CN106184764A - Commercial aircraft main cabin luggage carrier extended tip - Google Patents
Commercial aircraft main cabin luggage carrier extended tip Download PDFInfo
- Publication number
- CN106184764A CN106184764A CN201610705898.1A CN201610705898A CN106184764A CN 106184764 A CN106184764 A CN 106184764A CN 201610705898 A CN201610705898 A CN 201610705898A CN 106184764 A CN106184764 A CN 106184764A
- Authority
- CN
- China
- Prior art keywords
- luggage carrier
- main cabin
- rear board
- panel
- commercial aircraft
- 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.)
- Pending
Links
- 210000003141 lower extremity Anatomy 0.000 claims abstract description 4
- 229910000831 Steel Inorganic materials 0.000 claims description 31
- 239000010959 steel Substances 0.000 claims description 31
- 229910000838 Al alloy Inorganic materials 0.000 claims description 6
- 239000000956 alloy Substances 0.000 claims description 6
- 230000003014 reinforcing effect Effects 0.000 claims description 4
- 239000000463 material Substances 0.000 claims description 3
- 230000001413 cellular effect Effects 0.000 claims description 2
- 230000002787 reinforcement Effects 0.000 claims description 2
- 238000005034 decoration Methods 0.000 abstract description 4
- 230000002265 prevention Effects 0.000 description 4
- 238000005516 engineering process Methods 0.000 description 2
- 239000007787 solid Substances 0.000 description 2
- 229920000742 Cotton Polymers 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 239000011521 glass Substances 0.000 description 1
- 239000003292 glue Substances 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 238000007789 sealing Methods 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D11/00—Passenger or crew accommodation; Flight-deck installations not otherwise provided for
- B64D11/003—Stowage devices for passengers' personal luggage
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Laminated Bodies (AREA)
Abstract
A kind of commercial aircraft main cabin luggage carrier extended tip, including: by two front panels being parallel to each other and rear board, it is bonded and fixed to upper end and the box body structure of front opening that the inner panel of front panel and the bottom panel of rear board lower end and the circular arc that is bonded and fixed to front panel and rear board rear end is constituted；Described rear board is stairstepping, and it is fitted with luggage carrier front end face, described bottom panel and luggage carrier lower limb flush.Position after utilizing this commercial aircraft main cabin luggage carrier extended tip to remove locker in main cabin is blocked, and on the premise of meeting safety and airworthiness, plays good decoration function, and can save the expense newly purchasing luggage carrier of costliness.Owing in main cabin, other region is blocked by luggage carrier and sidewall paneling, install in luggage carrier front end so designed that little box body structure can facilitate, and form big main cabin free space.
Description
Technical field
The present invention relates to a kind of commercial aircraft main cabin luggage carrier extended tip.
Background technology
In aircraft passenger compartment retrofit process, after there is main cabin left front locker dismounting, the ceiling that aircraft was blocked originally
And the situation that the parts such as the interior of aircraft structure/glass cotton between sidewall paneling are exposed.
Summary of the invention
The present invention is in order to overcome the deficiency of above technology, it is provided that on the premise of one meets security row and airworthiness, rises
To good decoration function, the commercial aircraft main cabin luggage carrier extended tip of low cost.
The present invention overcomes its technical problem be the technical scheme is that
A kind of commercial aircraft main cabin luggage carrier extended tip, including: by two front panels being parallel to each other and rear board, glue
Connect and be fixed on front panel and the bottom panel of rear board lower end and be bonded and fixed to the circular arc of front panel and rear board rear end
The upper end of inner panel composition and the box body structure of front opening；Described rear board is stairstepping, and it pastes with luggage carrier front end face
Close, described bottom panel and luggage carrier lower limb flush.
In order to reduce weight, meeting fire prevention needs, above-mentioned front panel, rear board, bottom panel and inner panel use boat
Empty honeycomb board is made.
In order to improve intensity, in also including that horizontally disposed and two ends are connected with front panel and rear board medial surface respectively
Portion's support.
In order to improve intensity, front panel is fixed with angle steel IV with the seam crossing of inner panel, and front panel connects with bottom panel
The seam crossing being fixed with angle steel III, rear board and inner panel at seam is fixed with the seam crossing of angle steel II, rear board and bottom panel
It is fixed with angle steel I.
In order to improve intensity, the middle part of rear board medial surface is vertically fixed reinforcing plate.
In order to improve sealing, the lateral surface of above-mentioned bottom panel is provided with rubber and obturages I, and the upper surface of front panel is provided with
Rubber obturages II, and the upper surface of inner panel is provided with rubber and obturages III.
Above-mentioned internal stent is by horizontally disposed flat board and the riser of both sides before and after being the most vertically fixed on flat board lower end
Constitute U-shaped structure.
In order to reduce weight, meeting fire prevention needs, above-mentioned angle steel I, angle steel II, angle steel III and angle steel IV use aluminium alloy
Material is made.
In order to reduce weight, meeting fire prevention needs, above-mentioned reinforcement version uses aluminum alloy materials to make.
The invention has the beneficial effects as follows: utilize this commercial aircraft main cabin luggage carrier extended tip to locker in main cabin
Position after dismounting is blocked, and on the premise of meeting safety and airworthiness, plays good decoration function, and can save high
The expensive expense newly purchasing luggage carrier.Owing in main cabin, other region is blocked by luggage carrier and sidewall paneling, so designed that little
Box body structure can facilitate to be installed in luggage carrier front end, and forms big main cabin free space.
Accompanying drawing explanation
Fig. 1 is the perspective view I of the present invention；
Fig. 2 is the perspective view II of the present invention；
In figure, 1. front panel 2. rear board 3. bottom panel 4. inner panel 5. internal stent 51. flat board 52. riser 6.
Angle steel I 7. angle steel II 8. reinforcing plate 9. angle steel III 10. angle steel IV 11. rubber I 12. rubber of obturaging are obturaged II 13. rubber
Obturage III.
Detailed description of the invention
Below in conjunction with the accompanying drawings 1, the present invention will be further described for accompanying drawing 2.
A kind of commercial aircraft main cabin luggage carrier extended tip, including: by two front panels being parallel to each other 1 and below
Plate 2, it is bonded and fixed to front panel 1 and the bottom panel 3 of rear board 2 lower end and is bonded and fixed to front panel 1 and rear board 2 rear end
Circular arc inner panel 4 constitute upper end and the box body structure of front opening；Rear board 2 is stairstepping, itself and luggage carrier
Front end face is fitted, bottom panel 3 and luggage carrier lower limb flush.Utilize this commercial aircraft main cabin luggage carrier extended tip pair
Position after locker is removed in main cabin is blocked, and on the premise of meeting safety and airworthiness, plays good decoration and makees
With, and the expense newly purchasing luggage carrier of costliness can be saved.Owing in main cabin, other region is blocked by luggage carrier and sidewall paneling, because of
This is designed to little box body structure and can facilitate in the installation of luggage carrier front end, and forms big main cabin free space.
Front panel 1 is fixed with angle steel IV 10 with the seam crossing of inner panel 4, and front panel 1 is solid with the seam crossing of bottom panel 3
Surely angle steel III 9, rear board 2 is had to be fixed with angle steel II 7, rear board 2 and the seam of bottom panel 3 with the seam crossing of inner panel 4
Place is fixed with angle steel I 6.Angle steel IV 10 improves the bonding strength of front panel 1 and inner panel 4, before angle steel III 9 improves
Bonding strength between panel 1 and bottom panel 3, angle steel I 6 improves the bonding strength between rear board 2 and bottom panel 3, angle steel
II 7 improve the bonding strength between rear board 2 and inner panel 4.The middle part of rear board 2 medial surface is vertically fixed
Reinforcing plate 8, strengthens version 8 and improves the longitudinal strength of rear board 2, prevent its stress deformation.
Further, the lateral surface of bottom panel 3 is provided with rubber and obturages I 11, and the upper surface of front panel 1 is provided with rubber
Obturaging II 12, the upper surface of inner panel 4 is provided with rubber and obturages III 13.Rubber obturages I 11, rubber is obturaged II 12 and
Rubber is obturaged III 13 seams that can make this commercial aircraft main cabin luggage carrier extended tip and aircraft passenger compartment wallboard matching part
Realize at gap being in close contact.
The internal stent that horizontally disposed and two ends are connected respectively can also be included with front panel 1 and rear board 2 medial surface
5, front panel 1 and rear board 2 are connected by internal stent 5, can improve this commercial aircraft main cabin luggage carrier extended tip
Bonding strength, improves the reliability used.Further, internal stent 5 is the most solid by horizontally disposed flat board 51 and difference
Before and after flat board 51 lower end, the riser 52 of both sides constitutes U-shaped structure, and internal stent 5 rigidity of U-shaped structure is high, further
Improve bulk strength.
Further, front panel 1, rear board 2, bottom panel 3 and inner panel 4 use air cellular sheet material to make.Angle
Steel I 6, angle steel II 7, angle steel III 9 and angle steel IV 10 use aluminum alloy materials to make.Strengthen version 8 and use aluminum alloy materials
Make.It uses intensity and the fire prevention etc. of material require outer and possess lightweight feature in meeting main cabin.
Claims (9)
1. a commercial aircraft main cabin luggage carrier extended tip, it is characterised in that including: by two be parallel to each other before
Plate (1) and rear board (2), it is bonded and fixed to the bottom panel (3) of front panel (1) and rear board (2) lower end and is bonded and fixed to
Upper end that the inner panel (4) of the circular arc of front panel (1) and rear board (2) rear end is constituted and the box body structure of front opening；
Described rear board (2) is stairstepping, and it is fitted with luggage carrier front end face, described bottom panel (3) and luggage carrier lower limb flush.
Commercial aircraft main cabin the most according to claim 1 luggage carrier extended tip, it is characterised in that: described front panel
(1), rear board (2), bottom panel (3) and inner panel (4) use air cellular sheet material to make.
Commercial aircraft main cabin the most according to claim 1 luggage carrier extended tip, it is characterised in that: also include level
That arrange and that two ends are connected with front panel (1) and rear board (2) medial surface respectively internal stent (5).
Commercial aircraft main cabin the most according to claim 1 luggage carrier extended tip, it is characterised in that: front panel (1)
Being fixed with angle steel IV (10) with the seam crossing of inner panel (4), front panel (1) is fixed with angle steel with the seam crossing of bottom panel (3)
III (9), rear board (2) is fixed with angle steel II (7) with the seam crossing of inner panel (4), and rear board (2) connects with bottom panel (3)
Angle steel I (6) it is fixed with at seam.
Commercial aircraft main cabin the most according to claim 1 luggage carrier extended tip, it is characterised in that: rear board (2)
The middle part of medial surface is vertically fixed reinforcing plate (8).
Commercial aircraft main cabin the most as claimed in any of claims 1 to 5 luggage carrier extended tip, its feature exists
: the lateral surface of described bottom panel (3) being provided with rubber and obturages I (11), the upper surface of front panel (1) is provided with rubber and obturages II
(12), the upper surface of inner panel (4) is provided with rubber and obturages III (13).
Commercial aircraft main cabin the most according to claim 3 luggage carrier extended tip, it is characterised in that: described inside is propped up
Frame (5) by horizontally disposed flat board (51) and before and after being the most vertically fixed on flat board (51) lower end the riser (52) of both sides constitute
U-shaped structure.
Commercial aircraft main cabin the most according to claim 4 luggage carrier extended tip, it is characterised in that: described angle steel I
(6), angle steel II (7), angle steel III (9) and angle steel IV (10) use aluminum alloy materials to make.
Commercial aircraft main cabin the most according to claim 5 luggage carrier extended tip, it is characterised in that: described reinforcement version
(8) aluminum alloy materials is used to make.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610705898.1A CN106184764A (en) | 2016-08-23 | 2016-08-23 | Commercial aircraft main cabin luggage carrier extended tip |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610705898.1A CN106184764A (en) | 2016-08-23 | 2016-08-23 | Commercial aircraft main cabin luggage carrier extended tip |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106184764A true CN106184764A (en) | 2016-12-07 |
Family
ID=57524940
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610705898.1A Pending CN106184764A (en) | 2016-08-23 | 2016-08-23 | Commercial aircraft main cabin luggage carrier extended tip |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106184764A (en) |
Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101687550A (en) * | 2007-06-29 | 2010-03-31 | 空中客车营运有限公司 | Pivoting equipment carrier in combination with a modified luggage rack |
| US20100206985A1 (en) * | 2007-06-29 | 2010-08-19 | Airbus Operations Gmbh | Modular hatrack for a passenger compartment of an aircraft |
| CN102361793A (en) * | 2009-03-24 | 2012-02-22 | 空中客车营运有限公司 | Integration of electrical supply functions into overhead storage bin |
| CN102947180A (en) * | 2010-04-20 | 2013-02-27 | Be知识产权公司 | Aircraft bin module with integrated air ducts and lighting |
| US20130200213A1 (en) * | 2010-07-09 | 2013-08-08 | Airbus Operations Gmbh | Interior component carrier system, aircraft interior component module and assembly method |
| CN205469838U (en) * | 2016-02-04 | 2016-08-17 | 中国商用飞机有限责任公司 | Luggage rack |
| CN205952322U (en) * | 2016-08-23 | 2017-02-15 | 山东太古飞机工程有限公司 | Civil aviation aircraft cabin luggage rack extends end |
-
2016
- 2016-08-23 CN CN201610705898.1A patent/CN106184764A/en active Pending
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101687550A (en) * | 2007-06-29 | 2010-03-31 | 空中客车营运有限公司 | Pivoting equipment carrier in combination with a modified luggage rack |
| US20100206985A1 (en) * | 2007-06-29 | 2010-08-19 | Airbus Operations Gmbh | Modular hatrack for a passenger compartment of an aircraft |
| CN102361793A (en) * | 2009-03-24 | 2012-02-22 | 空中客车营运有限公司 | Integration of electrical supply functions into overhead storage bin |
| CN102947180A (en) * | 2010-04-20 | 2013-02-27 | Be知识产权公司 | Aircraft bin module with integrated air ducts and lighting |
| US20130200213A1 (en) * | 2010-07-09 | 2013-08-08 | Airbus Operations Gmbh | Interior component carrier system, aircraft interior component module and assembly method |
| CN205469838U (en) * | 2016-02-04 | 2016-08-17 | 中国商用飞机有限责任公司 | Luggage rack |
| CN205952322U (en) * | 2016-08-23 | 2017-02-15 | 山东太古飞机工程有限公司 | Civil aviation aircraft cabin luggage rack extends end |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20161207 |
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| WD01 | Invention patent application deemed withdrawn after publication |