CN201633918U - Passenger-cargo mixed airplane passenger cabin - Google Patents
Passenger-cargo mixed airplane passenger cabin Download PDFInfo
- Publication number
- CN201633918U CN201633918U CN2010200005159U CN201020000515U CN201633918U CN 201633918 U CN201633918 U CN 201633918U CN 2010200005159 U CN2010200005159 U CN 2010200005159U CN 201020000515 U CN201020000515 U CN 201020000515U CN 201633918 U CN201633918 U CN 201633918U
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- CN
- China
- Prior art keywords
- passenger
- cabin
- cargo
- dividing plate
- passenger cabin
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
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Abstract
The utility model provides a passenger-cargo mixed airplane passenger cabin. The passenger cabin is internally provided with two dismountable clapboards, wherein one clapboard is near to a cabin door, the other clapboard is separated from the cabin door, the two clapboards divide the airplane passenger cabin into a passenger cabin segment and a cargo cabin segment, and division frames at the upper parts of the clapboards are provided with arresting nets. A small door is arranged at the clapboard which is near to the side of the cabin door to be taken as a passageway between the passenger cabin and the cargo cabin, and an air vent is arranged at the right lower part of the clapboard which is far away from the side of the cabin door. By adding the movable clapboards and the arresting nets in the passenger cabin, and arranging apparatuses such as a ventilating device, an illumination device and the like in the cargo cabin segment, the passenger cabin can disassemble the clapboards and the arresting nets when needing to increase the passenger carrying capacity or being used for the other purposes, thereby achieving the aim of transforming the passenger-cargo mixed passenger cabin into a standard passenger cabin.
Description
One, technical field
A kind of aircraft passenger compartment is especially for passenger-cargo aircraft passenger compartment that loads in mixture.
Two, background technology
The main cabin of passenger-cargo mixed packing machine requires passenger area and cargo area closed quarantine measures to be arranged to prevent the injury of goods to the passenger.At present, external similar aircraft generally adopts the form that increases fixing main frame between passenger area and the cargo area, and bulkhead is non-dismountable, so the main cabin can only be used for passenger-cargo a kind of purposes that loads in mixture.
Three, summary of the invention
Can only be used for passenger-cargo deficiency that loads in mixture a kind of purposes at the main cabin, of the present utility modelly provide a kind of and can increase passenger-cargo use alerting ability that loads in mixture the main cabin, make that passenger-cargo main cabin that loads in mixture can be to the main cabin of common passenger traffic main cabin conversion.
The technical scheme that the utility model is taked is: be provided with two detouchable dividing plates in the main cabin, wherein one near hatch door, another piece dividing plate is away from hatch door, and two dividing plates are divided into passenger cabin section and cargo compartment section to aircraft passenger compartment, on the bulkhead of the top of dividing plate arresting net is installed.
Be provided with the passage of wicket near hatch door side dividing plate, be provided with vent window away from position, hatch door side dividing plate bottom right as aircraft passenger compartment and cargo hold.
The detouchable dividing plate adopts honeycomb sandwich panel, and every is connected with screw with the fuselage frame by connecting flange, and aluminum alloy clamping plate are respectively installed in both sides during the butt joint of left and right sides dividing plate, and the dividing plate between the clamping plate is worn the screw place and got through the hole and adopt the screw connection.
In the cargo compartment section layout is simple and easy, establish simultaneously, and with passenger cabin section in establish reasonable link, vent window is set makes main cabin, cargo hold can realize conventional the ventilation, the needs that throw light on of the passenger after the newly-increased lighting installation of cargo hold can satisfy the cargo hold handling goods simultaneously and convert the main cabin to.
By increase mobilizable dividing plate and arresting net in the main cabin, and in cargo compartment section is provided with, establish, ventilate, facility such as illumination, can when customer requirement increases carrying or be used for other purposes, remove dividing plate and arresting net, realize passenger-cargo purpose that the main cabin converts standard passenger traffic main cabin to that loads in mixture.
Four, description of drawings
Fig. 1 arranges scheme drawing for passenger-cargo main cabin that loads in mixture, wherein, and 1: passenger cabin section, 2: dual seat, 3: the individual seat, 4: cabin door, 5: cargo door, 6: main cabin airstair hitch point, 7: dividing plate, 8: arresting net, 9: cargo compartment section, 10: wicket, 11: cargo hold airstair hitch point;
The contrary course view structure scheme drawing of Fig. 2 dividing plate, wherein, 21: right side partition, 22: left side dividing plate, 10: wicket, 23: connect flange, 24: clamping plate.
The specific embodiment
For better explanation the present invention, provide a kind of passenger-cargo aircraft passenger compartment that loads in mixture one better embodiment of the present invention below.
See also Fig. 1, it is the structural representation of a kind of passenger-cargo aircraft passenger compartment better embodiment that loads in mixture of the present invention.
Determine the position of dividing plate 7 according to the size of main cabin and cargo hold, establish at dividing plate 7 places and be divided into passenger cabin section 1, cargo compartment section 9 main cabin.Install earlier along left side, course dividing plate 22, left side dividing plate 22 is connected flange 23 be connected with screw with the plate nut of airframe structure frame setting; Install again along course right side partition 21, the connection flange 23 of right side partition 21 is connected with screw with the plate nut of airframe structure frame setting; Joint connecting cleat 24 in the middle of left side dividing plate 22 right side partition 21 is screwed at last.Install respectively in main cabin and the cargo hold and establish, arrange dual seat 2 in the main cabin, the individual seat 3, cabin door 4, and main cabin airstair hitch point 6 is arranged cargo door 5, cargo hold airstair hitch point 11 in cargo hold.
Utilize design-calculated joint arrangement arresting net 8 on the airframe structure frame in cargo compartment section 9, prevent the passenger in the goods injury main cabin in the cargo hold.
The position, bottom right of right side partition 21 is provided with vent window, makes main cabin, cargo hold can realize conventional the ventilation.
Detouchable dividing plate 7 adopts honeycomb sandwich panel to reduce parts, about dividing plate 7 is divided into two, every is connected with screw with the fuselage frame by connecting flange 23, aluminum alloy clamping plate were respectively installed in both sides when left and right sides dividing plate docked, dividing plate between the clamping plate is worn the screw place and is got through the connection of hole employing screw, wicket 10 is set on left side dividing plate 22, is used for the passage from the main cabin to the cargo hold.
By increase mobilizable dividing plate 7 and arresting net 8 in the main cabin, and facilities such as ventilation, illumination are set in cargo compartment section 9, can when customer requirement increases carrying or be used for other purposes, remove dividing plate 7 and arresting net 8, realize passenger-cargo purpose that the main cabin converts standard passenger traffic main cabin to that loads in mixture.
Claims (3)
1. passenger-cargo aircraft passenger compartment that loads in mixture comprises passenger cabin, hatch door, it is characterized in that: be provided with two detouchable dividing plates in the main cabin, wherein one near hatch door, another piece dividing plate is away from hatch door, and two dividing plates are divided into passenger cabin section and cargo compartment section to aircraft passenger compartment, are provided with barrier on dividing plate top.
2. aircraft passenger compartment according to claim 1 is characterized in that: be provided with wicket near hatch door side dividing plate.
3. aircraft passenger compartment according to claim 1 is characterized in that: be provided with vent window away from position, hatch door side dividing plate bottom right.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2010200005159U CN201633918U (en) | 2010-01-07 | 2010-01-07 | Passenger-cargo mixed airplane passenger cabin |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2010200005159U CN201633918U (en) | 2010-01-07 | 2010-01-07 | Passenger-cargo mixed airplane passenger cabin |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN201633918U true CN201633918U (en) | 2010-11-17 |
Family
ID=43078402
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2010200005159U Expired - Fee Related CN201633918U (en) | 2010-01-07 | 2010-01-07 | Passenger-cargo mixed airplane passenger cabin |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN201633918U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102381489A (en) * | 2011-06-02 | 2012-03-21 | 北京航空航天大学 | Fuselage afterbody with large opening at tail part and hatchdoor |
-
2010
- 2010-01-07 CN CN2010200005159U patent/CN201633918U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102381489A (en) * | 2011-06-02 | 2012-03-21 | 北京航空航天大学 | Fuselage afterbody with large opening at tail part and hatchdoor |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20101117 Termination date: 20150107 |
|
| EXPY | Termination of patent right or utility model |