CN206982093U - Operating desk for airplane component assembling regulation - Google Patents
Operating desk for airplane component assembling regulation Download PDFInfo
- Publication number
- CN206982093U CN206982093U CN201720684946.3U CN201720684946U CN206982093U CN 206982093 U CN206982093 U CN 206982093U CN 201720684946 U CN201720684946 U CN 201720684946U CN 206982093 U CN206982093 U CN 206982093U
- Authority
- CN
- China
- Prior art keywords
- turntable
- top surface
- support
- slide rail
- supporter
- 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
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Abstract
For the operating desk of airplane component assembling regulation, including slide rail and turntable；The top surface of the overhead crane support is provided with driving, and overhead crane support is arranged on the top surface of base；The top surface centre position of the base is provided with supporter, and the top surface of the turntable support is provided with turntable, and turntable support is slided by the pulley of bottom surface and is arranged on slide rail；The top surface welding organism bracket of the supporter；The top connection organism bracket of the extension bar of the electric cylinder.For supporting airframe, and it is clamped by clamp system, turntable support at one is respectively installed in the both sides of body bracket, turntable is installed on the top of turntable support, clamp system is installed in the top surface of turntable, clamps aircraft both wings using this clamp system, and turntable support is slidably mounted on slide rail, therefore more flexibly aircraft both wings are arranged on airframe using its rotation and the sliding capability on slide rail, are easy to flexible modulation to install.
Description
Technical field
It the utility model is related to the operation of fitter's bench technical field, more particularly, to airplane component assembling regulation
Platform.
Background technology
For unmanned agricultural spraying machine in installation process, the installation process of its wing and fuselage is cumbersome, because fuselage is left
The scrambling of the wing shapes of right both sides, therefore typically support wing using wing supporting construction in installation process and lead to
Cross manpower or manipulator wing is arranged at left and right sides of fuselage on wall.
The inventors discovered that existing fuselage and wing mounting platform, complicated, flexible modulation poor performance, in reality
In installation process, large-scale lifting installation equipment is generally required, safe operation performance is poor.
Then, inventor in view of this, adhere to the relevant industries for many years it is abundant design and develop and the experience of actual fabrication,
Improvement is studied for existing structure and missing, there is provided a kind of airplane component assembling that is used for for being easy to flexible modulation is adjusted
Operating desk, to reach the purpose for having more more practical value.
Utility model content
The purpose of this utility model is to provide the operating desk for airplane component assembling regulation, to solve above-mentioned background
The existing fuselage proposed in technology and wing mounting platform, complicated, flexible modulation poor performance, in actual installation process
In, large-scale lifting installation equipment is generally required, the problem of safe operation performance difference.
The utility model is used for the purpose and effect of the operating desk of airplane component assembling regulation, by technology hand in detail below
Section is reached：
For the operating desk of airplane component assembling regulation, wherein, this is used for the operating desk of airplane component assembling regulation
Include：
Overhead crane support, driving, turntable support, body bracket, supporter, electric cylinder, slide rail and turntable；
The top surface of the overhead crane support is provided with driving, and overhead crane support is arranged on the top surface of base；The top of the base
Face centre position is provided with supporter, and the outer wall of supporter installs electric cylinder everywhere；The top surface peace of the turntable support
Equipped with turntable, and turntable support is slided by the pulley of bottom surface and is arranged on slide rail；The top surface welding organism of the supporter
Bracket；The top connection organism bracket of the extension bar of the electric cylinder.
Further, the body bracket is the string configuration of arc surface.
Further, the slide rail is semi arch structure, and it is fixed on ground cement table top by anchoring bolt.
With existing structure in comparison, the utility model has the following advantages that：
1. the utility model, as lifting airframe and the boom hoisting of wing, devises three supporting tables using driving
Face structure, it is middle for circular arc to improve the security in installation process instead of some traditional pure hoisting type mounting means
Strip body bracket, for supporting airframe, turntable support at one is respectively installed in the both sides of body bracket, rotated
The top of platform support is provided with turntable, and turntable support is slidably mounted on slide rail, thus using its rotation and
Aircraft both wings are more flexibly arranged on airframe by the sliding capability on slide rail, are easy to flexible modulation to install.
Brief description of the drawings
Fig. 1 is the utility model main structure diagram；
Fig. 2 is the utility model overlooking the structure diagram.
In figure：1st, overhead crane support, 2, driving, 3, turntable support, 4, body bracket, 5, supporter, 6, electric cylinder, 7,
Slide rail, 8, turntable.
Embodiment
Below, embodiment of the present utility model is will be explained in, the example is shown in the accompanying drawings and the description below.Although
The utility model will be described with reference to exemplary embodiment, it is to be understood that the description does not really want the utility model to be limited to this
Exemplary embodiment.On the contrary, the utility model will not only cover the exemplary embodiment, but also cover various replacements
, change, equivalent and other embodiment, its can be included in the spirit of the present utility model that appended claims are limited and
In the range of.
Referring to Fig. 1 to accompanying drawing 2, for the operating desk of airplane component assembling regulation, include：
Overhead crane support 1, driving 2, turntable support 3, body bracket 4, supporter 5, electric cylinder 6, slide rail 7 and turntable
8；
The top surface of overhead crane support 1 is provided with driving 2, and overhead crane support 1 is arranged on the top surface of base；Among the top surface of base
Position is provided with supporter 5, and the outer wall of supporter 5 installs electric cylinder 6 everywhere；The top surface of turntable support 3 is provided with rotation
Turntable 8, and turntable support 3 is slided by the pulley of bottom surface and is arranged on slide rail 7；The top surface welding organism bracket 4 of supporter 5；
The top connection organism bracket 4 of the extension bar of electric cylinder 6.
The preferred embodiment of operating desk described above for airplane component assembling regulation, wherein, body bracket 4 is circle
The string configuration of cambered surface, it is spacing to airframe progress for placing airframe, it is easy to follow-up wing to install.
The preferred embodiment of operating desk described above for airplane component assembling regulation, wherein, slide rail 7 is semi arch
Structure, it is fixed on ground cement table top by anchoring bolt, using the slide rail 7 of the two pieces of semicircular arc structures in left and right to left and right
Two turntable supports 3 are slidably installed, and turntable support 3 is had flexible adjustability, be easy to its support aircraft wing to
Region of interest on fuselage is installed；
The operation principle of the present embodiment：
Supporter 5, the top surface installation organism bracket 4 of supporter 5, on a left side for supporter 5 are installed on cement table top
Right both sides are separately installed with turntable support 3 at one, are provided with turntable 8 in the top surface of turntable support 3, utilize body bracket
4 and turntable 8 fuselage is supported with wing to the installation on fuselage, and the body bracket 4 of the top surface of supporter 5 is to use
Four electric cylinders 6 carry out telescoping support, therefore can be carried out according to the actual conditions for being laid in fuselage on body bracket 4 high
Degree regulation, corresponding, the turntable 8 of the top surface of turntable support 3 can also adjust angle, therefore can be to being supported on its top surface
It is mounted in the wing at left and right sides of fuselage and carries out angular adjustment, and turntable support is by pulley, is slidably mounted on arc
On the slide rail 7 of shape structure, therefore activity adjustment performance is more preferable.
It should be noted that the relation that is slidably connected for the pulley slide rail that the utility model is previously mentioned, the structure of rotation platform
And the operation principle and movement relation of electric cylinder are ripe prior art, the design does not remake the detailed of drawing and word
Explanation.
To sum up, although the utility model is described in detail with reference to the foregoing embodiments, for the technology of this area
For personnel, it can still modify to the technical scheme described in foregoing embodiments, or to which part technology
Feature carries out equivalent substitution, all within the spirit and principles of the utility model, any modification, equivalent substitution and improvements made
Deng should be included within the scope of protection of the utility model.
Claims (3)
1. the operating desk for airplane component assembling regulation, it is characterised in that：Described is used for airplane component assembling regulation
Operating desk include：
Overhead crane support (1), driving (2), turntable support (3), body bracket (4), supporter (5), electric cylinder (6), slide rail
And turntable (8) (7)；
The top surface of the overhead crane support (1) is provided with driving (2), and overhead crane support (1) is arranged on the top surface of base；The base
Top surface centre position supporter (5) is installed, and the outer wall installation of supporter (5) electric cylinder (6) everywhere；The turntable
The top surface of support (3) is provided with turntable (8), and turntable support (3) is slided by the pulley of bottom surface and is arranged on slide rail (7)；Institute
State the top surface welding organism bracket (4) of supporter (5)；The top connection organism of the extension bar of the electric cylinder (6) drags
Frame (4).
2. the operating desk according to claim 1 for airplane component assembling regulation, it is characterised in that：The body drags
Frame (4) is the string configuration of arc surface.
3. the operating desk according to claim 1 for airplane component assembling regulation, it is characterised in that：The slide rail
(7) it is semi arch structure, it is fixed on ground cement table top by anchoring bolt.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720684946.3U CN206982093U (en) | 2017-06-14 | 2017-06-14 | Operating desk for airplane component assembling regulation |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720684946.3U CN206982093U (en) | 2017-06-14 | 2017-06-14 | Operating desk for airplane component assembling regulation |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206982093U true CN206982093U (en) | 2018-02-09 |
Family
ID=61395348
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720684946.3U Expired - Fee Related CN206982093U (en) | 2017-06-14 | 2017-06-14 | Operating desk for airplane component assembling regulation |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206982093U (en) |
-
2017
- 2017-06-14 CN CN201720684946.3U patent/CN206982093U/en not_active Expired - Fee Related
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20180209 Termination date: 20180614 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |