CN102991682A - Cabin using multimedia display porthole and airplane - Google Patents
Cabin using multimedia display porthole and airplane Download PDFInfo
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- CN102991682A CN102991682A CN2012104878995A CN201210487899A CN102991682A CN 102991682 A CN102991682 A CN 102991682A CN 2012104878995 A CN2012104878995 A CN 2012104878995A CN 201210487899 A CN201210487899 A CN 201210487899A CN 102991682 A CN102991682 A CN 102991682A
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Abstract
The invention belongs to the design technology of the airplane cabin and relates to a cabin using a multimedia display porthole and an airplane. The cabin using the multimedia display porthole adopts an integrally-sealed structure; a multimedia display screen is arranged in a position of a cabin inner wall porthole on the side of a passenger seat and communicated with a panoramic camera, and the panoramic camera is arranged on an external part of an airplane body; the multimedia display screen communicated with the panoramic camera on the external part of the airplane body is arranged at the top of the cabin; and the multimedia display screen can reflect the external environment situation of the airplane in real time and play the selected content under the control of the crew members according the need. In the airplane with the cabin, the airplane body structure design is simplified, the airplane weight is reduced, the airplane structure strength is enhanced, the potential safety hazard is reduced and the structure reliability of the airplane is enhanced; and moreover, through the coordination with the reasonable arrangement of the multimedia and the lighting, the travel comfort of the passengers can be effectively improved.
Description
Technical field
The invention belongs to the aircraft cabin designing technique, relate to a kind of cabin and aircraft that adopts the multimedia display porthole.
Background technology
The existence of aircraft porthole mainly is the comfort that satisfies the passenger, avoids the passenger to occur constraining in enclosure space and frightened sensation.As on Boeing 787 Dreamliners, the porthole size has enlarged 70% than service aircraft, and is high 47 centimetres, wide 28 centimetres.No matter where be sitting in aircraft, the passenger can both appreciate the view on the ground line, and this makes passenger's flight experience more excellent.Air Passenger has proposed transparent skylight and man-machine interaction concept on the concept aircraft of estimating the year two thousand fifty place in operation, improve the comfort of route.
Porthole can be described as unremarkable parts aboard, if but arrange improperly, can have a strong impact on flight safety.On the one hand, aircraft is when high-altitude flight, for guaranteeing unit and passenger's eupnea; be supercharging in the cabin, porthole is oversize, and the pressure that side of a ship window edge bears is just larger; that causes that air leaks in the cabin may be just larger, so the porthole size should be controlled in the rational scope.On the other hand, porthole is oversize, just means that also the opening on fuselage is larger, can affect the structural strength of aircraft, causes the situation of aircraft accident to occur because the porthole place goes wrong more.In addition, also the weakened noise abatement of fuselage integral body of the structure and material at porthole place has increased noise in the cabin.
Larger porthole means the larger difficulty in the engineering design.Because if the hatch door that cuts on the fuselage and porthole are less and less, the load that aircaft configuration bears just is easier to solve.Therefore, on some special aircrafts and military aircraft, fuselage does not have porthole.As be under the jurisdiction of " the doomsday aircraft " of United States Air Force, designed the protecting crust that fits together perfectly for anti-nuclear radiation, to guarantee that personnel in the cabin can not be subject to nuclear bomb and impact.But, concerning groups of people, the characteristics of " doomsday aircraft " also are its " shortcomings ", U.S. minister of defense Gates just complains the reporter, window of his freight space does not all have, seal everywhere, allowing him feel oneself is a warrier of Sparta in the experience tribulation, and not too similarly is the minister who takes senior aircraft.
Summary of the invention
The objective of the invention is: propose a kind of cabin of adopting this multimedia display porthole.
Provide a kind of cabin to adopt the aircraft of multimedia display porthole.
Technical scheme of the present invention is: a kind of cabin of adopting the multimedia display porthole, and wherein, the inwall porthole position, cabin of passenger-seat side is provided with multimedia display screen, and this multimedia display screen is communicated with the camera that is arranged on the fuselage outside.
Nacelle top is provided with the multimedia display screen that is connected with the outside camera of fuselage.
The one enclosed construction is adopted in described cabin.
Described multimedia display screen is camber display screen.
Described multimedia display screen is the flexible read-out of OLED.
Described head and tail and wing have at least a place to be provided with camera.
The cabin outer wall that the multimedia display screen place is set is provided with camera.
Described multimedia display screen links to each other with multimedia player.
Sidewall and/or top are provided with the LED lamp.
A kind of aircraft, it adopts above-mentioned cabin with multimedia porthole.
Advantage of the present invention is: the present invention is in the cabin of sealing without porthole, utilize the flexible read-out of organic thin film electroluminescent device (OLED), in conjunction with airborne visible image capturing device and multimedia image, can overcome in enclosure space, cut off the negative influence that the inside and outside visual connection in cabin causes passenger's visual information deficiency to bring owing to windowless.And utilize the LED lamp, and build the illumination near natural daylight, satisfy colour temperature and the colour rendering index of vision requirement, to satisfy healthy requirement.Its concrete advantage is as follows:
1) simplifies the civil aircraft structures design, reduce potential safety hazard, improve the reliability of aircaft configuration;
2) owing to reduced reinforced bulkhead and the number of rivets of airframe structure, can alleviate aircraft weight,
Energy savings reduces carbon emission;
3) improve noise abatement in the cabin, make in the cabin quieter;
4) cooperate multimedia and lamplit reasonable arrangement, improve the comfort level of passenger's travelling.
Description of drawings
Fig. 1 is the cabin schematic cross-section that the passenger plane of multimedia panorama numeral porthole is adopted in cabin of the present invention;
Fig. 2 is cabin sidewall scheme drawing;
Fig. 3 is camera setting position scheme drawing,
Wherein, the flexible read-out of 1-cabin sidewall OLED, the flexible read-out of 2-nacelle top OLED, 3-head full-view camera, 4-wing full-view camera, 5-tail full-view camera.
The specific embodiment
The present invention is further detailed explanation below in conjunction with drawings and Examples, but not as the foundation of the present invention being done any restriction.
See also Fig. 1, it is the cabin schematic cross-section that the passenger plane of multimedia panorama numeral porthole is adopted in cabin of the present invention.Aircraft of the present invention adopts without the porthole design, and namely the one enclosed construction is adopted in the cabin taken of passenger, and the bulkhead at passenger seat is not offered porthole.Wherein, the former porthole of cabin inwall position (window seat side) and nacelle top are provided with multimedia display screen.
Described multimedia display screen adopts OLED(organic thin film electroluminescent device) flexible read-out or other can be used for the screen of multimedia display, link to each other with passenger plane inner multimedia player, for the play multimedia video.In addition, each multimedia display screen is connected each full-view camera that is arranged on engine body exterior, can play in real time the outer full-view image of passenger plane, and the passenger as required, can switch the captured scene of diverse location camera, therefore the passenger who is sitting in the sealing cabin can enjoy the outer scenery of aircraft in real time, thus Effective Raise passenger's travelling traveling comfort.In addition, according to actual needs, the multimedia display screen at place, different seat can have the passenger to select, and extremely plays the multimedia image of being controlled by multimedia processor by real time panoramic image switching, such as film, TV etc.Simultaneously, cabin inwall (such as sidewall or top, by the multimedia display screen) also is provided with for the illumination of construction near natural daylight, satisfies the LED lamp of colour temperature and the colour rendering index of vision requirement, to satisfy the travelling health requirements.
Among the embodiment, the area of the flexible read-out of OLED is at 30 cun, be arranged on the position between the engine room inside front and rear row seat, the visible image capturing head that is used for panning outside the cabin is arranged on the cabin outer wall of head, wing tip, tail and each multimedia display screen position.
Certainly, technical solution of the present invention is not limited to the technology contents that above-described embodiment discloses, multimedia display screen wherein is not limited to use flexible OLED, also can be panel display screen, such as liquid crystal display, or other camber display screens, size also is not limited to 30 cun, can be 20 cun, 40 cun, arrange needs according to engine room inside, can do corresponding adjustment.And the visible image capturing head that is used for pan-shot is not limited to be arranged on the positions such as head, wing tip, tail, can be arranged on the body diverse location according to actual needs, to better meet passenger demand, improves the flight comfort level.In addition, the multimedia display screen that the present invention can panorama shows is not limited to and is installed in the fully enclosed cabin, and according to passenger's needs, the cabin inwall that porthole is less also can be installed.
Claims (10)
1. a cabin of adopting the multimedia display porthole is characterized in that, the inwall porthole position, cabin of passenger-seat side is provided with multimedia display screen, and this multimedia display screen is communicated with the camera that is arranged on the fuselage outside.
2. the cabin of employing multimedia display porthole according to claim 1 is characterized in that, nacelle top is provided with the multimedia display screen that is connected with the outside camera of fuselage.
3. the cabin of employing multimedia display porthole according to claim 2 is characterized in that, the one enclosed construction is adopted in described cabin.
4. the cabin of employing multimedia display porthole according to claim 3 is characterized in that, described multimedia display screen is camber display screen.
5. the cabin of employing multimedia display porthole according to claim 4 is characterized in that, described multimedia display screen is the flexible read-out of OLED.
6. the cabin of employing multimedia display porthole according to claim 1 is characterized in that, described head and tail and wing have at least a place to be provided with camera.
7. the cabin of employing multimedia display porthole according to claim 1 is characterized in that, the cabin outer wall that the multimedia display screen place is set is provided with camera.
8. the cabin of employing multimedia display porthole according to claim 1 is characterized in that, described multimedia display screen links to each other with multimedia player.
9. the cabin of employing multimedia display porthole according to claim 1 is characterized in that, sidewall and/or top are provided with the LED lamp.
10. an aircraft is characterized in that, adopts such as each described cabin of claim 1 to 9.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2012104878995A CN102991682A (en) | 2012-11-26 | 2012-11-26 | Cabin using multimedia display porthole and airplane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2012104878995A CN102991682A (en) | 2012-11-26 | 2012-11-26 | Cabin using multimedia display porthole and airplane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN102991682A true CN102991682A (en) | 2013-03-27 |
Family
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2012104878995A Pending CN102991682A (en) | 2012-11-26 | 2012-11-26 | Cabin using multimedia display porthole and airplane |
Country Status (1)
| Country | Link |
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| CN (1) | CN102991682A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114228973A (en) * | 2021-12-31 | 2022-03-25 | 中国商用飞机有限责任公司 | Aircraft porthole system with transparent display, display method and medium thereof |
Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP0913325A1 (en) * | 1997-10-30 | 1999-05-06 | Ioannis Vassilios Constantopoulos | Passenger aircraft |
| JP2000350195A (en) * | 1999-06-04 | 2000-12-15 | Mitsubishi Heavy Ind Ltd | Virtual window forming system for aircraft |
| JP2002178997A (en) * | 2000-12-14 | 2002-06-26 | Mitsubishi Heavy Ind Ltd | Window monitor device for aircraft |
| US20120320508A1 (en) * | 2011-06-10 | 2012-12-20 | Airbus Operations Gmbh | Display apparatus for a passenger cabin of an aircraft or spacecraft |
| CN202642101U (en) * | 2012-04-19 | 2013-01-02 | 智比特信息技术（镇江）有限公司 | Window-free passenger plane |
| CN203078760U (en) * | 2012-11-26 | 2013-07-24 | 中国商用飞机有限责任公司 | Passenger compartment using multi-media panorama digital porthole and airplane |
| US20140092206A1 (en) * | 2011-04-01 | 2014-04-03 | Latecoere | Aircraft provided with a system for observing part of the aircraft's environment |
-
2012
- 2012-11-26 CN CN2012104878995A patent/CN102991682A/en active Pending
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP0913325A1 (en) * | 1997-10-30 | 1999-05-06 | Ioannis Vassilios Constantopoulos | Passenger aircraft |
| JP2000350195A (en) * | 1999-06-04 | 2000-12-15 | Mitsubishi Heavy Ind Ltd | Virtual window forming system for aircraft |
| JP2002178997A (en) * | 2000-12-14 | 2002-06-26 | Mitsubishi Heavy Ind Ltd | Window monitor device for aircraft |
| US20140092206A1 (en) * | 2011-04-01 | 2014-04-03 | Latecoere | Aircraft provided with a system for observing part of the aircraft's environment |
| US20120320508A1 (en) * | 2011-06-10 | 2012-12-20 | Airbus Operations Gmbh | Display apparatus for a passenger cabin of an aircraft or spacecraft |
| CN202642101U (en) * | 2012-04-19 | 2013-01-02 | 智比特信息技术（镇江）有限公司 | Window-free passenger plane |
| CN203078760U (en) * | 2012-11-26 | 2013-07-24 | 中国商用飞机有限责任公司 | Passenger compartment using multi-media panorama digital porthole and airplane |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114228973A (en) * | 2021-12-31 | 2022-03-25 | 中国商用飞机有限责任公司 | Aircraft porthole system with transparent display, display method and medium thereof |
| CN114228973B (en) * | 2021-12-31 | 2024-06-07 | 中国商用飞机有限责任公司 | Aircraft porthole system with transparent display and display method and medium thereof |
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| PB01 | Publication | ||
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| RJ01 | Rejection of invention patent application after publication | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20130327 |