CN205522158U - Can put up aeronautical composite material finished piece frock of taking - Google Patents
Can put up aeronautical composite material finished piece frock of taking Download PDFInfo
- Publication number
- CN205522158U CN205522158U CN201620224413.2U CN201620224413U CN205522158U CN 205522158 U CN205522158 U CN 205522158U CN 201620224413 U CN201620224413 U CN 201620224413U CN 205522158 U CN205522158 U CN 205522158U
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- connecting hole
- frock
- hole
- utility
- pitman
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Abstract
The utility model discloses a can put up aeronautical composite material finished piece frock of taking has the supplementary working face of outer lane, middle work profile in the adj. Tabular frock, still include the connective bar, the connecting hole has been seted up on the supplementary working face, the connective bar inserts in the connecting hole, the connective bar both ends are the step, the cross section of the first step in the outside with the hole shape of connecting hole matches, and the terminal surface of second step is greater than the hole shape of connecting hole. The utility model has the advantages that: design standard connecting hole on the supplementary working face of frock, the simultaneous design is excellent with the metallic interconnect that the cooperation of standard connection hole was used for in the solidification process, the frock is connected through the connective bar each other and is placed, and convenient to use for reducing the time of preparation of finished piece frock before solidification, improves production efficiency, the creation of value in promoting the unit interval.
Description
Technical field
This utility model relates to the frock of a kind of aviation composite product.
Background technology
At present, the frock of aviation composite product is all in accordance with the size of type of product, individually designed, and its typical structure is near
It is similar to tabular.
When frock prepares before curing, need first to carry out taking jig rack, treat that jig rack could be incited somebody to action after building
Frock is placed in jig rack.Therefore the time of the solidification of hot-press tank technique of manufacture process is long, and production efficiency is low.
Utility model content
Utility model purpose: for the problems referred to above, the purpose of this utility model is to provide a kind of when saving curing process preparation
Between aviation composite product frock, to improve production efficiency.
Technical scheme: a kind of can the aviation composite product frock taken of frame, tabular frock has the back work of outer ring
Face, middle working surface, also include pitman, described back work face offer connecting hole, described pitman is inserted
Entering in described connecting hole, described pitman two ends are step, the cross section of the first step in outside and described connecting hole
Hole shape coupling, the end face of second step is more than the hole shape of described connecting hole.
Described connecting hole is any closed figures such as circle, square, rectangle, triangle.
Described connecting hole symmetry in frock is offered.
Beneficial effect: compared with prior art, the utility model has the advantages that: design mark on the back work face of frock
Quasi-connecting hole, design simultaneously and standard connecting hole with the use of metal pitman, in the curing process, frock phase
It is attached placing by pitman between Hu, easy to use, for reducing product frock time before curing, improve
Production efficiency, promotes the creation of value in the unit interval.
Accompanying drawing explanation
Fig. 1 is this utility model structural front view；
Fig. 2 is the A-A sectional view of Fig. 1；
Fig. 3 is pitman structural front view.
Detailed description of the invention
Below in conjunction with the accompanying drawings and specific embodiment, it is further elucidated with this utility model, it should be understood that these embodiments are only used for
Bright this utility model rather than limit scope of the present utility model, after having read this utility model, art technology
Personnel all fall within the application claims limited range to the amendment of the various equivalent form of values of the present utility model.
As illustrated in the accompanying drawings from 1 to 3, a kind of can the aviation composite product frock taken of frame, tabular frock is divided into the auxiliary of outer ring
Helping work surface 1, middle working surface 2, between back work face 1 and working surface 2 is ring-shaped gas-guiding trench 5,
Also include pitman 3.Offering connecting hole 4 on back work face 1, pitman 3 inserts in connecting hole 4.
Connecting hole 4 is any closed figures such as circle, square, rectangle, triangle, and connecting hole 4 is right in frock
Title is offered, and forms uniform distribution of force.Pitman 3 two ends are step, the cross section of the first step 31 in outside
Mating with the hole shape of connecting hole 4, the end face of second step 32, more than the hole shape of connecting hole 4, forms supporting surface.
Pitman 3 is metal material.
This utility model completely avoid the building of jig rack, at the Fixture Design initial stage, just in the auxiliary of frock
Design standard connecting hole on work surface, design corresponding pitman simultaneously, directly select pitman to carry out frock between the upper and lower
Connection place, reduce product frock time before curing, improve work efficiency greatly.
Claims (3)
1. one kind can the aviation composite product frock taken of frame, it is characterised in that: there is in tabular frock the auxiliary of outer ring
Help work surface (1), middle working surface (2), also include that pitman (3), described back work face are opened on (1)
Being provided with connecting hole (4), described pitman (3) inserts in described connecting hole (4), and described pitman (3) two ends are
Step, the cross section of the first step (31) in outside mates with the hole shape of described connecting hole (4), second step (32)
End face more than the hole shape of described connecting hole (4).
The most according to claim 1 a kind of can the aviation composite product frock taken of frame, it is characterised in that: institute
State any closed figures such as connecting hole (4) is circle, square, rectangle, triangle.
The most according to claim 1 a kind of can the aviation composite product frock taken of frame, it is characterised in that: institute
State connecting hole (4) symmetry in frock to offer.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620224413.2U CN205522158U (en) | 2016-03-22 | 2016-03-22 | Can put up aeronautical composite material finished piece frock of taking |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620224413.2U CN205522158U (en) | 2016-03-22 | 2016-03-22 | Can put up aeronautical composite material finished piece frock of taking |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205522158U true CN205522158U (en) | 2016-08-31 |
Family
ID=56784533
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620224413.2U Active CN205522158U (en) | 2016-03-22 | 2016-03-22 | Can put up aeronautical composite material finished piece frock of taking |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205522158U (en) |
-
2016
- 2016-03-22 CN CN201620224413.2U patent/CN205522158U/en active Active
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant |