CN210859441U - Nonmetal clamping hoop for aviation - Google Patents
Nonmetal clamping hoop for aviation Download PDFInfo
- Publication number
- CN210859441U CN210859441U CN201921214771.5U CN201921214771U CN210859441U CN 210859441 U CN210859441 U CN 210859441U CN 201921214771 U CN201921214771 U CN 201921214771U CN 210859441 U CN210859441 U CN 210859441U
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- CN
- China
- Prior art keywords
- clamp
- quick
- release bolt
- buckle
- release
- 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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- 229910052755 nonmetal Inorganic materials 0.000 title claims abstract description 12
- 230000006978 adaptation Effects 0.000 abstract description 2
- 239000000463 material Substances 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 239000004677 Nylon Substances 0.000 description 1
- 230000006835 compression Effects 0.000 description 1
- 238000007906 compression Methods 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 239000007769 metal material Substances 0.000 description 1
- 229920001778 nylon Polymers 0.000 description 1
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- Clamps And Clips (AREA)
Abstract
The utility model relates to a nonmetal clamp hoop is used in aviation for it is longer to solve current clamp assembly time, and the clamp takes place to warp cracked problem even. This nonmetal clamp hoop for aviation, including the clamp, the clamp is the flexible body, is provided with the mounting on the outer anchor ring of clamp, is provided with the rubber circle on the anchor ring in the clamp, and the side of an end of clamp is provided with the fillet, is provided with the quick-release bolt on the fillet, sets up a plurality of buckles on the anchor ring of another end of clamp, buckle and quick-release bolt looks adaptation.
Description
Technical Field
The utility model relates to a clamp, concretely relates to nonmetal clamp hoop is used in aviation.
Background
In the aviation field, all have very high requirement to the structural strength and the weight of clamp, current clamp is metal material generally, but its weight can not satisfy the demand usually when being applied to the aviation field.
And current clamp need use screw or self-locking nut fastening usually, and the time that needs during the assembly is longer, and the narrow and small operation degree of difficulty that leads to of aircraft inner space simultaneously is big, easily causes screw, nut to scatter, forms the redundancy, because the clamp dismouting is frequent simultaneously, easily leads to the clamp to warp even fracture.
SUMMERY OF THE UTILITY MODEL
The utility model aims at providing an aviation is with nonmetal clamp hoop to it is longer to solve current clamp assemble duration, and the clamp takes place to warp cracked problem even.
In order to achieve the above object, the technical solution of the present invention is:
the utility model provides an aviation is with nonmetal clamp which characterized in that: including the clamp, the clamp is the flexible body, is provided with the mounting on the outer anchor ring of clamp, is provided with the rubber circle in the clamp on the anchor ring, and the side of an end of clamp is provided with the fillet, is provided with quick-release bolt on the fillet, sets up a plurality of buckles on the anchor ring of another end of clamp, buckle and quick-release bolt looks adaptation.
Preferably, one end of the fixing piece is fixed on the outer ring surface of the clamp, and the other end of the fixing piece is provided with two mounting holes.
Preferably, the width of the angle piece is the same as that of the clamp, the angle piece protrudes out of the outer ring surface of the clamp, and after the buckle and the quick-release bolt are assembled, the ring surfaces of two ends of the clamp are flush.
Preferably, one end of the quick-release bolt is a hexagonal square head, a straight groove is formed in the end face of the quick-release bolt, the other end of the quick-release bolt sequentially penetrates through the gasket, the spring and the corner piece, and a pin shaft perpendicular to the axis of the quick-release bolt is arranged at the end of the quick-release bolt.
Preferably, the buckle is provided with a strip hole, the center of the strip hole is provided with a through hole matched with the diameter of the quick-release bolt, the lower surface of the buckle is provided with a groove perpendicular to the symmetrical line of the strip hole, and the groove is matched with the pin shaft.
Preferably, the buckle is embedded in the ring surface of the hoop, and the lower surface of the buckle keeps a gap with the rubber ring.
Preferably, a quick-release clamping belt is sleeved on the ring body of the clamp.
The utility model has the advantages that:
1. the utility model discloses aviation nonmetal clamping clamp fixes through the mode of quick-release, has shortened assembly time greatly; the clamp adopts an integrated structure, and no redundant situation exists during assembly; the buckle through different positions can fix the part of not unidimensional for this clamp range of application is wide, and has promoted staff's assembly efficiency greatly.
