CN205952322U - Civil aviation aircraft cabin luggage rack extends end - Google Patents
Civil aviation aircraft cabin luggage rack extends end Download PDFInfo
- Publication number
- CN205952322U CN205952322U CN201620922076.4U CN201620922076U CN205952322U CN 205952322 U CN205952322 U CN 205952322U CN 201620922076 U CN201620922076 U CN 201620922076U CN 205952322 U CN205952322 U CN 205952322U
- Authority
- CN
- China
- Prior art keywords
- panel
- luggage carrier
- main cabin
- angle steel
- fixed
- 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
Links
Landscapes
- Body Structure For Vehicles (AREA)
- Laminated Bodies (AREA)
Abstract
The utility model provides a civil aviation aircraft cabin luggage rack extends end, includes: be fixed in upper end and the front end open -ended box body structure that the bottom surface board of front panel and rear panel lower extreme and inboard panel that the bonding is fixed in front panel and back rear end of the panel's arc constitute by two front panels that are parallel to each other and rear panel, bonding, the rear panel is the stairstepping, its and the preceding terminal surface laminating of the luggage rack, bottom surface board and luggage rack lower limb looks parallel and level. Position after utilizing this civil aviation aircraft cabin luggage rack extends end the locker being demolishd in to the main cabin shelters from, satisfy the prerequisite of security and airworthiness under, play good decoration effect to can save the dear expense of newly purchasing the luggage rack. Because other regions are sheltered from by the luggage rack and lateral wall board in the main cabin, consequently design into little box body structure and can conveniently install at luggage rack front end to form big main cabin available 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
The exposed situation of part such as interior of aircraft structure/mineral wool and sidewall paneling between.
Content of the invention
The present invention is in order to overcome the shortcomings of above technology, there is provided on the premise of one kind 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 employed technical scheme comprise that：
A kind of commercial aircraft main cabin luggage carrier extended tip, including：By two front panels being parallel to each other and below
Plate, it is bonded and fixed to the bottom panel of front panel and rear board lower end and is bonded and fixed to front panel and the circular arc of rear board rear end
Upper end and the box body structure of front opening that the inner panel of shape is constituted；Described rear board is stairstepping, and it is with luggage carrier front end
Face laminating, described bottom panel and luggage carrier lower limb flush.
In order to reduce weight, meet fire prevention needs, above-mentioned front panel, rear board, bottom panel and inner panel are using boat
Empty honeycomb board is made.
In order to improve intensity, also include in 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 is connect with bottom panel
It is fixed with angle steel III, rear board is fixed with angle steel II, the seam crossing of rear board and bottom panel with the seam crossing of inner panel at seam
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 that is vertically fixed on both sides before and after flat board lower end respectively
Constitute U-shaped structure.
In order to reduce weight, meet fire prevention needs, above-mentioned angle steel I, angle steel II, angle steel III and angle steel IV adopt aluminium alloy
Material is made.
In order to reduce weight, meet fire prevention needs, above-mentioned reinforcing plate is made using aluminum alloy materials.
The invention has the beneficial effects as follows：Using 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 security and airworthiness, plays good decoration function, and can save high
The expense of expensive new purchase luggage carrier.Because regions other in main cabin are 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.
Brief description
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. rubbers
Glue obturages III.
Specific embodiment
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 the bottom panel 3 of front panel 1 and 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 front opening box body structure；Rear board 2 is stairstepping, itself and luggage carrier
Front end face laminating, bottom panel 3 and luggage carrier lower limb flush.Using 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 security and airworthiness, plays good decoration and makees
With, and the expense of the new purchase luggage carrier of costliness can be saved.Because regions other in main cabin are blocked by luggage carrier and sidewall paneling, because
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 there is angle steel III 9, rear board 2 is fixed with angle steel II 7, the seam of rear board 2 and 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, reinforcing plate 8 improves the longitudinal strength of rear board 2, prevents 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
Obturage II 12, the upper surface of inner panel 4 is provided with rubber and obturages III 13.Rubber obturage I 11, rubber obturage 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 using.Further, internal stent 5 is vertically 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 are made using air cellular sheet material.Angle
Steel I 6, angle steel II 7, angle steel III 9 and angle steel IV 10 are made using aluminum alloy materials.Reinforcing plate 8 adopts aluminum alloy materials
Make.It meets and requires outer using the intensity of material and fire prevention etc. in main cabin and possess lightweight feature.
Claims (9)
1. a kind of commercial aircraft main cabin luggage carrier extended tip is it is characterised in that include：By two be parallel to each other before
Plate（1）And rear board（2）, be bonded and fixed to front panel（1）And rear board（2）The bottom panel of lower end（3）And be bonded and fixed to
Front panel（1）And rear board（2）The inner panel of the circular arc of rear end（4）The upper end constituting and the box body structure of front opening；
Described rear board（2）For stairstepping, it is fitted with luggage carrier front end face, described bottom panel（3）With luggage carrier lower limb flush.
2. commercial aircraft main cabin 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）Made using air cellular sheet material.
3. commercial aircraft main cabin according to claim 1 luggage carrier extended tip it is characterised in that：Also include level
Setting and two ends respectively with front panel（1）And rear board（2）The internal stent that medial surface is connected（5）.
4. commercial aircraft main cabin according to claim 1 luggage carrier extended tip it is characterised in that：Front panel（1）
With inner panel（4）Seam crossing be fixed with angle steel IV（10）, front panel（1）With bottom panel（3）Seam crossing be fixed with angle steel
Ⅲ（9）, rear board（2）With inner panel（4）Seam crossing be fixed with angle steel II（7）, rear board（2）With bottom panel（3）Connect
It is fixed with angle steel I at seam（6）.
5. commercial aircraft main cabin 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）.
6. commercial aircraft main cabin as claimed in any of claims 1 to 5 luggage carrier extended tip, its feature exists
In：Described bottom panel（3）Lateral surface be provided with rubber and obturage I（11）, front panel（1）Upper surface be provided with rubber and obturage II
（12）, inner panel（4）Upper surface be provided with rubber and obturage III（13）.
7. commercial aircraft main cabin 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 vertically it is fixed on flat board respectively（51）The riser of both sides before and after lower end（52）Constitute
U-shaped structure.
8. commercial aircraft main cabin 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）Made using aluminum alloy materials.
9. commercial aircraft main cabin according to claim 5 luggage carrier extended tip it is characterised in that：Described reinforcing plate
（8）Made using aluminum alloy materials.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620922076.4U CN205952322U (en) | 2016-08-23 | 2016-08-23 | Civil aviation aircraft cabin luggage rack extends end |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620922076.4U CN205952322U (en) | 2016-08-23 | 2016-08-23 | Civil aviation aircraft cabin luggage rack extends end |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205952322U true CN205952322U (en) | 2017-02-15 |
Family
ID=57976949
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620922076.4U Expired - Fee Related CN205952322U (en) | 2016-08-23 | 2016-08-23 | Civil aviation aircraft cabin luggage rack extends end |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205952322U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106184764A (en) * | 2016-08-23 | 2016-12-07 | 山东太古飞机工程有限公司 | Commercial aircraft main cabin luggage carrier extended tip |
-
2016
- 2016-08-23 CN CN201620922076.4U patent/CN205952322U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106184764A (en) * | 2016-08-23 | 2016-12-07 | 山东太古飞机工程有限公司 | Commercial aircraft main cabin luggage carrier extended tip |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN208715308U (en) | Truck cargo car body and transport van | |
| CN106184402B (en) | Vehicle body rear part structure | |
| US8672268B2 (en) | Oblique panel at the rear of a central box of an aircraft fuselage | |
| CN206202436U (en) | The mounting structure of decorative panel, vehicle body and vehicle after gusset | |
| CN205952322U (en) | Civil aviation aircraft cabin luggage rack extends end | |
| CN103802848B (en) | The hood structure of bullet train headstock and installation method | |
| CN209739175U (en) | automobile rear wheel cover reinforcing structure | |
| CN106184764A (en) | Commercial aircraft main cabin luggage carrier extended tip | |
| CN207241591U (en) | A kind of bus luggage frame assembly structure | |
| CN201400179Y (en) | Top plate mounting structure of passenger compartments of high-speed sleeper | |
| CN205202861U (en) | A baffle assembly for separating passenger cabin and goods cabin | |
| CN102729907A (en) | Whole luggage rack for passenger car | |
| CN201484513U (en) | Back door structure of van-type semi-trailer | |
| CN210793180U (en) | Novel lightweight air duct | |
| CN210822234U (en) | Rail vehicle and cab thereof | |
| CN2302228Y (en) | Aircraft transportation container | |
| CN107415836A (en) | A kind of bus luggage frame assembly structure | |
| CN206914205U (en) | A kind of inflammable solid transport van | |
| CN207916531U (en) | A kind of bus with front-mounted engine spare tyre hatch door connecting assembly | |
| CN106515547B (en) | A kind of seafood vehicle | |
| CN206278257U (en) | A kind of helicopter floor level structure | |
| CN206703640U (en) | New-energy automobile compartment composite board and new new-energy automobile compartment | |
| CN106627799B (en) | Carrying luggage cabin type full-bearing freight car body | |
| CN205632692U (en) | Detachable packing box of new energy automobile | |
| CN205165320U (en) | Nonmetal side support piece and fume chamber thereof |
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: 20170215 Termination date: 20200823 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |