CN2667594Y - Simulator for training emergency rescue - Google Patents
Simulator for training emergency rescue Download PDFInfo
- Publication number
- CN2667594Y CN2667594Y CN 200320129609 CN200320129609U CN2667594Y CN 2667594 Y CN2667594 Y CN 2667594Y CN 200320129609 CN200320129609 CN 200320129609 CN 200320129609 U CN200320129609 U CN 200320129609U CN 2667594 Y CN2667594 Y CN 2667594Y
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- China
- Prior art keywords
- main body
- simulator according
- inner chamber
- gas
- training
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- 229910000831 Steel Inorganic materials 0.000 claims description 12
- 239000010959 steel Substances 0.000 claims description 12
- 238000009423 ventilation Methods 0.000 claims description 5
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims description 3
- 229910052782 aluminium Inorganic materials 0.000 claims description 3
- 239000004411 aluminium Substances 0.000 claims description 3
- 239000011248 coating agent Substances 0.000 claims description 3
- 238000000576 coating method Methods 0.000 claims description 3
- 239000000463 material Substances 0.000 claims description 3
- 206010000369 Accident Diseases 0.000 abstract description 3
- 230000001629 suppression Effects 0.000 description 4
- 239000000446 fuel Substances 0.000 description 2
- 238000010586 diagram Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000004088 simulation Methods 0.000 description 1
Images
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- Fire-Extinguishing By Fire Departments, And Fire-Extinguishing Equipment And Control Thereof (AREA)
Abstract
The utility model relates to an emergent rescue train simulating device, which comprises a main body which is externally and internally similar to an airplane, an igniting torch system, an electric controlling system and an emergent controlling faceplates arranged in cavity and the external part of the main body. The bottom of the main body is provided with a supporting rack which contacts ground. The simulating device can be used for the fire accident training, antiterrorist and hijack training and in field shooting range of anti hijack situations of all airplanes. Furthermore, the utility model can also be used in escaping exercises, emergency rescue in accident status, moving exercises of wrecked airplane after accident and medical rescue rehearsal.
Description
Technical field
The utility model relates to a kind of simulator, specifically, relates to a kind of emergency management and rescue training simulators.
Background technology
When aircraft causes body, wing or engine to catch fire owing to accident, perhaps in the landing process because misoperation, perhaps after the other accident generation drift off the runway air crash accident, ground rescue team is transferred to the safety area with the passenger rapidly, and removing the aircraft accident condition rapidly is a very urgent thing.Hijacking takes place on aircraft, and anti-terrorism Convention for the Suppression of Unlawful Seizure of Aircraft army is ensureing that solving terrorist incident under passenger and the aircraft security prerequisite is a very difficult thing.At present, catch fire for aircraft, igniting rehearsal in oil drum is generally adopted in simulated training, and the not real impression of exercise personnel can not have good training effect.For the emergency management and rescue under the aircraft accident condition and to the disposal of anti-terrorism Convention for the Suppression of Unlawful Seizure of Aircraft incident, there is not the simulation trainer of real scene yet.
The utility model content
The purpose of this utility model is at the problems referred to above, and a kind of emergency management and rescue training simulators are provided.
Emergency management and rescue training simulators described in the utility model comprise profile and inner all with aircraft is the same really main body, lighting-off torch system, electric control system with in the inner chamber and the outer setting of main body the emergency control panel are arranged, are provided with the bracing frame on support ground in lower body part.
Described lighting-off torch system comprises gas distributing system and is arranged near each engine and easily catches fire the automatic ignitor place, that have safety feature during aviation accident.
Described gas distributing system comprises source of the gas by the dispensing of electric control system realization fuel, air delivering pipeline that is connected with source of the gas and the valving that is positioned on trunk line and each subtube.
Described electric control system comprises a master control computer and is installed in temperature sensor, the gas concentration sensor at each position of main body inner chamber.
Described main body inner chamber is provided with ventilation unit and safety feature.
Lay respectively at leading edge position, body both sides and body afterbody below on the described main body and be provided with the orcible entry position of aluminium matter covering.
The hatch door of main body is provided with night-mark(ing), and this sign is a kind of rectangular panel by Noctilucent material system.
Described main body adopts full steel structure, and the skeleton of its holding capacity adopts joist steel, channel-section steel or stringer; Shell utilizes sheet steel to make covering, and its outside surface scribbles frie retardant coating.
Passenger and terrorist's manikin is installed at the main body inner chamber.
Actual combat target range when emergency management and rescue training simulators described in the utility model can be used as the exercise of exercise, anti-terrorism Convention for the Suppression of Unlawful Seizure of Aircraft, the Convention for the Suppression of Unlawful Seizure of Aircraft of various aircraft fires, the handling exercise of residual machine, medical aid rehearsal behind the emergency management and rescue when escape exercise, accident condition, the accident condition.
Below in conjunction with example and accompanying drawing emergency management and rescue training simulators described in the utility model are described in detail.
Description of drawings
Fig. 1 is the front view of emergency management and rescue training simulators described in the utility model;
Fig. 2 is the top view of Fig. 1;
Fig. 3 is the synoptic diagram that shell has the orcible entry position.
Embodiment
Referring to Fig. 1 and Fig. 2, emergency management and rescue training simulators described in the utility model comprise simulator main body 1, lighting-off torch system 3, electric control system and in the inner chamber and the outer setting of main body the emergency control panel are arranged.The emergency control panel has the emergency cut-off source of the gas and opens the button of ventilation unit.The plausible aircraft of the equal class of the profile of described main body and interior shape promptly is a real model aircraft, and its underpart is provided with bracing frame 2 so that be supported in ground.This main body adopts full steel structure, and the skeleton of its holding capacity adopts joist steel, channel-section steel or stringer, and shell utilizes sheet steel to make covering, and its outside surface scribbles frie retardant coating, to strengthen the anti-ablative of body.
Described lighting-off torch system comprises gas distributing system 3 and is arranged near each engine and easily catches fire automatic ignitor 6 place, that have safety feature (there is sale in market, as SBN-GS series burner) during aviation accident.The effect of described gas distributing system is in order to realize the control and the different training program of the intensity of a fire to be controlled the independent of condition of a fire happening part, comprise source of the gas 4, air delivering pipeline 5 that is connected with source of the gas and the valving (not looking out) that is positioned on trunk line and each subtube are realized the dispensing of fuel by electric control system.
Described main body 1 inner chamber is provided with ventilation unit and safety alarm device, so that in case of emergency ventilate and warning.
Referring to Fig. 3, be positioned at the orcible entry position 7 that leading edge position, body both sides and body afterbody below is respectively equipped with aluminium matter covering on the main body 1, to carry out body orcible entry training.
Described electric control system (not looking out) is similar to industrial control system, comprises a master control computer, temperature sensor, gas concentration sensor.When temperature sensor and gas concentration sensor are picked up when surveying road air themperature and gas concentration and being higher than setting value, give the alarm, but the button that field staff's IMU is crossed on the panel cuts off source of the gas, control signal transfers to by Circuits System and respectively controls the position, as automatic ignitor, valving, ventilation unit, safety feature etc., and its feedback signal is by the temperature sensor at each position of being installed in the main body inner chamber and need testing, gas concentration sensors etc. transfer to the master control computer, for operating personnel provide the control foundation, and current events provide training on-the-spot truth, guarantee training program smoothly, safety is carried out.
Control system is positioned at the pulpit within the training of safety scope, and the control system of pulpit is connected with simulator by the operation circuit of burying underground.
The hatch door of main body 1 is provided with night-mark(ing), and this sign is a kind of rectangular panel that is made by Noctilucent material, is used to remind orientation, the security of direction to guarantee to train of trainer fire exit and passage.
Anti-terrorism is counter robs when training carrying out, and passenger and terrorist's manikin can be installed in main body, rehearsal when training for the trainer, and perhaps true man practice.
Claims (9)
1, emergency management and rescue training simulators, it is characterized in that comprising all the same main body (1) of profile and interior shape, lighting-off torch system (3), electric control system and the emergency control panel is arranged, be provided with the bracing frame (2) that supports ground in lower body part in the inner chamber and the outer setting of main body with real aircraft.
2, simulator according to claim 1 is characterized in that described lighting-off torch system comprises gas distributing system (3) and is arranged near each engine and easily catches fire automatic ignitor (6) place, that have safety feature during aviation accident.
3, simulator according to claim 1 and 2 is characterized in that described gas distributing system comprises source of the gas (4), the air delivering pipeline that is connected with source of the gas (5) and be positioned at valving on trunk line and each subtube.
4, simulator according to claim 3 is characterized in that described electric control system comprises a master control computer and the temperature sensor, the gas concentration sensor that are installed in main body (1) each position of inner chamber.
5, simulator according to claim 4 is characterized in that described main body (1) inner chamber is provided with ventilation unit and safety feature.
6, simulator according to claim 5 is characterized in that laying respectively on the described main body (1) the orcible entry position (7) that leading edge position, body both sides and body afterbody below is provided with aluminium matter covering.
7, simulator according to claim 6 is characterized in that the hatch door of main body (1) is provided with night-mark(ing), and this sign is a kind of rectangular panel by Noctilucent material system.
8, simulator according to claim 7 is characterized in that described main body (1) adopts full steel structure, and the skeleton of its holding capacity adopts joist steel, channel-section steel or stringer; Shell utilizes sheet steel to make covering, and its outside surface scribbles frie retardant coating.
9, simulator according to claim 8 is characterized in that being equipped with at the main body inner chamber passenger and terrorist's manikin.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 200320129609 CN2667594Y (en) | 2003-12-19 | 2003-12-19 | Simulator for training emergency rescue |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 200320129609 CN2667594Y (en) | 2003-12-19 | 2003-12-19 | Simulator for training emergency rescue |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN2667594Y true CN2667594Y (en) | 2004-12-29 |
Family
ID=34349985
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 200320129609 Expired - Fee Related CN2667594Y (en) | 2003-12-19 | 2003-12-19 | Simulator for training emergency rescue |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN2667594Y (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103996320A (en) * | 2014-05-20 | 2014-08-20 | 天津航佳机场设备科技有限公司 | Airplane entity fire training simulator |
| CN103996321A (en) * | 2014-05-20 | 2014-08-20 | 天津航佳机场设备科技有限公司 | Aircraft cabin firefighting forcible entry training device |
| CN107038945A (en) * | 2017-05-09 | 2017-08-11 | 中安（天津）航空设备有限公司 | A kind of split type practice device |
| CN107067874A (en) * | 2017-01-24 | 2017-08-18 | 佛山市三水区希望火炬教育科技有限公司 | A kind of helicopter of the special suitable desert area anti-terrorism of teenager's national defence research |
| CN112071159A (en) * | 2020-09-21 | 2020-12-11 | 航大联合航空设备有限公司 | Aviation simulator for ground real-practice drilling and simulation use method thereof |
-
2003
- 2003-12-19 CN CN 200320129609 patent/CN2667594Y/en not_active Expired - Fee Related
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103996320A (en) * | 2014-05-20 | 2014-08-20 | 天津航佳机场设备科技有限公司 | Airplane entity fire training simulator |
| CN103996321A (en) * | 2014-05-20 | 2014-08-20 | 天津航佳机场设备科技有限公司 | Aircraft cabin firefighting forcible entry training device |
| CN107067874A (en) * | 2017-01-24 | 2017-08-18 | 佛山市三水区希望火炬教育科技有限公司 | A kind of helicopter of the special suitable desert area anti-terrorism of teenager's national defence research |
| CN107038945A (en) * | 2017-05-09 | 2017-08-11 | 中安（天津）航空设备有限公司 | A kind of split type practice device |
| CN112071159A (en) * | 2020-09-21 | 2020-12-11 | 航大联合航空设备有限公司 | Aviation simulator for ground real-practice drilling and simulation use method thereof |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C56 | Change in the name or address of the patentee | ||
| CP03 | Change of name, title or address |
Patentee address after: 100176 room 36, floor 201, Tulip House, Yizhuang Development Zone, Beijing Patentee address before: 100012 Beijing City, Chaoyang District Asian Sports Village huizhongbeili Huaxin apartment 412-3-101 |
|
| C19 | Lapse of patent right due to non-payment of the annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |