CN109592042A - A method of equipment is installed on aircraft trim panel - Google Patents
A method of equipment is installed on aircraft trim panel Download PDFInfo
- Publication number
- CN109592042A CN109592042A CN201811304749.XA CN201811304749A CN109592042A CN 109592042 A CN109592042 A CN 109592042A CN 201811304749 A CN201811304749 A CN 201811304749A CN 109592042 A CN109592042 A CN 109592042A
- Authority
- CN
- China
- Prior art keywords
- equipment
- slot
- trim panel
- cover board
- sagging
- 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
- 238000000034 method Methods 0.000 title claims abstract description 15
- 238000007665 sagging Methods 0.000 claims abstract description 23
- 230000005540 biological transmission Effects 0.000 claims description 5
- 239000004677 Nylon Substances 0.000 claims 1
- 229920001778 nylon Polymers 0.000 claims 1
- 230000000694 effects Effects 0.000 description 5
- 238000009434 installation Methods 0.000 description 3
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 2
- 238000005034 decoration Methods 0.000 description 2
- 229910052760 oxygen Inorganic materials 0.000 description 2
- 239000001301 oxygen Substances 0.000 description 2
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N Silicium dioxide Chemical compound O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000001427 coherent effect Effects 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 238000003032 molecular docking Methods 0.000 description 1
- 238000007493 shaping process Methods 0.000 description 1
- 239000000741 silica gel Substances 0.000 description 1
- 229910002027 silica gel Inorganic materials 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
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Fittings On The Vehicle Exterior For Carrying Loads, And Devices For Holding Or Mounting Articles (AREA)
Abstract
A method of equipment is installed on aircraft trim panel, the slot that sink is equipped on trim panel, is equipped with equipment through hole in the bottom for the slot that sink；It places a device in the equipment through hole of sagging trench bottom；Separately there is one to be covered on sagging notch with the matched cover board of sagging slot, matches the outer surface of cover board with the trim panel around sagging slot.
Description
Technical field
The application belongs to airplane design technical field, is further aircraft interior design, specifically a kind of in aircraft interior trim
The method of equipment is installed on plate.
Background technique
Equipped with many equipment, equipment and interior trims such as headlamp, ring control air outlet, oxygen mask, loudspeakers on aircraft interior trim
There are many types of attachment.Some equipment is connect by clamp button of the spring with interior trim, this type of attachment by equipment own wt about
Beam is larger；Some equipment be connected directly between on interior trim or be connected on aircaft configuration by screw but with the opening pair on interior trim
It connects, this type of attachment ailhead or seam (big, uneven) are directly exposed in cabin, influence interior trim overall effect.
There are also some equipment, such as oxygen mask, lifesaving axe box to be mounted on aircraft body structure on aircraft, but in needs
Via hole is opened on decorations keeps environment division exposed.Equipment is different from interior trim datum mark, and often seam is uneven at docking, this to avoid
It happens, can generally take some measures, it is a kind of that seam is expanded to and used silica gel strip caulking joint, there is unfavorable shadow to interior trim appearance
It rings, one is equipment to be directly installed on interior trim, influences the demolition and maintenance of interior trim.
Any surface finish is completely the important indicator of aircraft interior trim installation effect, and the equipment installation ailhead on interior trim how to be allowed to close
Reason is hidden, and guarantees mounting surface effect, is solved the problems, such as required for the interior design of domestic and international all aircrafts.
Summary of the invention
The application's is designed to provide a kind of method that equipment is installed on aircraft trim panel, at interior trim layering
Reason, efficiently solves the problems, such as the joint treatment of interior trim and equipment interconnection.
A method of equipment is installed on aircraft trim panel, which is characterized in that 1) it on trim panel is equipped with the slot that sink,
The bottom of sagging slot is equipped with equipment through hole；2) it places a device in the equipment through hole of sagging trench bottom；3) separately have one with
The matched cover board of slot that sink is covered on sagging notch, matches the outer surface of cover board with the trim panel around sagging slot.
Supporting block is equipped between the bottom and cover board of the sagging slot, the height of the supporting block is less than the depth for the slot that sink
Degree, cover board are connect with supporting block by velcro fastener, flush the height of cover board outer surface with the surface of trim panel.
Equipment for being mounted on trim panel is additionally provided with equipment mounting hole in the bottom for the slot that sink, equipment is mounted on
On the equipment mounting hole of the bottom of sagging slot.
It is the servicing property that passenger provides according to equipment, facilitates cover board transmission equipment information, the cover board can be one
Kind is equipped with the flase floor of one or more through-holes；The cover board can also be the plate or lighttight plate of a kind of energy light transmission
Material.
The beneficial effects of the present application are as follows: 1) by interior trim layered shaping, equipment is mounted in the sagging slot of trim panel,
Additionally by one have decoration and the cover board of covering effect by the sagging slot of trim panel and equipment mounting hole, nail and equipment with it is interior
Gap between plaque is covered, the effective solution joint treatment installation question of interior trim and equipment interconnection.2) decorative cover in
Plate and this figure of interior trim face are coherent, and the gap that can be blocked equipment ailhead and dock with interior trim guarantees decorative effect.
The application is described in further detail with reference to embodiments.
Detailed description of the invention
Fig. 1 is the method signal that equipment is installed on aircraft trim panel.
Fig. 2 is that have the grid-like cover board of multiple through-holes to illustrate.
Explanation: 1 trim panel, 2 cover boards, 3 sagging slots, 4 cushion blocks, 5 equipment through holes, 6 equipment, 7 connecting holes is numbered in figure.
Specific embodiment
Referring to attached drawing, the method that equipment is installed on aircraft trim panel of the application is equipped with the slot 3 that sink on trim panel 1,
Equipment through hole 5 is equipped in the bottom for the slot 3 that sink；Equipment 6 is placed in the equipment through hole 5 of sagging 3 bottom of slot fixed；Separately have
One is covered on the mouth of sagging slot 3 with the matched cover board 2 of sagging slot 3, make the outer surface of cover board 2 with it is interior around sagging slot 3
Plaque 1 matches.
Supporting block 4 is equipped between the bottom and cover board of the sagging slot 3, the height of the supporting block 4 is less than the slot 3 that sink
Depth, in implementation, supporting block 4 is equipped with velcro fastener, and cover board 2 is connect with supporting block 4 by velcro fastener, makes 2 appearance of cover board
The height in face is flushed with the surface of trim panel 1.
Equipment for being mounted on trim panel 1 is additionally provided with equipment mounting hole 7 in the bottom for the slot 3 that sink, equipment is installed
On the equipment mounting hole 7 of the bottom for the slot 3 that sink.
In addition, being the servicing property that passenger provides according to equipment, facilitate cover board transmission equipment information, the cover board 2 can
To be a kind of flase floor equipped with one or more through-holes, as shown in Fig. 2, cover board is a kind of flase floor；The cover board 2 may be used also
To be the plate or lighttight plate of a kind of energy light transmission.
Claims (6)
1. a kind of method for installing equipment on aircraft trim panel, which is characterized in that 1) slot that sink is equipped on trim panel, under
The bottom for falling into slot is equipped with equipment through hole；2) it places a device in the equipment through hole of sagging trench bottom；3) separately have one under
It falls into the matched cover board of slot to be covered on sagging notch, matches the outer surface of cover board with the trim panel around sagging slot.
2. the method for equipment is installed on aircraft trim panel as described in claim 1, which is characterized in that the sagging slot
Supporting block is equipped between bottom and cover board, the height of the supporting block is less than the depth for the slot that sink, and cover board and supporting block pass through nylon
Hasp connection, flushes the height of cover board outer surface with the surface of trim panel.
3. the method for equipment is installed on aircraft trim panel as claimed in claim 1 or 2, which is characterized in that in the slot that sink
Bottom is additionally provided with equipment mounting hole, and equipment is mounted on the equipment mounting hole of the bottom of sagging slot.
4. the method for equipment is installed on aircraft trim panel as claimed in claim 3, which is characterized in that the cover board is one
Kind is equipped with the flase floor of one or more through-holes.
5. the method for equipment is installed on aircraft trim panel as claimed in claim 3, which is characterized in that the cover board is one
The plate of kind energy light transmission.
6. the method for equipment is installed on aircraft trim panel as claimed in claim 3, which is characterized in that the cover board is one
The lighttight dalle of kind.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811304749.XA CN109592042A (en) | 2018-11-02 | 2018-11-02 | A method of equipment is installed on aircraft trim panel |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811304749.XA CN109592042A (en) | 2018-11-02 | 2018-11-02 | A method of equipment is installed on aircraft trim panel |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN109592042A true CN109592042A (en) | 2019-04-09 |
Family
ID=65958456
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201811304749.XA Pending CN109592042A (en) | 2018-11-02 | 2018-11-02 | A method of equipment is installed on aircraft trim panel |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN109592042A (en) |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20030082943A1 (en) * | 2001-10-31 | 2003-05-01 | Chen Kuo-Wen | Dustproof cover of connector slot |
| CN202186341U (en) * | 2011-07-13 | 2012-04-11 | 北汽福田汽车股份有限公司 | Plug, automobile interior trimming panel and automobile |
| CN206171469U (en) * | 2016-10-18 | 2017-05-17 | 苏州大成电子科技有限公司 | Carriage with light source interior trim part |
| CN106741832A (en) * | 2016-12-15 | 2017-05-31 | 中国航空工业集团公司西安飞机设计研究所 | A kind of adjustable interior trim lid of dock |
-
2018
- 2018-11-02 CN CN201811304749.XA patent/CN109592042A/en active Pending
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20030082943A1 (en) * | 2001-10-31 | 2003-05-01 | Chen Kuo-Wen | Dustproof cover of connector slot |
| CN202186341U (en) * | 2011-07-13 | 2012-04-11 | 北汽福田汽车股份有限公司 | Plug, automobile interior trimming panel and automobile |
| CN206171469U (en) * | 2016-10-18 | 2017-05-17 | 苏州大成电子科技有限公司 | Carriage with light source interior trim part |
| CN106741832A (en) * | 2016-12-15 | 2017-05-31 | 中国航空工业集团公司西安飞机设计研究所 | A kind of adjustable interior trim lid of dock |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| RJ01 | Rejection of invention patent application after publication | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20190409 |