CN209027765U - A kind of fixed mechanism and vibration device for simulating airborne indicator actual installation - Google Patents
A kind of fixed mechanism and vibration device for simulating airborne indicator actual installation Download PDFInfo
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- CN209027765U CN209027765U CN201821935691.4U CN201821935691U CN209027765U CN 209027765 U CN209027765 U CN 209027765U CN 201821935691 U CN201821935691 U CN 201821935691U CN 209027765 U CN209027765 U CN 209027765U
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- panel
- fixed mechanism
- bottom plate
- plate
- airborne indicator
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Abstract
The utility model discloses a kind of fixed mechanisms and vibration device for simulating airborne indicator actual installation, the fixed mechanism includes bottom plate, multiple side plates and the panel being obliquely installed on the bottom plate, multiple side plates are vertically arranged on the bottom plate, and the side wall of multiple side plates is wherein fixedly connected with the panel on one side；Wherein, through slot is provided on the panel, airborne indicator, which is capable of fixing, to be embedded in the through slot, and the slanted angle of the panel and the bottom plate is identical as setting angle of the airborne indicator in aircraft cockpit.In this way, setting angle of the airborne indicator on panel is identical as the setting angle in actual aircraft cockpit, then places it in simulated experiment, can actually use operating condition to airborne indicator and be simulated in advance, to find and overcome the problems, such as to exist in applying working condition, hidden danger of quality is reduced.
Description
Technical field
The utility model relates to airborne indicator ancillary equipment fields, and in particular, to a kind of simulation airborne indicator is real
The fixed mechanism and vibration device of border installation.
Background technique
In military airborne display field, liquid crystal display was almost shown instead of former mechanical pointer.But liquid crystal
Display will work in cockpit domestic demand under conditions of exceedingly odious for a long time, need to bear violent vibration.Violent in this way
Effect of vibration under, vibration pressure is easy to act on liquid crystal display, and resultant harmonic vibration energy will lead to liquid
The display effect of crystal display screen is deteriorated, such as will appear bracing wire or hickie etc..Therefore, it assembles and completes in LCD MODULE
Afterwards, it needs to carry out vibration test to product.
Vibration test is done, primarily on condition that, a set of vibration device is needed to fix product.Some liquid crystal displays are in aircraft
Upper installation has angle requirement, and present vibration tong does not account for actual installation direction of the product in aircraft cockpit.
The vibration device of design is the vertical direction of tri- axis of X, Y, Z, can not simulate airbome liquid crystal display in actual use process
Middle Impact direction cannot effectively simulate true use environment, cannot also estimate to true service condition, thus gram
The problem of taking real applying working condition.This will lead to, and airbome liquid crystal display is in true prolonged use process
In there are hidden danger of quality.
Therefore, a kind of vibration device for simulating airborne indicator actual installation how is provided, thus to airborne indicator reality
Border applying working condition is simulated in advance, to find and overcome the problems, such as to exist in applying working condition, is reduced hidden danger of quality, is current
Urgent problem to be solved.
Utility model content
The purpose of the utility model is to provide it is a kind of simulate airborne indicator actual installation fixed mechanism and vibration device,
The actual installation mode for recording display can be simulated, so that airborne indicator actual use operating condition is simulated in advance, with
It was found that and overcome the problems, such as can exist in applying working condition, reduce hidden danger of quality.
To achieve the goals above, the utility model provides a kind of fixed mechanism for simulating airborne indicator actual installation,
The fixed mechanism includes bottom plate, multiple side plates and the panel being obliquely installed on the bottom plate, and multiple side plates are perpendicular
It is directly set on the bottom plate, and the side wall of multiple side plates is wherein fixedly connected with the panel on one side；Wherein, institute
It states and is provided with through slot on panel, airborne indicator, which is capable of fixing, to be embedded in the through slot, and the panel and the bottom
The slanted angle of plate is identical as setting angle of the airborne indicator in aircraft cockpit.
Preferably, the fixed mechanism further includes multiple stiffening plates, the stiffening plate be fixedly installed on the bottom plate and
It is wherein fixedly connected on one side with the side plate respectively.
Preferably, the side plate is two, and is separately positioned on the ipsilateral of the panel.
Preferably, multiple mounting holes are provided on the bottom plate, the side plate, panel and stiffening plate connect with the bottom plate
Multiple threaded holes are provided on the side wall of touching, multiple screws to match with the threaded hole can pass through the mounting hole for institute
State side plate, panel and stiffening plate and the bottom plate bolt.
Preferably, it is provided with multiple through holes on the panel, is set on the side wall that the side plate is in contact with the panel
Multiple screw holes are equipped with, multiple nuts to match with the screw hole can pass through the through hole for the side plate and the panel
Bolt.
Preferably, it is provided with multiple through-holes on the side plate, is set on the side wall that the stiffening plate is in contact with the side plate
Multiple bolts hole are equipped with, multiple bolts to match with the bolt hole can pass through the through-hole and add the side plate with described
Strong plate bolt.
Preferably, multiple drillings are provided on the bottom plate.
Preferably, the panel can be with the airborne indicator bolt.
The utility model also provides a kind of vibration device for simulating airborne indicator actual installation, and the vibration device includes
Previously described fixed mechanism and vibrating mechanism with platform, wherein the bottom plate of the fixed mechanism is capable of fixing setting and exists
On the platform of the vibrating mechanism.
Preferably, the platform bolt that the fixed mechanism passes through the drilling and the vibrating mechanism.
The utility model provides a kind of fixed mechanism for simulating airborne indicator actual installation, and the fixed mechanism includes bottom
Plate, multiple side plates and the panel being obliquely installed on the bottom plate, multiple side plates are vertically arranged on the bottom plate,
And the side wall of multiple side plates is wherein fixedly connected with the panel on one side；Wherein, perforation is provided on the panel
Slot, airborne indicator, which is capable of fixing, to be embedded in the through slot, and the slanted angle of the panel and the bottom plate with it is described
Setting angle of the airborne indicator in aircraft cockpit is identical.In this way, airborne indicator is embedded in the through slot, it is airborne
Setting angle of the display on panel is identical as the setting angle in actual aircraft cockpit, and it is real then to place it in simulation
In testing, operating condition can be actually used to airborne indicator and be simulated in advance, to find and overcome in applying working condition existing for meeting
Problem reduces hidden danger of quality.
Other feature and advantage of the utility model will the following detailed description will be given in the detailed implementation section.
Detailed description of the invention
Attached drawing is to be used to provide a further understanding of the present invention, and constitute part of specification, and following
Specific embodiment be used to explain the utility model together, but do not constitute limitations of the present invention.In the accompanying drawings:
Fig. 1 is the structural schematic diagram for simulating the fixed mechanism of airborne indicator actual installation；
Fig. 2 is the structural scheme of mechanism for simulating the vibration device of airborne indicator actual installation.
Description of symbols
1 bottom plate, 2 side plate
3 panel, 4 through slot
5 stiffening plate, 6 bolt
7 platforms
Specific embodiment
Specific embodiment of the present utility model is described in detail below in conjunction with attached drawing.It should be understood that herein
Described specific embodiment is only used for describing and explaining the present invention, and is not intended to limit the utility model.
In the present invention, in the absence of explanation to the contrary, the side that " upper and lower, side, bottom " etc. is included in the term
Position word only represent orientation of the term under normal service condition, or be those skilled in the art understand that be commonly called as, without that should regard
For the limitation to the term.
The utility model provides a kind of fixed mechanism for simulating airborne indicator actual installation, and the fixed mechanism includes bottom
Plate 1, multiple side plates 2 and the panel 3 being obliquely installed on the bottom plate 1, multiple side plates 2 are vertically arranged at the bottom
On plate 1, and the side wall of multiple side plates 2 is wherein fixedly connected with the panel 3 on one side；Wherein, it is set on the panel 3
It is equipped with through slot 4, airborne indicator, which is capable of fixing, to be embedded in the through slot 4, and the panel 3 and the bottom plate 1 incline
Oblique angle is identical as setting angle of the airborne indicator in aircraft cockpit.In this way, airborne indicator is embedded at described
In through slot 4, airborne indicator is identical as the setting angle in actual aircraft cockpit in the setting angle on panel 3, so
After place it in simulated experiment, can to airborne indicator actually use operating condition be simulated in advance, made with finding and overcoming
The problem of with that can exist in operating condition, reduces hidden danger of quality.
In a kind of preferred embodiment of the utility model, the fixed mechanism further includes multiple stiffening plates 5, described to add
Strong plate 5 is fixedly installed on the bottom plate 1 and is wherein fixedly connected on one side with the side plate 2 respectively.In this way, may make that this is solid
It is more firm to determine mechanism.
In a kind of preferred embodiment of the utility model, the side plate 2 is two, and is separately positioned on the panel
3 it is ipsilateral.Such set-up mode, conducive to the installation for recording display.
In a kind of preferred embodiment of the utility model, multiple mounting holes, the side plate are provided on the bottom plate 1
2, it is provided with multiple threaded holes on the side wall that panel 3 and stiffening plate 5 are in contact with the bottom plate 1, it is multiple with the threaded hole phase
Matched screw can pass through the mounting hole for the side plate 2, panel 3 and stiffening plate 5 and 1 bolt of bottom plate.In this way,
It may make dismounting more flexible.
In a kind of preferred embodiment of the utility model, multiple through holes, the side plate are provided on the panel 3
Multiple screw holes are provided on 2 side walls being in contact with the panel 3, it is multiple to pass through institute with the nut that the screw hole matches
Through hole is stated by the side plate 2 and 3 bolt of panel.In this way, may make dismounting more flexible.
In a kind of preferred embodiment of the utility model, multiple through-holes, the stiffening plate are provided on the side plate 2
Multiple bolts hole are provided on 5 side walls being in contact with the side plate 2, multiple bolts 6 to match with the bolt hole can
Across the through-hole by the side plate 2 and 5 bolt of stiffening plate.In this way, may make dismounting more flexible.
In a kind of preferred embodiment of the utility model, multiple drillings are provided on the bottom plate 1.In this way, being conducive to
The connection of fixed mechanism and other analog machines.
In a kind of preferred embodiment of the utility model, the panel 3 can be with the airborne indicator bolt.
So that the airborne indicator dismounting is more convenient.
The utility model also provides a kind of vibration device for simulating airborne indicator actual installation, and the vibration device includes
Previously described fixed mechanism and vibrating mechanism with platform 7, wherein the bottom plate 1 of the fixed mechanism is capable of fixing setting
On the platform 7 of the vibrating mechanism.In this way, airborne indicator is embedded in the through slot 4, airborne indicator is in panel
Setting angle on 3 is identical as the setting angle in actual aircraft cockpit, then places it in the flat of the vibrating mechanism
On platform 7, operating condition can be actually used to airborne indicator and carry out vibrating preparatory simulation, can deposited with finding and overcoming in applying working condition
The problem of, reduce hidden danger of quality.
In a kind of preferred embodiment of the utility model, the fixed mechanism passes through the drilling and the bobbing machine
7 bolt of platform of structure.So that dismounting is more convenient.
Preferred embodiments of the present invention, still, the utility model and unlimited are described in detail in conjunction with attached drawing above
Detail in above embodiment can be to the skill of the utility model in the range of the technology design of the utility model
Art scheme carries out a variety of simple variants, these simple variants belong to the protection scope of the utility model.
It is further to note that specific technical features described in the above specific embodiments, in not lance
It in the case where shield, can be combined in any appropriate way, in order to avoid unnecessary repetition, the utility model is to each
No further explanation will be given for the possible combination of kind.
In addition, any combination can also be carried out between a variety of different embodiments of the utility model, as long as it is not disobeyed
The thought for carrying on the back the utility model, equally should be considered as content disclosed in the utility model.
Claims (10)
1. a kind of fixed mechanism for simulating airborne indicator actual installation, which is characterized in that the fixed mechanism includes bottom plate
(1), multiple side plates (2) and the panel (3) being obliquely installed on the bottom plate (1), multiple side plates (2) are vertically arranged
In on the bottom plate (1), and the side wall of multiple side plates (2) is wherein fixedly connected with the panel (3) on one side；Its
In, it is provided with through slot (4) on the panel (3), airborne indicator, which is capable of fixing, to be embedded in the through slot (4), and institute
The slanted angle for stating panel (3) and the bottom plate (1) is identical as setting angle of the airborne indicator in aircraft cockpit.
2. fixed mechanism according to claim 1, which is characterized in that the fixed mechanism further includes multiple stiffening plates (5),
The stiffening plate (5) is fixedly installed on the bottom plate (1) and is wherein fixedly connected on one side with the side plate (2) respectively.
3. fixed mechanism according to claim 2, which is characterized in that the side plate (2) is two, and is separately positioned on institute
State the ipsilateral of panel (3).
4. fixed mechanism according to claim 3, which is characterized in that be provided with multiple mounting holes, institute on the bottom plate (1)
It states and is provided with multiple threaded holes on the side wall that side plate (2), panel (3) and stiffening plate (5) are in contact with the bottom plate (1), it is multiple
The screw to match with the threaded hole can pass through the mounting hole by the side plate (2), panel (3) and stiffening plate (5) and
Bottom plate (1) bolt.
5. fixed mechanism according to claim 4, which is characterized in that be provided with multiple through holes, institute on the panel (3)
It states and is provided with multiple screw holes on the side wall that side plate (2) is in contact with the panel (3), multiple nuts to match with the screw hole
The through hole can be passed through by the side plate (2) and the panel (3) bolt.
6. fixed mechanism according to claim 5, which is characterized in that multiple through-holes are provided on the side plate (2), it is described
Multiple bolts hole are provided on the side wall that stiffening plate (5) is in contact with the side plate (2), what the multiple and bolt hole matched
Bolt (6) can pass through the through-hole for the side plate (2) and the stiffening plate (5) bolt.
7. fixed mechanism according to claim 6, which is characterized in that be provided with multiple drillings on the bottom plate (1).
8. fixed mechanism according to claim 7, which is characterized in that the panel (3) can be with the airborne indicator
Bolt.
9. a kind of vibration device for simulating airborne indicator actual installation, which is characterized in that the vibration device includes that right is wanted
It seeks the described in any item fixed mechanisms of 1-8 and has the vibrating mechanism of platform (7), wherein bottom plate (1) energy of the fixed mechanism
It is enough fixed on the platform (7) of the vibrating mechanism.
10. vibration device according to claim 9, which is characterized in that the fixed mechanism by it is described drilling with it is described
Platform (7) bolt of vibrating mechanism.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821935691.4U CN209027765U (en) | 2018-11-22 | 2018-11-22 | A kind of fixed mechanism and vibration device for simulating airborne indicator actual installation |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821935691.4U CN209027765U (en) | 2018-11-22 | 2018-11-22 | A kind of fixed mechanism and vibration device for simulating airborne indicator actual installation |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN209027765U true CN209027765U (en) | 2019-06-25 |
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ID=66910082
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201821935691.4U Active CN209027765U (en) | 2018-11-22 | 2018-11-22 | A kind of fixed mechanism and vibration device for simulating airborne indicator actual installation |
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| CN (1) | CN209027765U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111855117A (en) * | 2020-07-21 | 2020-10-30 | 中国石油天然气集团有限公司 | Three-dimensional vector vibration clamp |
-
2018
- 2018-11-22 CN CN201821935691.4U patent/CN209027765U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111855117A (en) * | 2020-07-21 | 2020-10-30 | 中国石油天然气集团有限公司 | Three-dimensional vector vibration clamp |
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