CN103996320A - Airplane entity fire training simulator - Google Patents
Airplane entity fire training simulator Download PDFInfo
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- CN103996320A CN103996320A CN201410211895.3A CN201410211895A CN103996320A CN 103996320 A CN103996320 A CN 103996320A CN 201410211895 A CN201410211895 A CN 201410211895A CN 103996320 A CN103996320 A CN 103996320A
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- fire
- wing
- aircraft
- distribution cabinet
- airplane
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Abstract
An airplane entity fire training simulator comprises a cylindrical cabin, wings on the two sides, propeller type engines, undercarriages, airplane wheels, jet engines, an empennage, a gas distribution cabinet, an electric control cabinet and a computer remote control system. The two sides of the cylindrical cabin are respectively provided with a cabin door and the corresponding wing. The bottom surface of each wing is connected with the corresponding propeller type engine or the corresponding jet engine and the corresponding undercarriage, and each airplane wheel is arranged at the bottom of the corresponding undercarriage. The empennage is arranged at the tail of the cabin. The gas distribution cabinet is connected with a gas station, and the electric control cabinet is electrically connected with an intelligent integrated electric fitting on the gas distribution cabinet and with the computer remote control system. According to the airplane entity fire training simulator, the parts can be matched and combined into various forms, lifting of the simulator is controlled through a screw, and the simulator can be used for fire training of different types of airplanes. The airplane entity fire training simulator is made of steel and is long in service life. The computer remote control system is adopted for achieving ignition, flameout and control over the intensity of a fire, security and environmental protection are achieved, the degree of similarity to a real airplane fire is high, and the fire training effect is good.
Description
Technical field
The present invention relates to a kind of fire drill simulator, particularly relate to a kind of simulator that carries out aircraft entity fire fire drill for airport fire-fighting and rescue personnel, belong to fire drill equipment technical field.
Background technology
For the casualty loss that crash fire is caused drops to minimum, airport fire-fighting and rescue personnel need to actively develop the fire drill for different type of machines, the ability of disposing true accident to improve it.
At present, most of airport adopts the true aircraft of certain type or special vehicle as imaginary wrecked aircraft, by throwing the mode of aerosol producer, builds fire scenario, and fire drill personnel utilize this virtual scene to train.But because this mode whole process there is no kidney-yangly, thereby fire-fighting participant is difficult to conscientiously to experience the kidney-yang fear of bringing, so the on-site experience of accumulation is very limited.
Some military airfields or large-scale civil airport utilization are scrapped aircraft and are carried out fire drill, but the material of scrapping aircraft is identical, comparatively inflammable with true aircraft, and burning condition is controlled the bad aircraft that easily causes and directly burnt or explode, and discharge toxic gas, thereby be unfavorable for safety and environment protection.In addition, scrap aircraft and can be destroyed by big fire very soon, serviceable life is short, therefore cannot repeatedly train.
Summary of the invention
In order to address the above problem, the object of the present invention is to provide a kind of aircraft entity fire fire drill simulator, for airport fire-fighting and rescue personnel, carry out aircraft entity fire fire drill.
In order to achieve the above object, aircraft entity fire fire drill simulator provided by the invention comprises cylindrical shape cabin body, both sides wing, propeller type engine, undercarriage, wheel, jet engine, empennage, gas distribution cabinet, electrical control cubicles and computer remote control system; Wherein the bottom of cylindrical shape cabin body by a front standing pillar and two back prop settings on the ground, is respectively equipped with hatch door on two sides, is connected with respectively a wing on two sides simultaneously; On the bottom surface of each wing, be at least connected with a propeller type engine or jet engine, and undercarriage is also installed on the bottom surface of wing, undercarriage bottom is provided with wheel; Empennage is arranged on cylindrical shape cabin body afterbody, and is equipped with gas nozzle on the surface of cylindrical shape cabin body, wing, propeller type engine, undercarriage, wheel, jet engine and hatch door; Gas distribution cabinet and electrical control cubicles are embedded in the subsurface that is positioned at body below, cylindrical shape cabin, wherein gas distribution cabinet is connected to gas station at a distance by underground gas pipeline, by supply air line, be connected with above-mentioned each gas nozzle, electrical control cubicles is electrically connected to intelligent integral Denso and computer remote control system on gas distribution cabinet simultaneously simultaneously.
Supply air line porch in described gas distribution cabinet is also provided with burnt gas valve, and burnt gas valve is connected with intelligent integral Denso, can utilize intelligent integral Denso to control switching and the uninterrupted of supply air line.
On described empennage, be also connected with a jet engine.
Described both sides wing is symmetric mode or the just mode that is arranges.
Ball-screw is all equipped with in the inside of described front standing pillar and back prop and undercarriage, for regulating the height of aircraft entity fire fire drill simulator.
Described front standing pillar and back prop are provided with the scale of being convenient to observe aircraft entity fire fire drill simulator height.
Described body inside, cylindrical shape cabin is provided with seat, and single channel pressed by seat or binary channels is arranged.
On described gas nozzle, be all furnished with burning torch, the ignition control switch of burning torch is positioned at electrical control cubicles, and realizes igniting with flame-out by computer remote control system.
Described intelligent integral Denso is switching mode or and adjustment type.
Between described computer remote control system and electrical control cubicles, be connected to wired or wireless mode.
Aircraft entity fire fire drill simulator provided by the invention, its each position can matched combined become various ways, adopts the lifting of leading screw control simulation device, can carry out fire drill for different type of machines; Structure adopts steel, long service life; Adopt computer remote control system to realize igniting, extinguishing and the control of intensity of a fire size, safety and environmental protection, high with true aircraft fire approach degree, fire drill is respond well.
Accompanying drawing explanation
Fig. 1 is aircraft entity fire fire drill simulator structure schematic diagram provided by the invention.
Fig. 2 is the aircraft entity fire fire drill simulator structure schematic diagram that empennage provided by the invention connects a jet engine.
Fig. 3 is both sides provided by the invention wing symmetry and the aircraft entity fire fire drill simulator structure schematic diagram that connects respectively a propeller type engine.
Fig. 4 is the aircraft entity fire fire drill simulator structure schematic diagram that lower wing provided by the invention connects two jet engines.
Fig. 5 is both sides provided by the invention wing symmetry and the aircraft entity fire fire drill simulator structure schematic diagram that connects respectively a jet engine.
Fig. 6 is both sides provided by the invention wing high level matches with low level and the aircraft entity fire fire drill simulator structure schematic diagram that connects respectively a jet engine.
Fig. 7 is seat deployment scenarios schematic diagram in aircraft entity fire fire drill simulator upper-deck cabin provided by the invention.
Fig. 8 is scale schematic diagram on aircraft entity fire fire drill simulator provided by the invention.
Embodiment
Below technical solution of the present invention is elaborated, but protection scope of the present invention is not limited to described embodiment.
As Figure 1-Figure 8, aircraft entity fire fire drill simulator provided by the invention comprises cylindrical shape cabin body 1, both sides wing 2, propeller type engine 3, undercarriage 5, wheel 8, jet engine 13, empennage 16, gas distribution cabinet 9, electrical control cubicles 10 and computer remote control system 14; Wherein the bottom of cylindrical shape cabin body 1 arranges on the ground by a front standing pillar 11 and two back props 6, is respectively equipped with hatch door 15 on two sides, is connected with respectively a wing 2 on two sides simultaneously; On the bottom surface of each wing 2, be at least connected with a propeller type engine 3 or jet engine 13, and undercarriage 5 is also installed on the bottom surface of wing 2, undercarriage 5 bottoms are provided with wheel 8; Empennage 16 is arranged on cylindrical shape cabin body 1 afterbody, and is equipped with gas nozzle on the surface of cylindrical shape cabin body 1, wing 2, propeller type engine 3, undercarriage 5, wheel 8, jet engine 13 and hatch door 15; Gas distribution cabinet 9 and electrical control cubicles 10 are embedded in the subsurface that is positioned at body 1 below, cylindrical shape cabin, wherein gas distribution cabinet 9 is connected to gas station 4 at a distance by underground gas pipeline 7, by supply air line, be connected with above-mentioned each gas nozzle, 10 whiles of electrical control cubicles are electrically connected to intelligent integral Denso and computer remote control system 14 on gas distribution cabinet 9 simultaneously.
Supply air line porch in described gas distribution cabinet 9 is also provided with burnt gas valve, and burnt gas valve is connected with intelligent integral Denso, can utilize intelligent integral Denso to control switching and the uninterrupted of supply air line.
On described empennage 16, be also connected with a jet engine 13.
Described both sides wing 2 is symmetric mode or the just mode that is arranges.
Ball-screw is all equipped with in the inside of described front standing pillar 11 and back prop 6 and undercarriage 5, for regulating the height of aircraft entity fire fire drill simulator.
Described front standing pillar 11 and back prop 6 are provided with the scale 12 of being convenient to observe aircraft entity fire fire drill simulator height.
Described body 1 inside, cylindrical shape cabin is provided with seat 17, and single channel pressed by seat 17 or binary channels is arranged.
On described gas nozzle, be all furnished with burning torch, the ignition control switch of burning torch is positioned at electrical control cubicles 10, and realizes igniting with flame-out by computer remote control system 14.
Described intelligent integral Denso is switching mode or and adjustment type.
Between described computer remote control system 14 and electrical control cubicles 10, be connected to wired or wireless mode.
Now the principle of work of aircraft entity fire fire drill simulator provided by the invention is described below: when needs utilize aircraft entity fire fire drill simulator simulated fire provided by the invention a situation arises, first utilize computer remote control system 14 to open burnt gas valve by the intelligent integral Denso in electrical control cubicles 10, at this moment, in gas station 4, comprise propane, rock gas, liquefied petroleum gas (LPG) or other air mixtures will offer each gas nozzle by gas pipeline 7 and supply air line in interior combustion gas, utilize the ignition control switch in electrical control cubicles 10 to open burning torch simultaneously, thereby combustion gas is ignited at gas nozzle place, build thus a real scene of fire, at this moment the airport fire-fighting and rescue personnel that participate in training just can take the measure of putting out a fire accordingly to train according to the concrete condition of a fire.
As mentioned above, although represented and explained the present invention with reference to specific preferred embodiment, it shall not be construed as inventing the restriction of self.Do not departing under the spirit and scope of the present invention prerequisite of claims definition, can in array configuration and CONSTRUCTED SPECIFICATION, make a variety of changes each position of the present invention, for example, if both sides wing 2 is symmetric mode setting, as shown in Figure 3, can connect a propeller type engine 32 times at each wing, or as shown in Figure 5, can connect a jet engine 13 2 times at each wing.If both sides wing 2 is height, mode arranges, as shown in Figure 2, can on higher wing 2, connect propeller type engine 3, on lower wing 2, connect jet engine 13, or as shown in Figure 4, on lower wing 2, connect two jet engines 13, also can as shown in Figure 6, on both sides wing 2, all connect a jet engine 13.
Claims (10)
1. an aircraft entity fire fire drill simulator, is characterized in that: it comprises cylindrical shape cabin body (1), both sides wing (2), propeller type engine (3), undercarriage (5), wheel (8), jet engine (13), empennage (16), gas distribution cabinet (9), electrical control cubicles (10) and computer remote control system (14); Wherein the bottom of cylindrical shape cabin body (1) arranges on the ground by a front standing pillar (11) and two back props (6), is respectively equipped with hatch door (15) on two sides, is connected with respectively a wing (2) on two sides simultaneously; On the bottom surface of each wing (2), be at least connected with a propeller type engine (3) or jet engine (13), and undercarriage (5) is also installed on the bottom surface of wing (2), and undercarriage (5) bottom is provided with wheel (8); Empennage (16) is arranged on cylindrical shape cabin body (1) afterbody, and is equipped with gas nozzle on the surface of cylindrical shape cabin body (1), wing (2), propeller type engine (3), undercarriage (5), wheel (8), jet engine (13) and hatch door (15); Gas distribution cabinet (9) and electrical control cubicles (10) are embedded in the subsurface that is positioned at cylindrical shape cabin body (1) below, wherein gas distribution cabinet (9) is connected to gas station (4) at a distance by underground gas pipeline (7), by supply air line, be connected with above-mentioned each gas nozzle, electrical control cubicles (10) is electrically connected to intelligent integral Denso and computer remote control system (14) on gas distribution cabinet (9) simultaneously simultaneously.
2. aircraft entity fire fire drill simulator according to claim 1, it is characterized in that: the supply air line porch in described gas distribution cabinet (9) is also provided with burnt gas valve, and burnt gas valve is connected with intelligent integral Denso, can utilize intelligent integral Denso to control switching and the uninterrupted of supply air line.
3. aircraft entity fire fire drill simulator according to claim 1, is characterized in that: on described empennage (16), be also connected with a jet engine (13).
4. aircraft entity fire fire drill simulator according to claim 1, is characterized in that: described both sides wing (2) is symmetric mode or the just mode that is arranges.
5. aircraft entity fire fire drill simulator according to claim 1, it is characterized in that: ball-screw is all equipped with in the inside of described front standing pillar (11) and back prop (6) and undercarriage (5), for regulating the height of aircraft entity fire fire drill simulator.
6. aircraft entity fire fire drill simulator according to claim 1, is characterized in that: described front standing pillar (11) and back prop (6) are provided with the scale (12) of being convenient to observe aircraft entity fire fire drill simulator height.
7. aircraft entity fire fire drill simulator according to claim 1, is characterized in that: described cylindrical shape cabin body (1) inside is provided with seat (17), and single channel pressed by seat (17) or binary channels is arranged.
8. aircraft entity fire fire drill simulator according to claim 1, it is characterized in that: on described gas nozzle, be all furnished with burning torch, the ignition control switch of burning torch is positioned at electrical control cubicles (10), and realizes igniting with flame-out by computer remote control system (14).
9. aircraft entity fire fire drill simulator according to claim 1, is characterized in that: described intelligent integral Denso is switching mode or and adjustment type.
10. aircraft entity fire fire drill simulator according to claim 1, is characterized in that: between described computer remote control system (14) and electrical control cubicles (10), be connected to wired or wireless mode.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410211895.3A CN103996320A (en) | 2014-05-20 | 2014-05-20 | Airplane entity fire training simulator |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410211895.3A CN103996320A (en) | 2014-05-20 | 2014-05-20 | Airplane entity fire training simulator |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN103996320A true CN103996320A (en) | 2014-08-20 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201410211895.3A Pending CN103996320A (en) | 2014-05-20 | 2014-05-20 | Airplane entity fire training simulator |
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| CN (1) | CN103996320A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108905036A (en) * | 2018-04-11 | 2018-11-30 | 中国船舶重工集团公司第七0三研究所 | A kind of aircraft fire disaster simulation training equipment |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5052933A (en) * | 1990-10-29 | 1991-10-01 | Symtron Systems, Inc. | Fire fighter trainer |
| US5415551A (en) * | 1992-12-24 | 1995-05-16 | R2 | Aircraft firefighter trainer |
| US5688136A (en) * | 1995-12-15 | 1997-11-18 | Symtron Systems, Inc. | Fire fighting trainer |
| CN2667594Y (en) * | 2003-12-19 | 2004-12-29 | 马玉山 | Simulator for training emergency rescue |
-
2014
- 2014-05-20 CN CN201410211895.3A patent/CN103996320A/en active Pending
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5052933A (en) * | 1990-10-29 | 1991-10-01 | Symtron Systems, Inc. | Fire fighter trainer |
| US5415551A (en) * | 1992-12-24 | 1995-05-16 | R2 | Aircraft firefighter trainer |
| US5688136A (en) * | 1995-12-15 | 1997-11-18 | Symtron Systems, Inc. | Fire fighting trainer |
| CN2667594Y (en) * | 2003-12-19 | 2004-12-29 | 马玉山 | Simulator for training emergency rescue |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108905036A (en) * | 2018-04-11 | 2018-11-30 | 中国船舶重工集团公司第七0三研究所 | A kind of aircraft fire disaster simulation training equipment |
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Application publication date: 20140820 |