CN206802012U - A kind of button for aircraft latches linkage - Google Patents
A kind of button for aircraft latches linkage Download PDFInfo
- Publication number
- CN206802012U CN206802012U CN201720425044.8U CN201720425044U CN206802012U CN 206802012 U CN206802012 U CN 206802012U CN 201720425044 U CN201720425044 U CN 201720425044U CN 206802012 U CN206802012 U CN 206802012U
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- China
- Prior art keywords
- briquetting
- button
- depression bar
- thumb
- linkage
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Abstract
A kind of button for aircraft latches linkage, including mounting seat, depression bar, button, the first briquetting, the second briquetting, Pressure-bar spring and two distance conversion centering blocks；Pass through pressing or release button and the first briquetting, the cooperation of the second briquetting, Pressure-bar spring, the rear end of distance conversion centering block is set to flip over or inwardly overturn reset, as long as applied to airplane compartment by each lock on compartment with being linked apart from the outer end of conversion centering block, it can be achieved with the folding of each lock, the storage devices such as dining car, storage tank are locked or passed in and out, it is simple in construction easy to operate, and lock is light more than existing handle, so as to mitigate the overall weight of aircraft.
Description
Technical field
It the utility model is related to a kind of lock linkage, more particularly to a kind of button lock linkage dress for aircraft
Put.
Background technology
The storage device such as dining car, storage tank is after use on aircraft, it is necessary to is pushed into the compartment on aircraft, then carries out
Locking, fix, at present, locking, fixed structure for storage devices such as dining car, storage tanks are typically all by multiple rotatable
Handle is locked, and by swing handle, is realized when each handle is kept off before the storage devices such as dining car, storage tank simultaneously
Locking, when each handle is away from before the storage devices such as dining car, storage tank, the storage device such as dining car, storage tank can be with
Compartment is freed in and out, so, when dining car or storage tank etc. will pass in and out compartment, certain dynamics need to be used to rotate more one or two simultaneously
Hand, operate cumbersome.
In addition, causing to release in order to avoid vibrations and force unbalance, generally require and be uniformly arranged on the periphery of compartment
Multiple handles, handle is generally large, heavier, so undoubtedly adds the overall weight of aircraft.
The content of the invention
The technical problems to be solved in the utility model is to provide a kind of button for aircraft and latches linkage, this
Button lock linkage structures are simple, easy to operate, and mitigate weight.The technical scheme of use is as follows：
A kind of button for aircraft latches linkage, it is characterized in that：Including mounting seat, depression bar, button, the first pressure
Block, the second briquetting, Pressure-bar spring and two distance conversion centering blocks；Mounting seat is provided with front panel and squab panel, is set in front panel
There is first through hole, squab panel is provided with the second through hole, and depression bar is arranged in mounting seat through first through hole, the second through hole；Button
Installed in one end of depression bar and in front panel outside；First briquetting is fixedly mounted on the front portion of depression bar and is in front panel
Inner side；Second briquetting is arranged on depression bar and can slided along depression bar, and the second briquetting is in the rear of the first briquetting；Pressure-bar spring
It is socketed on depression bar and between the second briquetting and squab panel；Two distance conversion centering blocks are hinged in mounting seat and difference
Both sides in depression bar, the front end of distance conversion centering block are between the first briquetting and the second briquetting.
Refer to close to the side of operator, refer to the side away from operator after above-mentioned before above-mentioned.
When pressing knob, depression bar rearward stretches out, drive the first briquetting rearward move, the first briquetting oppress two away from
From the front end of conversion centering block, flip over the rear end of distance conversion centering block, while the second briquetting compression Pressure-bar spring；Work as release
During knob, in the presence of Pressure-bar spring, the front end of the second briquetting top pressure two distance conversion centering block, make distance conversion centering block
Rear end inwardly overturns reset, meanwhile, the first briquetting and button reset；So, as long as by each lock on compartment
Linked with the outer end of distance conversion centering block, can be achieved with the folding of each lock, the storage devices such as dining car, storage tank are locked
Tight or disengaging, it is simple to operate, and lock is light more than existing handle, so as to mitigate the overall weight of aircraft.
Generally, above-mentioned button is additionally provided with button set, has protective effect to button.
Being hinged between above-mentioned distance conversion centering block and mounting seat can pass through connecting shaft or pin etc..
As preferred scheme of the present utility model, the distance conversion centering block includes short thumb, long thumb and be hinged hole position, is hinged
Hole position is in the junction of short thumb and long thumb, and described two distance conversion centering blocks are hinged on the installation by be hinged hole position respectively
On seat, short thumb is interposed between first briquetting and second briquetting, and long thumb is in the side of the depression bar.
As the further preferred scheme of the utility model, the short thumb and long thumb of the distance conversion centering block are be hinged hole position
For end points shape in an angle.
As the further preferred scheme of the utility model, the angle is more than 90 degree.
As the further preferred scheme of the utility model, short thumb, long thumb and the be hinged hole position of the distance conversion centering block
It is integrally formed.
As preferred scheme of the present utility model, in addition to depression bar axle sleeve, depression bar axle sleeve is before the mounting seat
On wallboard.
As preferred scheme of the present utility model, in addition to spring block, after spring block is arranged on the mounting seat
On wallboard.
The utility model compared with prior art, has the following advantages that：
By pressing or release button and the first briquetting, the cooperation of the second briquetting, Pressure-bar spring, make distance conversion centering block
Rear end flips over or inwardly overturn reset, as long as turning each lock on compartment and distance applied to airplane compartment
The outer end linkage of centering block is changed, the folding of each lock is can be achieved with, the storage devices such as dining car, storage tank is locked or entered
Go out, it is simple in construction easy to operate, and lock is light more than existing handle, so as to mitigate the overall weight of aircraft.
Brief description of the drawings
Fig. 1 is the structural representation of the utility model preferred embodiment.
Embodiment
It is described further below in conjunction with the accompanying drawings with preferred embodiment of the present utility model.
As shown in figure 1, a kind of button for aircraft latches linkage, including mounting seat 1, depression bar 2, depression bar axle sleeve
3rd, button 4, the first briquetting 5, the second briquetting 6, Pressure-bar spring 7,8, two distance conversion centering blocks 9 of spring block and two connecting shafts
10；Mounting seat 1 is provided with front panel 101 and squab panel 102, and front panel 101 is provided with first through hole 103, set on squab panel 102
There is the second through hole 104, depression bar 2 is arranged in mounting seat 1 through first through hole 103, the second through hole 104；Depression bar axle sleeve 3 is arranged on
In the front panel 101 of mounting seat 1；Button 4 is arranged on one end of depression bar 2 and the outside in front panel 101；First briquetting 5 is solid
Dingan County is mounted in the front portion of depression bar 2 and is in the inner side of front panel 101；Second briquetting 6 is arranged on depression bar 2 and can be along depression bar 2
Slide, the second briquetting 6 is in the rear of the first briquetting 5；Pressure-bar spring 7 is socketed on depression bar 2 and is in the second briquetting 6 and rear wall
Between plate 102；Spring block 8 is arranged on the squab panel 102 of mounting seat 1；Distance conversion centering block 9 includes short thumb 901, long thumb
902 and be hinged hole position 903, be hinged hole position 903 be in the junction of short thumb 901 and long thumb 902, and two distances are changed centering blocks 9 and divided
It is not hinged on by be hinged hole position 903 and connecting shaft 10 in mounting seat 1 and is respectively at the both sides of depression bar 2, short thumb 901 is interposed in the
Between one briquetting 5 and the second briquetting 6, long thumb 902 is in the side of depression bar 2, and short thumb 901 and long thumb 902 are be hinged hole position 903
End points forms one 135 degree of angle.
Refer to close to the side of operator, refer to the side away from operator after above-mentioned before above-mentioned.
Generally, above-mentioned button 4 is additionally provided with button set, has protective effect to button 4.
Short thumb 901, long thumb 902 and the be hinged hole position 903 of above-mentioned distance conversion centering block 9 are integrally formed.
When pressing knob 4, depression bar 2 rearward stretches out, and drives the first briquetting 5 rearward to move, the first briquetting 5 compressing two
The short thumb 901 of individual distance conversion centering block 9, flip over the long thumb 902 of distance conversion centering block 9, while the second briquetting 6 compression pressure
Bar spring 7；When unclamping knob 4, in the presence of Pressure-bar spring 7,6 top pressure of the second briquetting, two distances change the short of centering blocks 9
Thumb 901, make the inwardly upset reset of long thumb 902 of distance conversion centering block 9, meanwhile, the first briquetting 5 and button 4 reset；So,
As long as by each lock on compartment and the outer end linkage apart from conversion centering block 9, the folding of each lock is can be achieved with,
The storage devices such as dining car, storage tank are locked or passed in and out, it is simple to operate, and lock is light more than existing handle,
So as to mitigate the overall weight of aircraft.
Furthermore, it is necessary to illustrate, the specific embodiment, its each several part title etc. described in this specification can not
Together, the equivalent or simple change that all construction, feature and the principle described according to the utility model patent design are done, is included in this
In the protection domain of utility model patent.The utility model person of ordinary skill in the field can be to described specific reality
Example is applied to make various modifications or supplement or substitute using similar mode, without departing from structure of the present utility model or
Surmount scope defined in the claims, the scope of protection of the utility model all should be belonged to.
Claims (7)
1. a kind of button for aircraft latches linkage, it is characterized in that：Including mounting seat, depression bar, button, the first pressure
Block, the second briquetting, Pressure-bar spring and two distance conversion centering blocks；Mounting seat is provided with front panel and squab panel, is set in front panel
There is first through hole, squab panel is provided with the second through hole, and depression bar is arranged in mounting seat through first through hole, the second through hole；Button
Installed in one end of depression bar and in front panel outside；First briquetting is fixedly mounted on the front portion of depression bar and is in front panel
Inner side；Second briquetting is arranged on depression bar and can slided along depression bar, and the second briquetting is in the rear of the first briquetting；Pressure-bar spring
It is socketed on depression bar and between the second briquetting and squab panel；Two distance conversion centering blocks are hinged in mounting seat and difference
Both sides in depression bar, the front end of distance conversion centering block are between the first briquetting and the second briquetting.
2. button as claimed in claim 1 latches linkage, it is characterized in that：It is described distance conversion centering block include short thumb,
Long thumb and be hinged hole position, be hinged hole position are in the junction of short thumb and long thumb, and described two distance conversion centering blocks pass through hinge respectively
Connect hole position to be hinged in the mounting seat, short thumb is interposed between first briquetting and second briquetting, and long thumb is in institute
State the side of depression bar.
3. button as claimed in claim 2 latches linkage, it is characterized in that：The short thumb and length of the distance conversion centering block
Thumb using be hinged hole position as end points shape in an angle.
4. button as claimed in claim 3 latches linkage, it is characterized in that：The angle is more than 90 degree.
5. button as claimed in claim 2 latches linkage, it is characterized in that：The short thumb of the distance conversion centering block, length
Thumb and be hinged hole position are integrally formed.
6. button as claimed in claim 1 latches linkage, it is characterized in that：Also include depression bar axle sleeve, depression bar axle sleeve peace
In the front panel of the mounting seat.
7. button as claimed in claim 1 latches linkage, it is characterized in that：Also include spring block, spring block peace
On the squab panel of the mounting seat.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720425044.8U CN206802012U (en) | 2017-04-21 | 2017-04-21 | A kind of button for aircraft latches linkage |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720425044.8U CN206802012U (en) | 2017-04-21 | 2017-04-21 | A kind of button for aircraft latches linkage |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206802012U true CN206802012U (en) | 2017-12-26 |
Family
ID=60732170
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720425044.8U Active CN206802012U (en) | 2017-04-21 | 2017-04-21 | A kind of button for aircraft latches linkage |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206802012U (en) |
-
2017
- 2017-04-21 CN CN201720425044.8U patent/CN206802012U/en active Active
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant |