CN204990832U - Take aircraft boilerplate of integrated form air conditioner - Google Patents
Take aircraft boilerplate of integrated form air conditioner Download PDFInfo
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- CN204990832U CN204990832U CN201520765866.1U CN201520765866U CN204990832U CN 204990832 U CN204990832 U CN 204990832U CN 201520765866 U CN201520765866 U CN 201520765866U CN 204990832 U CN204990832 U CN 204990832U
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- air
- boilerplate
- conditioning
- air conditioner
- simulation cabin
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Abstract
Take aircraft boilerplate of integrated form air conditioner, the below on aircraft boilerplate floor (1 -1) is provided with air conditioner switchboard (2), the bottom periphery of aircraft boilerplate (1) is provided with semi -ring shape intake stack (2 -1), air conditioner switchboard (2) is connected through the pipeline of taking a breath (2 -2) to intake stack (2 -1), aircraft boilerplate (1) inner wall is provided with a plurality of air -out windows (2 -3), air conditioner switchboard (2) is connected through air conditioner air duct (2 -4) to air -out window (2 -3). Air conditioning system is integrated totally in the intermediate layer of boilerplate floor for the overall structure in flight simulation cabin is compacter, and the sense of reality that the operator experienced in inside strengthens, and the intake stack on the boilerplate can make the powerful space to simulating under -deck portion of air conditioner take a breath and freeze.
Description
Technical field
The utility model relates to flight-simulation equipment field, is specifically the plane simulation cabin of band integrated form air-conditioning.
Background technology
Plane simulation cabin refers to a kind of simulated flight, and bring the equipment that user's Live Flying is experienced, it does not need superb piloting technique just can realize the experience of simulated flight.Huge help is not only played in flight simulation cabin in the training of technical flight person, and in civilian, amusement also more and more like by people.But because the space of inside, plane simulation cabin is less, need to place seat, display and some hardware, cause its inner space less, so the air-conditioning system in flight simulation cabin is all arranged on outside, connect flight simulation cabin by air-conditioning duct, such structure needs a large amount of air-conditioning ducts and link, because flight simulation cabin needs certain apron space, so the operate power of outdoor machine of air-conditioner needs larger power by contrast, cause wasting more electricity.
Summary of the invention
In order to solve the problem, the utility model provides the plane simulation cabin of band integrated form air-conditioning.
The plane simulation cabin of the utility model band integrated form air-conditioning is achieved through the following technical solutions:
With the plane simulation cabin of integrated form air-conditioning, comprise plane simulation cabin (1), floor, plane simulation cabin (1-1), air-conditioning exchange (2), intake stack (2-1), air refreshing tube (2-2), air outlet window (2-3), air conditioning ducts (2-4), it is characterized in that: the below on floor, plane simulation cabin (1-1) is provided with air-conditioning exchange (2), the bottom periphery in plane simulation cabin (1) is provided with semi-circular intake stack (2-1), intake stack (2-1) connects air-conditioning exchange (2) by air refreshing tube (2-2), plane simulation cabin (1) inwall is provided with some air outlet windows (2-3), air outlet window (2-3) connects air-conditioning exchange (2) by air-conditioning duct (2-4).
The beneficial effect that the utility model has: the air-conditioning system of this structure is completely integrated in boiler-plate interlayer, make the one-piece construction in flight simulation cabin compacter, the degree enhancing that operator experiences in inside, the air inlet that intake stack two ends are arranged ensure that air-conditioning exchange has enough air outputs when running, air outlet window on boiler-plate shell can make the powerful space to boiler-plate inside of air-conditioning take a breath and freeze, and economizes on resources.
Below in conjunction with the embodiment of accompanying drawing illustrated embodiment, foregoing of the present utility model is described in further detail again.
Accompanying drawing explanation
Fig. 1 is the utility model external structure schematic diagram;
Fig. 2 is the utility model inner structure schematic diagram;
Fig. 3 is that the utility model implements structural representation.
Mark in figure: plane simulation cabin (1), floor, plane simulation cabin (1-1), air-conditioning exchange (2), intake stack (2-1), air refreshing tube (2-2), air outlet window (2-3), air conditioning ducts (2-4).
Embodiment
With the plane simulation cabin of integrated form air-conditioning, comprise plane simulation cabin, floor, plane simulation cabin, air-conditioning exchange, intake stack, air refreshing tube, air outlet window, air conditioning ducts, the below on floor, plane simulation cabin is provided with air-conditioning exchange, the bottom periphery in plane simulation cabin is provided with semi-circular intake stack, intake stack connects air-conditioning exchange by air refreshing tube, plane simulation cabin inwall is provided with some air outlet windows, and air outlet window connects air-conditioning exchange by air-conditioning duct.
During use, open air-conditioning switch, the air inlet at intake stack two ends is started working, and the air of outside is sent to air-conditioning exchange by intake stack through air refreshing tube, and the air after process is sent to air outlet window by after air-treatment by air-conditioning duct by air-conditioning exchange; The air of boiler-plate inside is sent to air-conditioning exchange by air-conditioning duct by air outlet window, and air is sent out flight simulation cabin by air refreshing tube and intake stack by air-conditioning exchange again.
Claims (1)
1. be with the plane simulation cabin of integrated form air-conditioning, comprise plane simulation cabin (1), floor, plane simulation cabin (1-1), air-conditioning exchange (2), intake stack (2-1), air refreshing tube (2-2), air outlet window (2-3), air conditioning ducts (2-4), it is characterized in that: the below on floor, plane simulation cabin (1-1) is provided with air-conditioning exchange (2), the bottom periphery in plane simulation cabin (1) is provided with semi-circular intake stack (2-1), intake stack (2-1) connects air-conditioning exchange (2) by air refreshing tube (2-2), plane simulation cabin (1) inwall is provided with some air outlet windows (2-3), air outlet window (2-3) connects air-conditioning exchange (2) by air-conditioning duct (2-4).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520765866.1U CN204990832U (en) | 2015-09-30 | 2015-09-30 | Take aircraft boilerplate of integrated form air conditioner |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520765866.1U CN204990832U (en) | 2015-09-30 | 2015-09-30 | Take aircraft boilerplate of integrated form air conditioner |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204990832U true CN204990832U (en) | 2016-01-20 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520765866.1U Active CN204990832U (en) | 2015-09-30 | 2015-09-30 | Take aircraft boilerplate of integrated form air conditioner |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN204990832U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105938667A (en) * | 2016-06-01 | 2016-09-14 | 广东思泓国际贸易有限公司 | Simulation platform |
| CN112482484A (en) * | 2020-11-25 | 2021-03-12 | 贵州詹阳动力重工有限公司 | Remote control simulation cabin and remote control system for excavator |
-
2015
- 2015-09-30 CN CN201520765866.1U patent/CN204990832U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105938667A (en) * | 2016-06-01 | 2016-09-14 | 广东思泓国际贸易有限公司 | Simulation platform |
| CN112482484A (en) * | 2020-11-25 | 2021-03-12 | 贵州詹阳动力重工有限公司 | Remote control simulation cabin and remote control system for excavator |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant |