CN210428900U - Airplane simulation cabin for fire drill - Google Patents
Airplane simulation cabin for fire drill Download PDFInfo
- Publication number
- CN210428900U CN210428900U CN201921108720.4U CN201921108720U CN210428900U CN 210428900 U CN210428900 U CN 210428900U CN 201921108720 U CN201921108720 U CN 201921108720U CN 210428900 U CN210428900 U CN 210428900U
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- cabin
- cabin body
- wall
- fire
- convenient
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- Expired - Fee Related
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Abstract
The utility model discloses an aircraft simulation cabin for fire drill only is equipped with an ignition point to current cabin, is not convenient for develop the fire drill, is not convenient for put out a fire emergency training to the air crew member to be not convenient for add the fuel problem toward the ignition point in, now proposes following scheme, and it includes the cabin body, the welding has four group's bracing pieces on the bottom inner wall of the cabin body, and the quantity of every group bracing piece is two, and the top welding that is located two bracing pieces of same group has same burning fill, and the top fixed mounting of the cabin body has the fuel tank, and fixed mounting has the push rod motor on the top inner wall of fuel tank, and the welding has the slurcam on the output shaft of push rod motor, and first sunshade has all been welded to the bottom both sides of slurcam. The utility model discloses the practicality is good, is convenient for develop the fire drill, is convenient for put out a fire emergency training to the air crew member, is convenient for add fuel toward in the fuel hopper.
Description
The technical field is as follows:
the utility model relates to a simulation cabin technical field especially relates to an aircraft simulation cabin for fire drill.
Background art:
the aircraft simulation cabin is designed in a simulation mode according to the size of the aircraft cabin, and fire drilling can be performed according to the aircraft simulation cabin.
Only be equipped with an ignition point on the current cabin, be not convenient for develop the fire drill, be not convenient for carry out the emergent training of putting out a fire to the air crew member to it adds fuel to be not convenient for in the ignition point.
The utility model has the following contents:
an object of the utility model is to provide an aircraft simulation cabin for fire drill solves and only is equipped with an ignition point on having the cabin among the prior art, is not convenient for develop the fire drill, is not convenient for put out a fire emergent training to the air crew member to be not convenient for add the shortcoming of fuel in the ignition point.
The utility model discloses by following technical scheme implement: an aircraft simulation cabin for fire drilling comprises a cabin body, wherein four groups of supporting rods are welded on the inner wall of the bottom of the cabin body, the number of each group of supporting rods is two, the top ends of the two supporting rods in the same group are welded with the same combustion bucket, the top of the cabin body is fixedly provided with a fuel tank, the inner wall of the top of the fuel tank is fixedly provided with a push rod motor, the output shaft of the push rod motor is welded with a push plate, the two sides of the bottom of the push plate are welded with first shielding plates, the inner walls of the two sides of the fuel tank are respectively provided with a liquid outlet hole, a first pipe is fixedly arranged in the liquid outlet hole, the first shielding plate covers the liquid outlet hole, the inner wall of the top of the cabin body is provided with two sliding grooves, sliding plates are slidably arranged in the sliding grooves, one sides, the downthehole fixed mounting of embedding has the second pipe, the second pipe welds with first pipe mutually, has seted up the first hole on the bottom inner wall of fuel tank, the second hole has been seted up at the top of the cabin body, the downthehole slidable mounting of first hole and second has same riser, the top of riser welds with the bottom of slurcam, the front side of riser articulates there is the one end of two down tube, the other end of down tube articulates on corresponding slide, all weld on the output shaft of push rod motor and the riser has a plurality of swash plates.
Preferably, the bottom of the cabin body is welded with two vertical plates, and the bottom of each vertical plate is provided with a universal wheel in a rolling manner, so that the cabin body can move conveniently.
Preferably, the inner walls of the two sides of the cabin body are respectively provided with an air inlet hole and an air outlet hole.
Preferably, the second shield covers the insertion hole.
Preferably, the front side of the cabin body is hinged with a cabin door, and the front side of the cabin door is fixedly provided with a handle.
Preferably, a feeding hole is formed in the inner wall of one side of the fuel tank, and a plug plate is clamped in the feeding hole, so that feeding is facilitated.
The utility model has the advantages that: in the utility model, the aircraft simulation cabin for fire drill is provided with only one ignition point on the existing cabin, so that the fire drill is not convenient to develop and the emergency training for fire extinguishment for the air crew is not convenient, and a plurality of combustion hoppers are arranged;
because be not convenient for add fuel in toward the ignition point, consequently, the push rod motor has been set up, a vertical plate, the slurcam, the slide, first sunshade and second sunshade, start the push rod motor, the output shaft of push rod motor drives the slurcam and removes, the slurcam drives first sunshade and removes, first sunshade and play liquid hole phase separation, the slurcam drives the riser simultaneously and removes, the riser drives the down tube and rotates, the down tube drives the slide and removes, the slide drives the second sunshade and removes, make the guide hole be linked together with the inlay hole, the intraductal fuel of second flows into each fuel fill through the guide hole this moment, be convenient for add fuel in toward the fuel fill, and is simple in operation.
The utility model discloses the practicality is good, is convenient for develop the fire drill, is convenient for put out a fire emergency training to the air crew member, is convenient for add fuel toward in the fuel hopper.
Description of the drawings:
in order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings used in the description of the embodiments or the prior art will be briefly described below, it is obvious that the drawings in the following description are only some embodiments of the present invention, and for those skilled in the art, other drawings can be obtained according to these drawings without creative efforts.
Fig. 1 is a schematic structural diagram of an aircraft simulation cabin for fire drill according to the present invention;
fig. 2 is a schematic structural diagram of a part a of an aircraft simulation cabin for fire drill according to the present invention;
fig. 3 is a side view schematic structural diagram of an aircraft simulation cabin for fire drill provided by the utility model.
In the figure: 1 cabin body, 2 combustion hoppers, 3 fuel tanks, 4 push rod motors, 5 push plates, 6 first shielding plates, 7 first pipes, 8 second shielding plates, 9 guide holes, 10 second pipes, 11 vertical plates, 12 inclined plates, 13 sliding grooves, 14 sliding plates and 15 inclined rods.
The specific implementation mode is as follows:
the technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative efforts belong to the protection scope of the present invention.
Example one
Referring to fig. 1-3, an airplane simulation cabin for fire drill includes a cabin body 1, four sets of support rods are welded on the inner bottom wall of the cabin body 1, each set of support rods is two, the top end of the two support rods in the same set is welded with a same combustion bucket 2, the top of the cabin body 1 is fixedly provided with a fuel tank 3, the inner top wall of the fuel tank 3 is fixedly provided with a push rod motor 4, an output shaft of the push rod motor 4 is welded with a push plate 5, two sides of the bottom of the push plate 5 are both welded with first shielding plates 6, two inner side walls of the fuel tank 3 are both provided with liquid outlet holes, a first pipe 7 is fixedly arranged in the liquid outlet hole, the first shielding plates 6 cover the liquid outlet holes, two sliding grooves 13 are arranged on the inner top wall of the cabin body 1, sliding plates 14 are slidably arranged in the sliding grooves 13, two guide holes 9 have been seted up at the top of second sunshade 8, two embedding holes have been seted up at the top of the cabin body 1, the downthehole fixed mounting of embedding has a second pipe 10, second pipe 10 welds with first pipe 7 mutually, the first hole has been seted up on the bottom inner wall of fuel tank 3, the second hole has been seted up at the top of the cabin body 1, the downthehole slidable mounting of first hole and second has same riser 11, the top of riser 11 welds with the bottom of slurcam 5, the front side of riser 11 articulates the one end that has two down tube 15, the other end of down tube 15 articulates on corresponding slide 14, all weld on output shaft and the riser 11 of push rod motor 4 has a plurality of swash plates 12.
The utility model discloses in, the bottom welding of the cabin body 1 has two risers, and the bottom roll mounting of riser has the universal wheel.
The utility model discloses in, inlet port and venthole have been seted up on the both sides inner wall of the cabin body 1 respectively.
In the utility model discloses in, second sunshade 8 covers the embedding hole.
In the utility model, the front side of the cabin body 1 is hinged with a cabin door, and the front side of the cabin door is fixedly provided with a handle.
The utility model discloses in, seted up the charge cavity on one side inner wall of fuel-cell 3, the jam plate is equipped with to the card in the charge cavity.
Example two
Referring to fig. 1-3, an airplane simulation cabin for fire drilling comprises a cabin body 1, four groups of support rods are welded on the inner wall of the bottom of the cabin body 1, the number of each group of support rods is two, the top ends of the two support rods positioned in the same group are welded with a same combustion bucket 2, the top of the cabin body 1 is fixedly provided with a fuel tank 3 through bolts, the inner wall of the top of the fuel tank 3 is fixedly provided with a push rod motor 4 through bolts, an output shaft of the push rod motor 4 is welded with a push plate 5, two sides of the bottom of the push plate 5 are both welded with first shielding plates 6, two inner walls of two sides of the fuel tank 3 are both provided with liquid outlet holes, a first pipe 7 is fixedly provided in the liquid outlet holes through bolts, the first shielding plates 6 cover the liquid outlet holes, two sliding grooves 13 are provided on the inner wall of the top of the cabin body 1, two guide holes 9 have been seted up at the top of second sunshade 8, two embedding holes have been seted up at the top of the cabin body 1, there is second pipe 10 at the downthehole bolt fixed mounting of embedding, second pipe 10 welds with first pipe 7 mutually, the first hole has been seted up on the bottom inner wall of fuel tank 3, the second hole has been seted up at the top of the cabin body 1, the downthehole slidable mounting of first hole and second has same riser 11, the top of riser 11 welds with the bottom of slurcam 5, the front side of riser 11 articulates the one end that has two down tube 15, the other end of down tube 15 articulates on corresponding slide 14, all weld on the output shaft of push rod motor 4 and riser 11 has a plurality of swash plates 12.
The utility model discloses in, the bottom welding of the cabin body 1 has two risers, and the bottom roll mounting of riser has the universal wheel, the removal of the cabin body 1 of being convenient for.
The utility model discloses in, inlet port and venthole have been seted up on the both sides inner wall of the cabin body 1 respectively.
In the utility model discloses in, second sunshade 8 covers the embedding hole.
The utility model discloses in, the front side of the cabin body 1 articulates there is the hatch door, and there is the handle front side of hatch door through bolt fixed mounting.
The utility model discloses in, seted up the charge cavity on one side inner wall of fuel-tank 3, the jam plate is equipped with to the charge cavity inside callipers, is convenient for feed in raw material.
In the utility model, in use, a plurality of combustion hoppers 2 are arranged, when fire-fighting training is carried out, fuel in the plurality of fuel hoppers 2 can be ignited, fire-fighting drill is convenient to develop, fire-fighting emergency training is convenient to put out a fire for passengers in the air, and when fuel is added to the fuel hoppers 2, the push rod motor 4 is started, the push rod motor 4 is powered by the storage battery, the push rod motor 4 is controlled by the control switch, the output shaft of the push rod motor 4 drives the push plate 5 to move, the push plate 5 drives the first shielding plate 6 to move, the first shielding plate 6 is separated from the liquid outlet hole, at the moment, the fuel in the fuel tank 3 enters the second pipe 10 through the first pipe 7, the push plate 5 simultaneously drives the vertical plate 11 to move, the vertical plate 11 drives the diagonal rod 15 to rotate, the diagonal rod 15 drives the sliding plate 14 to move, the sliding plate 14 drives the second shielding plate 8 to move, the second sunshade 8 drives the guide hole 9 to move, the output shaft of the push rod motor 4 and the vertical plate 11 drive the inclined plate 12 to move, fuel in the fuel tank 3 is shaken, the guide hole 9 is communicated with the embedding hole, at the moment, fuel in the second pipe 10 flows into each fuel hopper 2 through the guide hole, fuel is convenient to add into the fuel hopper 2, and the operation is simple.
The above description is only a preferred embodiment of the present invention, and should not be taken as limiting the invention, and any modifications, equivalent replacements, improvements, etc. made within the spirit and principle of the present invention should be included in the protection scope of the present invention.
Claims (6)
1. The utility model provides an aircraft simulation cabin for fire drill, including the cabin body (1), a serial communication port, it has four groups of bracing pieces to weld on the bottom inner wall of the cabin body (1), the quantity of every group bracing piece is two, the top welding that is located two bracing pieces of same group has same burning fill (2), the top fixed mounting of the cabin body (1) has fuel tank (3), fixed mounting has push rod motor (4) on the top inner wall of fuel tank (3), the welding has catch plate (5) on the output shaft of push rod motor (4), first sunshade (6) have all been welded to the bottom both sides of catch plate (5), the liquid outlet has all been seted up on the both sides inner wall of fuel tank (3), fixed mounting has first pipe (7) in the liquid outlet, first sunshade (6) cover the liquid outlet, set up two spouts (13) on the top inner wall of the cabin body (1), sliding installation has slide (14) in, two slide (14) one side of keeping away from each other all weld second sunshade (8), two guide holes (9) have been seted up at the top of second sunshade (8), two embedding holes have been seted up at the top of the cabin body (1), the downthehole fixed mounting of embedding has second pipe (10), second pipe (10) weld with first pipe (7) mutually, the first hole has been seted up on the bottom inner wall of fuel tank (3), the second hole has been seted up at the top of the cabin body (1), the downthehole slidable mounting of first hole and second has same riser (11), the top of riser (11) welds with the bottom of slurcam (5), the front side of riser (11) articulates the one end of two down tubes (15), the other end of down tube (15) articulates on corresponding slide (14), all weld on the output shaft of push rod motor (4) and riser (11) has a plurality of swash plates (12).
2. The aircraft simulation cabin for fire drill according to claim 1, characterized in that two vertical plates are welded to the bottom of the cabin (1), and universal wheels are mounted on the bottoms of the vertical plates in a rolling manner.
3. The aircraft simulation cabin for fire drill according to claim 1, characterized in that the inner walls of the cabin (1) are respectively provided with an air inlet and an air outlet.
4. An aircraft simulation cabin for fire drilling according to claim 1, characterized in that said second shutter (8) covers the insertion hole.
5. The aircraft simulation cabin for fire drill according to claim 1, characterized in that the front side of the cabin body (1) is hinged with a cabin door, and a handle is fixedly installed on the front side of the cabin door.
6. The aircraft simulation cabin for fire drilling according to claim 1, characterized in that a filling hole is opened on one side of the inner wall of the fuel tank (3), and a plug board is clamped in the filling hole.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921108720.4U CN210428900U (en) | 2019-07-15 | 2019-07-15 | Airplane simulation cabin for fire drill |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921108720.4U CN210428900U (en) | 2019-07-15 | 2019-07-15 | Airplane simulation cabin for fire drill |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN210428900U true CN210428900U (en) | 2020-04-28 |
Family
ID=70380931
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201921108720.4U Expired - Fee Related CN210428900U (en) | 2019-07-15 | 2019-07-15 | Airplane simulation cabin for fire drill |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN210428900U (en) |
-
2019
- 2019-07-15 CN CN201921108720.4U patent/CN210428900U/en not_active Expired - Fee Related
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20200428 Termination date: 20210715 |