CN207985235U - A kind of cylinder assembly assembly jig suitable for aviation assembly - Google Patents
A kind of cylinder assembly assembly jig suitable for aviation assembly Download PDFInfo
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- CN207985235U CN207985235U CN201721880611.5U CN201721880611U CN207985235U CN 207985235 U CN207985235 U CN 207985235U CN 201721880611 U CN201721880611 U CN 201721880611U CN 207985235 U CN207985235 U CN 207985235U
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- assembly
- aviation
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- support
- bottom plate
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Abstract
The utility model provides a kind of cylinder assembly assembly jig suitable for aviation assembly, including bottom plate, bottom end abutment sleeve, multiple main supports, multiple secondary supports and multiple support plates；Multiple main supports are arranged in bottom plate upper surface, multiple secondary supports are arranged in the front of multiple main supports, multiple support plates are arranged at multiple main support rears, bottom end abutment sleeve is arranged in front of multiple secondary supports, through-hole is equipped among the abutment sleeve of bottom end, bottom plate lower face is equipped with multiple pulleys.A kind of cylinder assembly assembly jig suitable for aviation assembly of the utility model, to pass through the requirement of the technology of planning and market to assembling structure entirety, vertical structure is used when design, and then locating shaft vertical display, for fixing lower end, it solves shaft problem on deformation, ensures the concentricity of locating shaft two ends, increase the assembly precision between workpiece.
Description
Technical field
The utility model belongs to aviation assembly tooling field, more particularly, to a kind of cylinder assembly suitable for aviation assembly
Assembly jig.
Background technology
Cylinder assembly is complicated, and very high to the requirement of the concentricity of both ends bulkhead, and it is fixed with a perforative axis to need
The bulkhead at this both ends of position, the locating shaft are influenced that one end can only be fixed by structure, otherwise will be had an impact to the undercarriage of product, however
Being fixed when axis can be caused one end sagging, is influenced concentricity when one section of transverse direction is put due to the influence of gravity again.
Invention content
In view of this, the utility model is directed to a kind of cylinder assembly assembly jig suitable for aviation assembly, with logical
Crossing the technology requirement in the planning to assembling structure entirety and market, when design, uses vertical structure, and then locating shaft vertical display,
For fixing lower end, solves shaft problem on deformation, ensure the concentricity of locating shaft two ends, increase the assembly essence between workpiece
Degree.
In order to achieve the above objectives, the technical solution of the utility model is realized in：
A kind of cylinder assembly assembly jig suitable for aviation assembly, including bottom plate, bottom end abutment sleeve, multiple main branch
Frame, multiple secondary supports and multiple support plates；
Multiple main supports are arranged in the bottom plate upper surface, and multiple secondary supports are arranged in multiple
The front of the main support, multiple support plates are arranged at multiple main support rears, and the bottom end abutment sleeve is set
It sets in front of multiple secondary supports, through-hole is equipped among the bottom end abutment sleeve, the bottom plate lower face is equipped with multiple cunnings
Wheel.
Further, there are six the main support is set, six main support Rotating with Uniform are arranged in the bottom plate
Upper surface.
Further, it is equipped with cross beam frame on each main support.
Further, there are six the secondary support is set, each main support front is correspondingly arranged a pair
Holder.
Further, there are six the support plate is set, each equal rear of main support is correspondingly arranged a branch
Fagging.
Further, there are six the pulley is set, six pulley Rotating with Uniform are arranged in the bottom plate lower end
Face.
Further, each pulley be can brake sheave.
Compared with the existing technology, a kind of cylinder assembly assembly jig tool suitable for aviation assembly described in the utility model
There is following advantage：
A kind of cylinder assembly assembly jig suitable for aviation assembly of the present invention, is placed with main support and secondary support
Workpiece positions upper workpiece by bottom end abutment sleeve and bottom workpieces, main support and secondary support Rotating with Uniform is arranged in bottom
On plate, positioning datum up and down is provided for workpiece, solving locating shaft is influenced that one end can only be fixed by structure.
Description of the drawings
The attached drawing for constituting the part of the utility model is used to provide a further understanding of the present invention, this practicality is new
The illustrative embodiments and their description of type are not constituted improper limits to the present invention for explaining the utility model.
In attached drawing：
Fig. 1 is a kind of cylinder assembly assembly jig signal suitable for aviation assembly described in the utility model embodiment
Figure；
Fig. 2 is a kind of another angle of cylinder assembly assembly jig suitable for aviation assembly described in the utility model embodiment
Spend structural schematic diagram.
Reference sign：
101- bottom plates；201- main supports；202- support plates；203- cross beam frames；301- secondary supports；The bottom ends 401- positioning sleeve
Cylinder；402- through-holes.
Specific implementation mode
It should be noted that in the absence of conflict, the feature in the embodiments of the present invention and embodiment can
To be combined with each other.
In the description of the present invention, it should be understood that term "center", " longitudinal direction ", " transverse direction ", "upper", "lower",
The orientation or positional relationship of the instructions such as "front", "rear", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outside" is
It is based on the orientation or positional relationship shown in the drawings, is merely for convenience of describing the present invention and simplifying the description, rather than indicate
Or imply that signified device or element must have a particular orientation, with specific azimuth configuration and operation, therefore cannot understand
For limitations of the present invention.In addition, term " first ", " second " etc. are used for description purposes only, and should not be understood as indicating
Or it implies relative importance or implicitly indicates the quantity of indicated technical characteristic." first ", " second " etc. are defined as a result,
Feature can explicitly or implicitly include one or more this feature.It is in the description of the present invention, unless another
It is described, the meaning of " plurality " is two or more.
In the description of the present invention, it should be noted that unless otherwise clearly defined and limited, term " is pacified
Dress ", " connected ", " connection " shall be understood in a broad sense, for example, it may be being fixedly connected, may be a detachable connection, or integrally
Connection；It can be mechanical connection, can also be electrical connection；Can be directly connected, can also indirectly connected through an intermediary,
It can be the connection inside two elements.For the ordinary skill in the art, on being understood by concrete condition
State the concrete meaning of term in the present invention.
The utility model will be described in detail below with reference to the accompanying drawings and embodiments.
A kind of cylinder assembly assembly jig suitable for aviation assembly, as shown in Figure 1, including bottom plate 101, bottom end positioning sleeve
Cylinder 401, multiple main supports 201, multiple secondary supports 301 and multiple support plates 202；
Multiple main supports 201 are arranged in 101 upper surface of bottom plate, and multiple secondary supports 301 are arranged in multiple masters
The front of holder 201, multiple support plates 202 are arranged at 201 rear of multiple main supports, and bottom end abutment sleeve 401 is arranged more
301 front of a secondary support, 401 centre of bottom end abutment sleeve are equipped with through-hole 402, and 101 lower face of bottom plate is equipped with multiple pulleys 501.
There are six main support 201 is set, six 201 Rotating with Uniform of main support are arranged in 101 upper surface of bottom plate.Each master
Cross beam frame 203 is equipped on holder 201.There are six secondary support 301 is set, the front of each main support 201 is correspondingly arranged one
Secondary support 301.
There are six support plate 202 is set, 201 equal rear of each main support is correspondingly arranged a support plate 202.Pulley 501
If there are six, six 501 Rotating with Uniform of pulley are arranged in 101 lower face of bottom plate, and each pulley 501 is that can brake cunning
Wheel, frame convenient for assembly are moved and are positioned.
The working method of this example
By the way that workpiece is placed on main support 201 on secondary support 301, bottom is placed on 301 lower end angled end-face of secondary support
Workpiece, 301 upper ends upper workpiece of main support 201 and secondary support are placed on through-hole 402 by main shaft among assembly fixture vertically
The location of workpiece of top and the bottom is fixed for inside.
The above is only the preferred embodiments of the present utility model only, is not intended to limit the utility model, all in this practicality
Within novel spirit and principle, any modification, equivalent replacement, improvement and so on should be included in the guarantor of the utility model
Within the scope of shield.
Claims (7)
1. a kind of cylinder assembly assembly jig suitable for aviation assembly, it is characterised in that：It is positioned including bottom plate (101), bottom end
Sleeve (401), multiple main supports (201), multiple secondary supports (301) and multiple support plates (202)；
Multiple main supports (201) are arranged in the bottom plate (101) upper surface, and multiple secondary supports (301) are arranged
Row are arranged in the front of multiple main supports (201), and multiple support plates (202) are arranged at multiple main supports
(201) rear, bottom end abutment sleeve (401) setting is in front of multiple secondary supports (301), the bottom end abutment sleeve
(401) intermediate to be equipped with through-hole (402), bottom plate (101) lower face is equipped with multiple pulleys (501).
2. a kind of cylinder assembly assembly jig suitable for aviation assembly according to claim 1, it is characterised in that：It is described
There are six main support (201) is set, six main support (201) Rotating with Uniform are arranged in the bottom plate (101) upper surface.
3. a kind of cylinder assembly assembly jig suitable for aviation assembly according to claim 2, it is characterised in that：It is each
It is equipped with cross beam frame (203) on the main support (201).
4. a kind of cylinder assembly assembly jig suitable for aviation assembly according to claim 1, it is characterised in that：It is described
There are six secondary support (301) is set, a secondary support (301) is correspondingly arranged in front of each main support (201).
5. a kind of cylinder assembly assembly jig suitable for aviation assembly according to claim 1, it is characterised in that：It is described
There are six support plate (202) is set, each main support (201) rear is correspondingly arranged a support plate (202).
6. a kind of cylinder assembly assembly jig suitable for aviation assembly according to claim 1, it is characterised in that：It is described
There are six pulley (501) is set, six pulley (501) Rotating with Uniform are arranged in the bottom plate (101) lower face.
7. a kind of cylinder assembly assembly jig suitable for aviation assembly according to claim 6, it is characterised in that：It is each
The pulley (501) is can brake sheave.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721880611.5U CN207985235U (en) | 2017-12-28 | 2017-12-28 | A kind of cylinder assembly assembly jig suitable for aviation assembly |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721880611.5U CN207985235U (en) | 2017-12-28 | 2017-12-28 | A kind of cylinder assembly assembly jig suitable for aviation assembly |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207985235U true CN207985235U (en) | 2018-10-19 |
Family
ID=63818203
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201721880611.5U Active CN207985235U (en) | 2017-12-28 | 2017-12-28 | A kind of cylinder assembly assembly jig suitable for aviation assembly |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207985235U (en) |
-
2017
- 2017-12-28 CN CN201721880611.5U patent/CN207985235U/en active Active
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