2. The clamp adopts flexible body material, can not take place the condition of deformation, fracture at the in-process of buckling, dismouting repeatedly, has promoted the reliability of clamp.
3. The quick-release clamp belt can fix the ends of the clamp, and one end is prevented from being in a natural disengagement state after the clamp is fixed.
Drawings
FIG. 1 is a schematic view of the structure of the aviation nonmetal clamping hoop of the present invention;
FIG. 2 is a schematic view of the construction of the quick release bolt mounted on the corner piece;
FIG. 3 is a schematic structural view of the clamp after locking the two ends;
FIG. 4 is a top view of the buckle;
FIG. 5 is a bottom view of the buckle;
FIG. 6 is a cross-sectional view of the snap-fit mounting to the clip.
The reference numbers are as follows:
1-clamp, 2-fixing piece, 3-rubber ring, 4-angle piece, 5-quick-release bolt, 6-buckle, 7-gasket, 8-spring, 9-pin shaft, 10-quick-release clamping belt and 11-groove.
Detailed Description
The invention is described in further detail below with reference to the following figures and specific examples:
as shown in fig. 1 to 6, the aviation nonmetal clamping hoop comprises a hoop 1, a fixing piece 2, a rubber ring 3, a quick-release bolt 5, a buckle 6 and a quick-release clamping band 10.
The clamp 1 is a flexible body and is made of nylon materials; the clamp 1 is in a natural state, and two ends of the clamp can be in a state of being side by side and contacting with each other, as shown in fig. 3.
As shown in fig. 1, the fixing member 2 has one end fixed to the outer circumferential surface of the yoke 1 and the other end provided with two mounting holes. The fixing member 2 is used to fix the clip 1 at a set position.
The inner ring surface of the clamp 1 is provided with a rubber ring 3, the rubber ring 3 is in contact with a part to be fixed, and the rubber ring 3 can protect the surface of the part to be fixed from being scratched by the clamp 1 body.
A plurality of buckles 6 are arranged on the ring surface of one end of the hoop 1, and the buckles 6 are matched with the quick-release bolts 5.
As shown in figure 2, a corner piece 4 with the same width as the clamp 1 is arranged on the side face of the other end of the clamp 1, a quick-release bolt 5 is arranged on the corner piece 4, the corner piece 4 protrudes out of the outer ring face of the clamp 1, and after the buckle 6 is assembled with the quick-release bolt 5, the ring faces of the two ends of the clamp 1 are flush.
As shown in fig. 2 and 3, one end of the quick-release bolt 5 is a hexagonal square head, and a straight groove is formed in the end surface of the quick-release bolt, so that a worker can apply force to the quick-release bolt 5 to twist the quick-release bolt, and the quick-release bolt 5 is assembled on the buckle 6.
The other end of the quick-release bolt 5 sequentially penetrates through the gasket 7, the spring 8 and the angle piece 4, and the end of the quick-release bolt is provided with a pin shaft 9 perpendicular to the axis of the quick-release bolt 5. The spring 8 can keep the quick-release bolt 5 in an axial compression state, so that the quick-release bolt 5 is prevented from being disengaged from the buckle 6.
As shown in fig. 4, the buckle 6 is provided with a long hole, and the center of the long hole is provided with a through hole matched with the diameter of the quick-release bolt 5;
as shown in fig. 5, the lower surface of the buckle 6 is provided with a groove 11 perpendicular to the symmetry line of the strip hole, and the groove 11 is matched with the pin shaft 9.
As shown in fig. 1 and 6, the buckle 6 is embedded in the ring surface of the clamp 1, and the lower surface of the buckle 6 keeps a space with the rubber ring 3, wherein the space can facilitate the pin shaft 9 of the quick-release bolt 5 to rotate and turn into the groove 11.
The quick-release clamping band 10 is sleeved on the ring body of the clamp 1, the quick-release clamping band 10 can move on the ring body of the clamp 1, and two ends of the quick-release clamping band 10 are detachably connected. The quick-release clamp belt 10 can fix the ends of the clamp 1, and avoids the situation that one end is in a natural disengagement state after the clamp 1 is fixed.
The utility model discloses a nonmetal clamp hoop application method for aviation:
installing the clamp 1 to a set position through a fixing piece 2;
placing the part to be fixed into the hoop 1;
placing the corner piece 4 over the snap 6 in place;
moving the quick-release clamp belt 10 to one end of the clamp 1;
the quick-release bolt 5 is rotated and pressed, the end of the quick-release bolt 5 penetrates through the strip-shaped hole of the buckle 6, and the quick-release bolt 5 is rotated again to enable the pin shaft 9 on the quick-release bolt to be positioned in the groove 11;
and finely adjusting the position of the quick-release clamp belt 10, fixing the two ends of the clamp 1 and further fixing the clamp 1 to the component.
The above is only the embodiment of the present invention, and is not the limitation of the protection scope of the present invention, all the equivalent structure changes made in the contents of the specification and the drawings, or the direct or indirect application in other related technical fields are included in the patent protection scope of the present invention.
Claims (7)
1. The utility model provides an aviation is with nonmetal clamp, its characterized in that: the clamp comprises a clamp (1), wherein the clamp (1) is a flexible body, a fixing part (2) is arranged on the outer annular surface of the clamp (1), a rubber ring (3) is arranged on the inner annular surface of the clamp (1), a corner piece (4) is arranged on the side surface of one end of the clamp (1), a quick-release bolt (5) is arranged on the corner piece (4), a plurality of buckles (6) are arranged on the annular surface of the other end of the clamp (1), and the buckles (6) are matched with the quick-release bolt (5).
2. The non-metallic aerospace clamp clip of claim 1, wherein: one end of the fixing piece (2) is fixed on the outer ring surface of the hoop (1), and the other end of the fixing piece is provided with two mounting holes.
3. The non-metallic aerospace clamp clip of claim 2, wherein: the width of the angle piece (4) is the same as that of the clamp (1), the angle piece (4) protrudes out of the outer ring surface of the clamp (1), and after the buckle (6) and the quick-release bolt (5) are assembled, the ring surfaces of two ends of the clamp (1) are flush.
4. The non-metallic aerospace clamp clip of claim 3, wherein: one end of the quick-release bolt (5) is a hexagonal square head, a straight groove is formed in the end face of the quick-release bolt, the other end of the quick-release bolt (5) sequentially penetrates through the gasket (7), the spring (8) and the corner piece (4), and a pin shaft (9) perpendicular to the axis of the quick-release bolt (5) is arranged at the end of the quick-release bolt.
5. The non-metallic aerospace clamp clip of claim 4, wherein: the quick-release bolt is characterized in that a strip hole is formed in the buckle (6), a through hole matched with the diameter of the quick-release bolt (5) is formed in the center of the strip hole, a groove (11) perpendicular to the symmetrical line of the strip hole is formed in the lower surface of the buckle (6), and the groove (11) is matched with the pin shaft (9).
6. The non-metallic aerospace clamp clip of claim 5, wherein: the buckle (6) is embedded in the ring surface of the hoop (1), and the lower surface of the buckle (6) keeps a gap with the rubber ring (3).
7. The non-metallic aerospace clamp clip of claim 6, wherein: the ring body of the hoop (1) is sleeved with a quick-release clamping band (10).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921214771.5U CN210859441U (en) | 2019-07-30 | 2019-07-30 | Nonmetal clamping hoop for aviation |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921214771.5U CN210859441U (en) | 2019-07-30 | 2019-07-30 | Nonmetal clamping hoop for aviation |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN210859441U true CN210859441U (en) | 2020-06-26 |
Family
ID=71285979
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201921214771.5U Active CN210859441U (en) | 2019-07-30 | 2019-07-30 | Nonmetal clamping hoop for aviation |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN210859441U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114059528A (en) * | 2021-12-23 | 2022-02-18 | 平高集团有限公司 | A kind of protective tube for excavation foundation |
-
2019
- 2019-07-30 CN CN201921214771.5U patent/CN210859441U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114059528A (en) * | 2021-12-23 | 2022-02-18 | 平高集团有限公司 | A kind of protective tube for excavation foundation |
| CN114059528B (en) * | 2021-12-23 | 2025-09-12 | 平高集团有限公司 | A protective tube for excavating foundation |
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| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant |