CN205464152U - Aircraft riveter encoder axle - Google Patents
Aircraft riveter encoder axle Download PDFInfo
- Publication number
- CN205464152U CN205464152U CN201620257431.0U CN201620257431U CN205464152U CN 205464152 U CN205464152 U CN 205464152U CN 201620257431 U CN201620257431 U CN 201620257431U CN 205464152 U CN205464152 U CN 205464152U
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- CN
- China
- Prior art keywords
- encoder axle
- encoder
- axle body
- axle
- riveter
- 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.)
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Abstract
The utility model discloses an aircraft riveter encoder axle, its structure includes encoder axle body (1) and connecting axle (2) that integrative casting formed, and boss (3) are established to encoder axle body (1) and connecting axle (2) junction, and fabrication hole (4) are established at encoder axle body (1) middle part, and connecting axle (2) center is mounting hole (5), fixed orifices (6) of establishing round evenly distributed outside the encoder axle body (1). The utility model discloses an advantage: be equipped with aircraft riveter compact structure, stable performance, the convenient operation safety of this encoder axle, have automatic coordinate system, realize that automatic fixed position rotation punches, it is accurate high -efficient, sturdy and durable.
Description
Technical field
The utility model relates to airplane riveting machine encoder axle.
Background technology
In the manufacture of aircraft produces, being Manual punching before rivet hole, efficiency is low, and speed is slow,
There is also the inaccurate situation of punch position.
Rivet driver is based on the riveting equipment that cold rolling principle develops, and referring to can be with rivet article riveting
Pick up mechanized equipment.Common are pneumatic, oil pressure and electronic, single head and double end equal-specification model.
Common type mainly has automatic riveter and riveter.
But common rivet driver insufficient strength, and the high-precision requirement in airplane riveting hole cannot be met.
Summary of the invention
The utility model proposes airplane riveting machine encoder axle, play purpose and be intended to overcome existing skill
Art above shortcomings, it is achieved High Precision Automatic position rotating is punched.
Technical solution of the present utility model: airplane riveting machine encoder axle, its structure includes one
The encoder axle body of body casting and connecting shaft, encoder axle body and connecting shaft junction set
Boss, sets fabrication hole in the middle part of encoder axle body, connecting shaft center is installing hole, and encoder axle is originally
External side sets the fixing hole that a circle is evenly distributed.
Preferably, the quantity of described fixing hole is 6.
Preferably, a circle boss draw-in groove is set by described boss.
Preferably, described connecting shaft end sets a circle draw-in groove.
Advantage of the present utility model: with the airplane riveting machine compact conformation of this encoder axle, performance
Stable, easy and safe to operate, have from moving coordinate system, it is achieved automatic positioning rotating punches, accurately
Efficiently, sturdy and durable.
Accompanying drawing explanation
Fig. 1 is the structural representation of airplane riveting machine encoder axle.
Fig. 2 is the side view of Fig. 1.
In figure 1 be encoder axle body, 2 be connecting shaft, 3 be boss, 4 be fabrication hole, 5
It is installing hole, 6 is fixing hole, 7 is boss draw-in groove, 8 is draw-in groove.
Detailed description of the invention
Below in conjunction with embodiment and detailed description of the invention, this utility model made further details of theory
Bright.
As shown in Figure 1, 2, airplane riveting machine encoder axle, its structure includes being integrally cast
Encoder axle body 1 and connecting shaft 2, encoder axle body 1 and connecting shaft 2 junction set boss 3,
Setting fabrication hole 4 in the middle part of encoder axle body 1, connecting shaft 2 center is installing hole 5, and encoder axle is originally
The fixing hole 6 that a circle is evenly distributed is set outside body 1.
The quantity of described fixing hole 6 is 6, is used for fixing.
Described boss 3 is other sets a circle boss draw-in groove 7, facilitates clamping to install.
Described connecting shaft 2 end sets a circle draw-in groove 8, facilitates clamping to install.
Above-described is only preferred implementation of the present utility model, it is noted that for ability
For the those of ordinary skill in territory, on the premise of creating design without departing from this utility model, also may be used
To make some deformation and improvement, these broadly fall into protection domain of the present utility model.
Claims (4)
1. airplane riveting machine encoder axle, its feature includes the encoder axle body being integrally cast
And connecting shaft (2), encoder axle body (1) and connecting shaft (2) junction set boss (1)
(3), encoder axle body (1) middle part sets fabrication hole (4), and connecting shaft (2) center is peace
Dress hole (5), encoder axle body (1) outside sets the fixing hole (6) that a circle is evenly distributed.
2. airplane riveting machine encoder axle as claimed in claim 1, is characterized in that described fixing
The quantity in hole (6) is 6.
3. airplane riveting machine encoder axle as claimed in claim 1, is characterized in that described boss
(3) side sets circle boss draw-in groove (7).
4. airplane riveting machine encoder axle as claimed in claim 1, is characterized in that described connection
Axle (2) end sets a circle draw-in groove (8).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620257431.0U CN205464152U (en) | 2016-03-30 | 2016-03-30 | Aircraft riveter encoder axle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620257431.0U CN205464152U (en) | 2016-03-30 | 2016-03-30 | Aircraft riveter encoder axle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205464152U true CN205464152U (en) | 2016-08-17 |
Family
ID=56647761
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620257431.0U Active CN205464152U (en) | 2016-03-30 | 2016-03-30 | Aircraft riveter encoder axle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205464152U (en) |
-
2016
- 2016-03-30 CN CN201620257431.0U patent/CN205464152U/en active Active
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| PE01 | Entry into force of the registration of the contract for pledge of patent right | ||
| PE01 | Entry into force of the registration of the contract for pledge of patent right |
Denomination of utility model: Encoder shaft of aircraft riveting machine Effective date of registration: 20200921 Granted publication date: 20160817 Pledgee: Jiangsu Yixing rural commercial bank Limited by Share Ltd. Branch Park Branch Pledgor: YIXING RONGXING CASTING Co.,Ltd. Registration number: Y2020990001143 |
|
| PC01 | Cancellation of the registration of the contract for pledge of patent right | ||
| PC01 | Cancellation of the registration of the contract for pledge of patent right |
Date of cancellation: 20210825 Granted publication date: 20160817 Pledgee: Jiangsu Yixing rural commercial bank Limited by Share Ltd. Branch Park Branch Pledgor: YIXING RONGXING CASTING Co.,Ltd. Registration number: Y2020990001143 |
|
| TR01 | Transfer of patent right | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20220516 Address after: 100000 courtyard 1, Chaoyang Road, Chaoyang District, Beijing Patentee after: AVIC BEIJING AERONAUTICAL MANUFACTURING TECHNOLOGY Research Institute Address before: 214200 Yixing Rongxing Foundry Co., Ltd., No. 15, Huixing North Road, Zhuqiao Economic Development Zone, Yixing City, Wuxi City, Jiangsu Province Patentee before: YIXING RONGXING CASTING CO.,LTD. |