CN103133805A - Fast-dismantled clamp structure - Google Patents
Fast-dismantled clamp structure Download PDFInfo
- Publication number
- CN103133805A CN103133805A CN2011103773351A CN201110377335A CN103133805A CN 103133805 A CN103133805 A CN 103133805A CN 2011103773351 A CN2011103773351 A CN 2011103773351A CN 201110377335 A CN201110377335 A CN 201110377335A CN 103133805 A CN103133805 A CN 103133805A
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- CN
- China
- Prior art keywords
- connecting rod
- snap ring
- pad
- quick release
- nut
- 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 invention provides a fast-dismantled clamp structure which is characterized by comprising a lower clamp ring, an upper clamp ring, a connecting rod, an elastic gasket, a connecting rod, a saddle-shaped pad, a first hinge pin, a dowel, a second hinge pin, a gasket and a nut. The connecting rod is connected with the lower clamp ring and the upper clamp ring through the first hinge pin. The elastic gasket is connected with the gasket and the upper clamp ring through the second hinge pin. The dowel is installed on the lower clamp ring. The saddle-shaped gasket is arranged between the connecting rod and the elastic gasket. The nut is installed on the connecting rod. No parts are loose. The fast-dismantled clamp structure has the advantages of being simple, practical and reliable in structure, and being widely applied to pipeline connection of aviation, spaceflight and civil products. Moreover, the fast-dismantled clamp structure can ensure that the upper clamp ring and the lower clamp ring can be opened freely during installation, and therefore installation operation becomes easy. Simultaneously, the clamp structure is compact, the loose parts are avoided, and a probability of falling off of the parts during installation can be effectively reduced.
Description
Technical field
The present invention relates to mechanical structure field, particularly a kind of Quick Release Hoop structure.
Background technique
The aeroengine installation and maintenance require more and more higher, require installation time shorter and shorter, and this just requires the installation of connected element to want succinct, fast, and without loose parts, prevents that accident drops in installation process.For this reason, need a kind of quick-release structure of design, to realize the quick mounting requirement.
Traditional yoke configurations, generally be divided into a plurality of loose parts such as the first half, Lower Half, bolt, locking plate and form, such structure is relatively loaded down with trivial details in installation process, and limited by installing space, than being easier to occur the situation that part drops, cause work to be incured loss through delay.
For this reason, design a kind of Quick Release Hoop structure, on clip, all parts link together, and the clip two halves are split along bearing pin, make the installation behavior more convenient, quick, thereby realize saving the purpose of installation time.
Summary of the invention
The objective of the invention is provides a kind of Quick Release Hoop structure especially in order to make the installation behavior more convenient, quick.
The invention provides a kind of Quick Release Hoop structure, it is characterized in that: described Quick Release Hoop structure comprises lower snap ring 1, upper snap ring 2, connecting rod 3, resilient pad 4, connecting rod 5, saddle type pad 6, bearing pin 1, pin 8, bearing pin 29, pad 10, nut 11;
Wherein: connecting rod 3 connects lower snap ring 1 and upper snap ring 2 by bearing pin 1, resilient pad 4 is connected with pad by bearing pin 29 and is connected with upper snap ring 2, pin 8 is arranged on lower snap ring 1, saddle type pad 6 pads are between connecting rod 5 and resilient pad 4, nut 11 is arranged on connecting rod 5, and is whole without loose parts.
The material of described resilient pad 4 is sheet material or the band of GH624, and when guaranteeing open lathe dog, resilient pad 4 can be out of shape and streaks pin 8.
Described connecting rod 3 is thick plate structure, or the thin plate multi-layer structure, and material is the GH625 material.
Screw thread on described connecting rod 5 can adopt metric thread, or inch screw thread, and when selecting inch screw thread, nut 11 is the nut with self-locking structure.
Advantage of the present invention:
Quick Release Hoop structure of the present invention, simple and practical, reliable in structure can be extensively practical in Aeronautics and Astronautics and the connection of product for civilian use pipeline.
Description of drawings
Fig. 1 is the Quick Release Hoop structure, the installation process schematic diagram;
Fig. 2 is the Quick Release Hoop structure, the mounted configuration schematic diagram;
Fig. 3 is that the Quick Release Hoop structure is overlooked the direction schematic diagram.
Embodiment
The present embodiment provides a kind of Quick Release Hoop structure, it is characterized in that: described Quick Release Hoop structure comprises lower snap ring 1, upper snap ring 2, connecting rod 3, resilient pad 4, connecting rod 5, saddle type pad 6, bearing pin 1, pin 8, bearing pin 29, pad 10, nut 11;
Wherein: connecting rod 3 connects lower snap ring 1 and upper snap ring 2 by bearing pin 1, resilient pad 4 is connected with pad by bearing pin 29 and is connected with upper snap ring 2, pin 8 is arranged on lower snap ring 1, saddle type pad 6 pads are between connecting rod 5 and resilient pad 4, nut 11 is arranged on connecting rod 5, and is whole without loose parts.
The material of described resilient pad 4 is the sheet material of GH624, and when guaranteeing open lathe dog, resilient pad 4 can be out of shape and streaks pin 8.
Described connecting rod 3 is thick plate structure, and material is the GH625 material.
Screw thread on described connecting rod 5 adopts metric thread.
The present embodiment provides a kind of Quick Release Hoop structure, it is characterized in that: described Quick Release Hoop structure comprises lower snap ring 1, upper snap ring 2, connecting rod 3, resilient pad 4, connecting rod 5, saddle type pad 6, bearing pin 1, pin 8, bearing pin 29, pad 10, nut 11;
Wherein: connecting rod 3 connects lower snap ring 1 and upper snap ring 2 by bearing pin 1, resilient pad 4 is connected with pad by bearing pin 29 and is connected with upper snap ring 2, pin 8 is arranged on lower snap ring 1, saddle type pad 6 pads are between connecting rod 5 and resilient pad 4, nut 11 is arranged on connecting rod 5, and is whole without loose parts.
The material of described resilient pad 4 is the band of GH624, and when guaranteeing open lathe dog, resilient pad 4 can be out of shape and streaks pin 8.
Described connecting rod 3 is the thin plate multi-layer structure, and material is the GH625 material.
Screw thread on described connecting rod 5 adopts inch screw thread, and nut 11 is the nut with self-locking structure.
Claims (5)
1. Quick Release Hoop structure, it is characterized in that: described Quick Release Hoop structure comprises lower snap ring (1), upper snap ring (2), connecting rod (3), resilient pad (4), connecting rod (5), saddle type pad (6), bearing pin one (7), pin (8), bearing pin two (9), pad (10), nut (11);
Wherein: connecting rod (3) connects lower snap ring (1) and upper snap ring (2) by bearing pin one (7), resilient pad (4) is connected 10 by bearing pin two (9) with pad) be connected with upper snap ring (2), pin (8) is arranged on lower snap ring (1), saddle type pad (6) pad is between connecting rod (5) and resilient pad (4), nut (11) is arranged on connecting rod (5), and is whole without loose parts.
2. according to Quick Release Hoop structure claimed in claim 1, it is characterized in that: lower snap ring (1), upper snap ring (2) can open around bearing pin one (7) rotation.
3. according to Quick Release Hoop structure claimed in claim 1, it is characterized in that: the material of described resilient pad (4) is sheet material or the band of GH624.
4. according to Quick Release Hoop structure claimed in claim 1, it is characterized in that: described connecting rod (3) is thick plate structure, or the thin plate multi-layer structure, and material is the GH625 material.
5. according to Quick Release Hoop structure claimed in claim 1, it is characterized in that: the screw thread on described connecting rod (5), can adopt metric thread, or inch screw thread, when selecting inch screw thread, nut (11) is the nut with self-locking structure.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201110377335.1A CN103133805B (en) | 2011-11-24 | 2011-11-24 | A kind of Quick Release Hoop structure |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201110377335.1A CN103133805B (en) | 2011-11-24 | 2011-11-24 | A kind of Quick Release Hoop structure |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN103133805A true CN103133805A (en) | 2013-06-05 |
| CN103133805B CN103133805B (en) | 2015-09-30 |
Family
ID=48494017
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201110377335.1A Expired - Fee Related CN103133805B (en) | 2011-11-24 | 2011-11-24 | A kind of Quick Release Hoop structure |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN103133805B (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104757782A (en) * | 2015-04-06 | 2015-07-08 | 马党 | Bed table and bed |
| CN104806445A (en) * | 2015-05-13 | 2015-07-29 | 中国科学院工程热物理研究所 | Connecting method of blade and bracket for H-shaped vertical-shaft wind turbine |
| CN107448702A (en) * | 2017-09-29 | 2017-12-08 | 大连长之琳科技发展有限公司 | The cold pipeline of liquid is rigidly connected Quick Release Hoop |
| CN112813569A (en) * | 2020-12-31 | 2021-05-18 | 厦门郑萌迈纺织有限公司 | Shuttle sliding track for loom |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN2158019Y (en) * | 1993-05-28 | 1994-03-02 | 王献 | Fluid pipe coupling |
| CN2833299Y (en) * | 2005-05-12 | 2006-11-01 | 日扬科技股份有限公司 | Pipe clamp |
| CN201891974U (en) * | 2010-11-04 | 2011-07-06 | 上海易玺电子科技有限公司 | Vacuum sealing clamp |
| CN202708423U (en) * | 2011-11-24 | 2013-01-30 | 中国航空工业集团公司沈阳发动机设计研究所 | Clamp structure capable of being dismantled quickly |
-
2011
- 2011-11-24 CN CN201110377335.1A patent/CN103133805B/en not_active Expired - Fee Related
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN2158019Y (en) * | 1993-05-28 | 1994-03-02 | 王献 | Fluid pipe coupling |
| CN2833299Y (en) * | 2005-05-12 | 2006-11-01 | 日扬科技股份有限公司 | Pipe clamp |
| CN201891974U (en) * | 2010-11-04 | 2011-07-06 | 上海易玺电子科技有限公司 | Vacuum sealing clamp |
| CN202708423U (en) * | 2011-11-24 | 2013-01-30 | 中国航空工业集团公司沈阳发动机设计研究所 | Clamp structure capable of being dismantled quickly |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104757782A (en) * | 2015-04-06 | 2015-07-08 | 马党 | Bed table and bed |
| CN104806445A (en) * | 2015-05-13 | 2015-07-29 | 中国科学院工程热物理研究所 | Connecting method of blade and bracket for H-shaped vertical-shaft wind turbine |
| CN107448702A (en) * | 2017-09-29 | 2017-12-08 | 大连长之琳科技发展有限公司 | The cold pipeline of liquid is rigidly connected Quick Release Hoop |
| CN112813569A (en) * | 2020-12-31 | 2021-05-18 | 厦门郑萌迈纺织有限公司 | Shuttle sliding track for loom |
Also Published As
| Publication number | Publication date |
|---|---|
| CN103133805B (en) | 2015-09-30 |
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| PB01 | Publication | ||
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| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20150930 Termination date: 20161124 |
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| CF01 | Termination of patent right due to non-payment of annual fee |