and an emergency module to ensure the safety of personnel during single training and the ability to safely extinguish fires.
[0053] Furthermore, the boxes can be spliced or used independently, or divided into multiple spaces by partitions. At the same time, the box is equipped with at least an emergency module and a monitoring module to ensure the safety of personnel.
[0054] Furthermore, an emergency button is provided on the box body, which can directly trigger the emergency cut-off device of the emergency module. The fuel tank of the ignition point module is arranged outside the training device and connected through a line.
[0055] In this embodiment, the chamber structure includes:
[0056] The rear cargo hold box 13 and the front cargo hold box 14 are connected end to end;
[0057] The cabin box 12 and the cockpit box 11 are connected end to end and are interconnected.
[0058] The passenger cabin box 12 is located above the rear cargo compartment box 13, and a first ladder is provided between the passenger cabin box 12 and the rear cargo compartment box 13;
[0059] The cockpit box 11 is located above the front cargo compartment box 14 , and a second ladder is provided between the cockpit box 11 and the front cargo compartment box 14 .
[0060] Specifically, the four boxes, namely the rear cargo hold box 13, the front cargo hold box 14, the passenger cabin box 12 and the cockpit box 11, are spliced into a two-layer chamber structure, which fits the layout of an actual passenger aircraft.
[0061] In this embodiment, the rear cargo compartment box 13 includes:
[0062] The head, middle and tail parts are connected in sequence, the head of the rear cargo hold box 13 is close to the front cargo hold box 14, the head of the rear cargo hold box 13 is provided with an air path room 18, and the middle part of the rear cargo hold box 13 is provided with a fixed cargo cage 25 and a movable cargo cage 26.
[0063] Specifically, the simulation module is set according to the actual aircraft structure, and both the fixed cargo cage 25 and the mobile cargo cage 26 can be provided with a fire point module or various combustibles to adapt to different cargo stacking and combustion conditions.
[0064] In this embodiment, the front cargo compartment box 14 includes:
[0065] The head, middle and tail parts are connected in sequence, the tail part of the front cargo hold box 14 is close to the rear cargo hold box 13, the tail part of the front cargo hold box 14 is provided with a PLC control room 19, and the middle part of the front cargo hold box 14 is provided with a fixed shelf 23 and / or a movable shelf.
[0066] Specifically, simulation modules are set according to the actual aircraft structure, and the fixed shelves 23 and mobile shelves are set according to the aircraft model. Different types of fire point modules can be set in sections to simulate fires caused by different reasons. The PLC control room 19 controls the opening and closing of the fire point module, monitoring module and emergency module, and transfers the control signal and monitoring signal to the external main control console.
[0067] In this embodiment, the cabin box 12 includes:
[0068] The head, middle and tail parts are connected in sequence, the head part of the cabin box 12 is provided with an isolation door 16 connected with the cockpit box 11, the middle part of the cabin box 12 is provided with a first seat 21, and the tail part of the cabin box 12 is provided with a dining preparation area 17.
[0069] Specifically, it is set according to the actual aircraft structure to improve the real effect, and it is also convenient to simulate the fire in the food preparation area 17.
[0070] In this embodiment, the cockpit box 11 includes:
[0071] The head, middle and tail parts are connected in sequence. The head part of the cockpit box 11 is provided with a cab 15, the tail part of the cockpit box 11 is provided with an isolation door 16 connected with the cockpit box 11, and the middle part of the cockpit box 11 is provided with a second seat 22 and a second ladder.
[0072] Specifically, according to the actual aircraft structure setting, to improve the real effect and also facilitate the simulation of the fire in the cockpit 15, the first seat 21 and the second seat 22 can be the same or different real seats, thereby simulating different combustion temperature gas environments.
[0073] Furthermore, the cab 15 may be provided with a driver's seat.
[0074] In this embodiment, the chamber structure is suspended in the air by a bracket, and each box is provided with a staircase connected to the ground.
[0075] Specifically, the chamber structure is suspended in the air by supporting a bracket to simulate the real size of an aircraft, thereby training the ability to perform high-altitude operations.
[0076] In this embodiment, it also includes:
[0077] The aircraft engine 24 is arranged on one side of the chamber structure through a bracket;
[0078] A bridge gallery, one end of which is connected to the chamber structure, and the other end of which is close to the aircraft engine 24, and the bridge gallery is used to simulate an aircraft wing.
[0079] Specifically, the aircraft wing fire state is simulated by the aircraft engine 24 and the bridge.
[0080] In this embodiment, the fire point module is arranged on the inner wall of the box or the simulation module, and includes:
[0081] A flash fire unit 31, used to simulate a flash fire;
[0082] A wall fire unit 32, used to simulate a line fire or a bulkhead fire;
[0083] Smoke point 33, smoke point 33 is used to produce smoke and open flame;
[0084] Burning point 34, burning point 34 is used for open flame ignition;
[0085] The ground flowing fire point 35 is arranged on the periphery of the chamber structure.
[0086] Specifically, various different fire point units are adapted to different fire transition states to ensure that the fire simulation is realistic and rich, and the fire spread, oil leakage and other conditions are simulated through the ground flowing fire point 35.
[0087] In this embodiment, the emergency module includes emergency exhaust equipment, emergency lighting equipment and a gas management emergency shut-off device. The emergency exhaust equipment and emergency lighting equipment systems are arranged inside the chamber structure, and the gas management emergency shut-off device is used to cut off the fuel of the fire point module.
[0088] Specifically, emergency exhaust equipment and emergency lighting equipment ensure the safety of the training process and ventilation and lighting for daily maintenance; the gas management emergency shut-off device is used to cut off the fuel of the fire point module, thereby extinguishing the fire by directly cutting off the fuel supply at the source or the separate fuel supply of the corresponding fire point module.
[0089] In this embodiment, when using an aircraft fire rescue real fire training device, take the use of a passenger aircraft as an example:
[0090] Four boxes with explosion-proof transparent windows on both sides form a double-layer chamber structure, exhaust fans 52, cameras, and emergency lights are set at both ends of the lower layer, and EMB fans 51, emergency lights, and cameras are set at the top of the upper layer;
[0091] The chamber structure is suspended by a bracket, and four boxes are respectively provided with stairs connected to the ground. The four boxes are a rear cargo box 13, a front cargo box 14, a cabin box 12 and a cockpit box 11;
[0092] The rear cargo hold box 13 and the front cargo hold box 14 are connected end to end; the cabin box 12 and the cockpit box 11 are connected end to end, and the cabin box 12 and the cockpit box 11 are connected to each other; the cabin box 12 is located above the rear cargo hold box 13, and a first ladder is provided between the cabin box 12 and the rear cargo hold box 13; the cockpit box 11 is located above the front cargo hold box 14, and a second ladder is provided between the middle of the cockpit box 11 and the front cargo hold box 14;
[0093] The rear cargo hold box 13 includes a head, a middle and a tail connected in sequence, the head of the rear cargo hold box 13 is close to the front cargo hold box 14, the head of the rear cargo hold box 13 is provided with an air path 18, the middle of the rear cargo hold box 13 is provided with a fixed cargo cage 25 and a mobile cargo cage 26, and the fixed cargo cage 25 and the mobile cargo cage 26 are respectively provided with combustibles for simulating cargo combustion;
[0094] The front cargo hold box 14 includes a head, a middle and a tail connected in sequence, the tail of the front cargo hold box 14 is close to the rear cargo hold box 13, a PLC control room 19 is arranged at the tail of the front cargo hold box 14, the PLC control room 19 is externally connected to the console signal, and a fixed shelf 23 and / or a mobile shelf is arranged in the middle of the front cargo hold box 14;
[0095] The cabin box 12 includes a head, a middle and a tail connected in sequence. The head of the cabin box 12 is provided with an isolation door 16 communicating with the cockpit box 11. The middle of the cabin box 12 is provided with a first seat 21. The tail of the cabin box 12 is provided with a dining preparation area 17.
[0096] The cockpit box 11 includes a head, a middle and a tail connected in sequence. The head of the cockpit box 11 is provided with a cab 15. The tail of the cockpit box 11 is provided with an isolation door 16 connected to the cockpit box 11. The middle of the cockpit box 11 is provided with a second seat 22. The isolation door 16 separates the passenger areas, and the layouts of the various passenger areas are different.
[0097] An aircraft engine 24 is disposed on one side of the cockpit box 11, and a bridge gallery connected to the aircraft engine 24 is disposed on the cockpit box 11;
[0098] The flashover fire unit 31 is arranged on the top wall of the rear cargo hold box 13 and the front cargo hold box 14, and is used to simulate a sudden flashover fire;
[0099] The wall fire unit 32 is arranged on the side walls of the rear cargo compartment box 13 and the front cargo compartment box 14, and is used to simulate the internal circuit fire of the wall;
[0100] Smoke generating points 33, provided in the cabin box 12 and the cockpit box 11, for generating smoke;
[0101] A burning point 34, disposed below the first seat 21 and the second seat 22, for igniting the seats;
[0102] At the same time, the cab 15 and the meal preparation area 17 are also provided with corresponding types of ignition modules, and emergency stop fire extinguishing alarm buttons are provided near each ignition module.
[0103] The various embodiments of the utility model have been described above, and the above description is exemplary, not exhaustive, and is not limited to the disclosed embodiments. Many modifications and changes are obvious to those of ordinary skill in the art without departing from the scope and spirit of the described embodiments.
Claims
1. An aircraft fire rescue real fire training device, characterized in that: include: A plurality of boxes, each box being provided with at least one hatch, and the boxes being able to be spliced together to form a communicating chamber structure; A simulation module, which is disposed in the box and is used to simulate various equipment of the aircraft; A fire point module, which is arranged on the box and the simulation module and is used to simulate the fire of each device of the aircraft individually or in conjunction with each other; A monitoring module and an emergency module, wherein the monitoring module and the emergency module are arranged in the box, and the monitoring module includes a video monitoring unit, a temperature monitoring unit and a combustible gas monitoring unit.
2. The aircraft fire rescue real fire training device according to claim 1, characterized in that: The chamber structure comprises: A rear cargo hold box and a front cargo hold box, wherein the rear cargo hold box and the front cargo hold box are connected end to end; A cabin box and a cockpit box, wherein the cabin box and the cockpit box are connected end to end and are in communication with each other; The passenger cabin box is located above the rear cargo compartment box, and a first ladder is provided between the passenger cabin box and the rear cargo compartment box; The cockpit box is located above the front cargo compartment box, and a second ladder is provided between the cockpit box and the front cargo compartment box.
3. The aircraft fire rescue real fire training device according to claim 2, characterized in that: The rear cargo compartment box comprises: The head, middle and tail parts are connected in sequence, the head of the rear cargo hold box is close to the front cargo hold box, the head of the rear cargo hold box is provided with an air path room, and the middle part of the rear cargo hold box is provided with a fixed cargo cage and a movable cargo cage.
4. The aircraft fire rescue real fire training device according to claim 2, characterized in that: The front cargo compartment box comprises: The head, middle and tail parts are connected in sequence, the tail part of the front cargo hold box is close to the rear cargo hold box, the tail part of the front cargo hold box is provided with a PLC control room, and the middle part of the front cargo hold box is provided with fixed shelves and / or mobile shelves.
5. The aircraft fire rescue real fire training device according to claim 4, characterized in that: The cabin box comprises: The head, middle and tail parts are connected in sequence, the head part of the cabin box is provided with an isolation door connected with the cockpit box, the middle part of the cabin box is provided with a first seat, and the tail part of the cabin box is provided with a kitchen.
6. The aircraft fire rescue real fire training device according to claim 2, characterized in that: The cockpit box comprises: The head, middle and tail parts are connected in sequence, the head part of the cockpit box is provided with a cab, the tail part of the cockpit box is provided with an isolation door connected with the cockpit box, and the middle part of the cockpit box is provided with a second seat and the second ladder.
7. The aircraft fire rescue real fire training device according to claim 1, characterized in that: The chamber structure is suspended in the air by a bracket, and each box body is respectively provided with a staircase connected to the ground.
8. The aircraft fire rescue real fire training device according to claim 1, characterized in that: Also includes: An aircraft engine, the aircraft engine being arranged on one side of the chamber structure through a bracket; A bridge gallery, one end of which is connected to the chamber structure, and the other end of which is close to the aircraft engine, and the bridge gallery is used to simulate an aircraft wing.
9. The aircraft fire rescue real fire training device according to claim 1, characterized in that: The fire point module is arranged on the inner wall of the box or on the simulation module, and includes: Flashover fire unit, used to simulate deflagration fire; Wall fire unit, used to simulate line fire or bulkhead fire; Smoke point, which is used to produce smoke and open flames; A burning point, the burning point being used for ignition with an open flame; A ground flowing fire point is arranged on the periphery of the chamber structure.
10. The aircraft fire rescue real fire training device according to claim 1, characterized in that: The emergency module includes emergency exhaust equipment, emergency lighting equipment and a gas management emergency cut-off device. The emergency exhaust equipment and the emergency lighting equipment are arranged inside the chamber structure. The gas management emergency cut-off device is used to cut off the fuel of the fire point module.