CN205770171U - A kind of aircraft water system maintenance panel - Google Patents
A kind of aircraft water system maintenance panel Download PDFInfo
- Publication number
- CN205770171U CN205770171U CN201620514634.3U CN201620514634U CN205770171U CN 205770171 U CN205770171 U CN 205770171U CN 201620514634 U CN201620514634 U CN 201620514634U CN 205770171 U CN205770171 U CN 205770171U
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- Prior art keywords
- panel
- water system
- system maintenance
- aircraft water
- switch
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Abstract
This utility model relates to the design of aircraft water system complete equipment under unified central planning, particularly to a kind of aircraft water system maintenance panel, to meet the air-tightness requirement of maintenance panel.Aircraft water system maintenance panel includes: panel body, and integrally disposed on its panel have intended joint；Mounting box, it is sealingly disposed on the panel of panel body, it is internally formed closed cavity, predetermined switch seals and is integrated on the panel of mounting box, and the connection conductor part of predetermined switch is positioned in closed cavity, pass the panel of panel body again, it is thus possible to further predetermined switch to be carried out waterproof sealing, thus to meet the air-tightness requirement of maintenance panel.
Description
Technical field
This utility model relates to the design of aircraft water system complete equipment under unified central planning, particularly to a kind of aircraft water
System maintenance panel.
Background technology
Aircraft water system includes clean water system and waste water system, all includes maintenance panel, safeguards
It is generally used on panel arranging corresponding control switch and display lamp etc.；Based on using environment
Particularity, for how, maintenance panel is airtight, to avoid from the gas leakage of parts installation place or infiltration
It is particularly important.
Summary of the invention
The purpose of this utility model there is provided a kind of aircraft water system maintenance panel, with satisfied dimension
The air-tightness requirement of protection slab.
The technical solution of the utility model is:
A kind of aircraft water system maintenance panel, including:
Panel body, integrally disposed on the panel of described panel body have intended joint；
Mounting box, is sealingly disposed on the panel of described panel body, is internally formed closed cavity,
Predetermined switch seals and is integrated on the panel of described mounting box, and the connection of described predetermined switch is led
Line part is positioned in described closed cavity, then passes the panel of described panel body.
Preferably, the junction between the panel of described mounting box and described panel body is provided with
First seal gasket.
Preferably, on the panel of the described panel body being positioned at described closed cavity part, offer
Having wire to install through hole, the connection conductor part of described predetermined switch passes described by wire-threading device
Through hole installed by wire.
Preferably, described wire-threading device and described wire are installed and are provided with the second fluid sealant between through hole
Pad.
Preferably, described intended joint includes that imbitition connecter, described predetermined switch include adding water out
Close and drainage switch.
Preferably, described aircraft water system maintenance panel also includes:
Water yield display lamp, is integrally disposed on the panel of described panel body, and adds described in being positioned at
The vertical top of water swivel.
Preferably, taps is added and drainage switch is positioned at same level, and higher than described described in
The top of imbitition connecter outlet.
Preferably, described intended joint includes cleaning joint and pollution discharge joint, described predetermined switch
Including thermal switch and the scum cock of adding water.
Preferably, described hydro-thermal switch and scum cock are positioned at same level, and higher than described
Clean top and the top of described pollution discharge joint outlet of joint outlet.
The utility model has the advantage of:
In aircraft water system maintenance panel of the present utility model, on the panel of described panel body
Sealing is provided with mounting box, and predetermined switch seals again on the panel being integrated in mounting box, it is thus possible to
Further predetermined switch is carried out waterproof sealing, thus wants to meet the air-tightness of maintenance panel
Ask.
Accompanying drawing explanation
Fig. 1 is the structure of this utility model aircraft water one preferred embodiment of system maintenance panel
Schematic diagram；
Fig. 2 is A-A sectional view in Fig. 1；
Fig. 3 is the knot of this utility model aircraft water system another preferred embodiment of maintenance panel
Structure schematic diagram；
Fig. 4 is B-B sectional view in Fig. 3.
Detailed description of the invention
Clearer for the purpose making this utility model implement, technical scheme and advantage, below will
In conjunction with the accompanying drawing in this utility model embodiment, to the technical scheme in this utility model embodiment
It is further described in more detail.In the accompanying drawings, the most same or similar label represents phase
With or similar element or there is the element of same or like function.Described embodiment is this
The a part of embodiment of utility model rather than whole embodiments.Retouch below with reference to accompanying drawing
The embodiment stated is exemplary, it is intended to be used for explaining this utility model, and it is not intended that right
Restriction of the present utility model.Based on the embodiment in this utility model, ordinary skill people
The every other embodiment that member is obtained under not making creative work premise, broadly falls into this
The scope of utility model protection.Below in conjunction with the accompanying drawings embodiment of the present utility model is carried out in detail
Explanation.
In description of the present utility model, it is to be understood that term " " center ", " longitudinally ",
" laterally ", "front", "rear", "left", "right", " vertically ", " level ", " top ", " end ",
Orientation or the position relationship of the instruction such as " interior ", " outward " are based on orientation shown in the drawings or position
Relation, is for only for ease of description this utility model and simplifies description rather than instruction or hint
The device of indication or element must have specific orientation, with specific azimuth configuration and operation,
Therefore it is not intended that restriction to this utility model protection domain.
This utility model aircraft water system maintenance panel is done into one by 1 to Fig. 4 below in conjunction with the accompanying drawings
Step describes in detail.
This utility model provides a kind of aircraft water system maintenance panel, including panel body 1 with
And mounting box 2.
Integrally disposed on the panel of panel body 1 have intended joint；Mounting box 2, seals and arranges
(being fixed by bolt or rivet), on the panel of panel body 1, is internally formed closed cavity
21；Predetermined switch seals and is integrated on the panel of mounting box 2, and the connection wire of predetermined switch
Part is positioned in closed cavity 21, then passes the panel of panel body 1.This utility model leads to
Cross and predetermined switch is sealed again on the panel being integrated in mounting box 2, it is thus possible to further to predetermined
Switch carries out waterproof sealing, thus to meet the air-tightness requirement of maintenance panel.
It addition, to be provided with first close the junction between the panel of mounting box 2 and panel body 1
Potting pad 22, to strengthen sealing function, it is ensured that sealing property；Further, it is positioned at confined air
On the panel of the panel body 1 of chamber 21 part, offer wire and through hole, predetermined switch are installed
Connection conductor part through wire, through hole is installed by wire-threading device 23；Wire-threading device 23 with lead
Line is installed and is provided with the second seal gasket 24 between through hole, strengthens the sealing property of through hole.
In aircraft water system maintenance panel of the present utility model, intended joint and predetermined switch can
To be arranged as required to as multiple applicable structure.
The most as shown in Figure 1 and Figure 2, in an embodiment of utility model, preferably aircraft
Water system maintenance panel is clean water system maintenance panel, and intended joint includes imbitition connecter 31,
Predetermined switch includes adding taps 32 and drainage switch 33.It addition, also wrap on system maintenance panel
Include water yield display lamp 34, be integrally disposed on the panel of panel body 1, and be positioned to add water and connect
31 vertical tops.
Further, preferably add taps 32 and drainage switch 33 is positioned at same level, and high
Top in imbitition connecter 31 outlet, it is ensured that the security performance of predetermined switch.It addition, adding
Accompanying heating cushion 5 between water swivel 31 and panel, heating cushion 5 is embedded with electricity for inside silica gel plate
Heater strip, when electrical heating wire be energized after, heating, it is ensured that imbitition connecter under icing weather not
Freeze.
The most as shown in Figure 1 and Figure 2, in an embodiment of utility model, preferably aircraft
Water system maintenance panel is waste water system maintenance panel, and intended joint includes cleaning joint 41 He
Pollution discharge joint 42, predetermined switch includes add water thermal switch 43 and scum cock 44.It addition, water
Thermal switch 43 and scum cock 44 are positioned at same level, and export higher than cleaning joint 41
Top and pollution discharge joint 42 outlet top.
Equally, accompanying heating cushion 5 cleaning between joint 41 and panel, heating cushion 5 is silicon
Electrical heating wire it is embedded with inside offset plate, after electrical heating wire is energized, heating, it is ensured that imbitition connecter
Do not freeze under icing weather.
The above, detailed description of the invention the most of the present utility model, but guarantor of the present utility model
The scope of protecting is not limited thereto, and any those familiar with the art is at this utility model
In the technical scope disclosed, the change that can readily occur in or replacement, all should contain in this practicality new
Within the protection domain of type.Therefore, protection domain of the present utility model should be with described claim
Protection domain be as the criterion.
Claims (9)
1. an aircraft water system maintenance panel, it is characterised in that including:
Panel body (1), integrally disposed on the panel of described panel body (1) have predetermined connecing
Head；
Mounting box (2), is sealingly disposed on the panel of described panel body (1), internal shape
Becoming closed cavity (21), predetermined switch seals and is integrated on the panel of described mounting box (2),
And the connection conductor part of described predetermined switch is positioned in described closed cavity (21), then pass
The panel of described panel body (1).
Aircraft water system maintenance panel the most according to claim 1, it is characterised in that
Junction between the panel of described mounting box (2) and described panel body (1) is provided with
One seal gasket (22).
Aircraft water system maintenance panel the most according to claim 1, it is characterised in that
On the panel of the described panel body (1) being positioned at described closed cavity (21) part, offer
Having wire to install through hole, the connection conductor part of described predetermined switch is worn by wire-threading device (23)
Cross described wire and through hole is installed.
Aircraft water system maintenance panel the most according to claim 3, it is characterised in that
Described wire-threading device (23) and described wire are installed and are provided with the second seal gasket (24) between through hole.
5., according to the aircraft water system maintenance panel described in any one of claim 1-4, it is special
Levying and be, described intended joint includes imbitition connecter (31), and described predetermined switch includes adding water
Switch (32) and drainage switch (33).
Aircraft water system maintenance panel the most according to claim 5, it is characterised in that
Also include:
Water yield display lamp (34), is integrally disposed on the panel of described panel body (1), and
It is positioned at described imbitition connecter (31) vertically top.
Aircraft water system maintenance panel the most according to claim 6, it is characterised in that
Described add taps (32) and drainage switch (33) is positioned at same level, and higher than described
The top that imbitition connecter (31) exports.
8., according to the aircraft water system maintenance panel described in any one of claim 1-4, it is special
Levying and be, described intended joint includes cleaning joint (41) and pollution discharge joint (42), described
Predetermined switch includes add water thermal switch (43) and scum cock (44).
Aircraft water system maintenance panel the most according to claim 8, it is characterised in that
Described hydro-thermal switch (43) and scum cock (44) are positioned at same level, and higher than described
Clean joint (41) top that exports and top that described pollution discharge joint (42) exports.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620514634.3U CN205770171U (en) | 2016-05-31 | 2016-05-31 | A kind of aircraft water system maintenance panel |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620514634.3U CN205770171U (en) | 2016-05-31 | 2016-05-31 | A kind of aircraft water system maintenance panel |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205770171U true CN205770171U (en) | 2016-12-07 |
Family
ID=58138714
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620514634.3U Active CN205770171U (en) | 2016-05-31 | 2016-05-31 | A kind of aircraft water system maintenance panel |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205770171U (en) |
-
2016
- 2016-05-31 CN CN201620514634.3U patent/CN205770171U/en active Active
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant |