CN205465857U - Aerial positioner - Google Patents
Aerial positioner Download PDFInfo
- Publication number
- CN205465857U CN205465857U CN201620286829.7U CN201620286829U CN205465857U CN 205465857 U CN205465857 U CN 205465857U CN 201620286829 U CN201620286829 U CN 201620286829U CN 205465857 U CN205465857 U CN 205465857U
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- Prior art keywords
- magnet
- external magnet
- assembly
- iii
- described external
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Abstract
The utility model relates to a mechanical device field is refered in particular to one kind and is used for strutting round aerial positioner with the flexible hose that length is very long through it. Mainly by the frame, the guide ring, the external magnet assembly, internal magnet assembly and terminal surface assembly constitute. The utility model discloses the design is novel, and is rational in infrastructure, easy and simple to handle, can not receive the length restriction to strut the circle to flexible hose.
Description
Technical field
This utility model relates to machinery field, refers in particular to a kind of for being strutted through it by flexible hose the longest for length
The aerial positioner held round.
Background technology
In production practices, it is often necessary to the flexible pipe of flattening deformation is strutted and holds round, but general instrument is due to limited length
The finite length of flexible pipe can only be applied to, also do not have effective device to complete this operation.
Summary of the invention
In order to solve the problems referred to above, this utility model provides a kind of aerial positioner.
This utility model be the technical scheme is that
Described aerial positioner is mainly made up of frame, guide ring, external magnet assembly, internal magnet assembly and end face assembly.
Described external magnet assembly is mainly made up of external magnet seat, external magnet I, external magnet II and external magnet III.Described internal magnet assembly master
Will be by internal magnet, mandrel and circular magnet are constituted.Described end face assembly is mainly made up of set shape Magnet and end face seat.Described mandrel
There are three uniform groove I and hole I.The external cylindrical surface of described set shape Magnet and the inner hole of described end face seat.Described circular magnetic
Ferrum coordinates with described hole I.Three blocks of identical described internal magnets described groove I uniform with the three of described mandrel coordinates.Outside described
Magnet I, described external magnet II, described external magnet III length equal, described external magnet I and the arc length phase of described external magnet II
Deng and arc length than described external magnet III long.Described external magnet I, described external magnet II, described external magnet III and described external magnet
After seat coordinates, described external magnet I, described external magnet II, the intrados of described external magnet III are cone, its tapering and three pieces
The extrados tapering of described internal magnet and the described mandrel rear three blocks of described internal magnets of cooperation is equal.
The beneficial effects of the utility model are:
This utility model is novel, rational in infrastructure, easy and simple to handle, can not be strutted flexible hose by length limitation and hold round.
Accompanying drawing explanation
Further illustrate below in conjunction with figure of the present utility model:
Fig. 1, Fig. 2 are structural representations of the present utility model.
Fig. 3 is the structural representation of described external magnet assembly.
Fig. 4 is the structural representation of described internal magnet assembly.
Fig. 5 is the structural representation of described end face assembly.
Fig. 6 is the structural representation of described mandrel.
In figure, 1. frame, 2. guide ring, 3. external magnet assembly, 4. internal magnet assembly, 5. end face assembly, 6. flexible pipe, 7.
Groove I, 8. hole I, 31. external magnet seats, 32. external magnet I, 33. external magnet II, 34. external magnet III, 41. internal magnets, 42.
Mandrel, 43. circular magnet, 51. set shape Magnet, 52. end face seats.
Detailed description of the invention
Described aerial positioner mainly by described frame (1), described guide ring (2), described external magnet assembly (3),
Described internal magnet assembly (4) and described end face assembly (5) are constituted.See Fig. 2.
Described external magnet assembly (3) is main by described external magnet seat (31), described external magnet I (32), described outer magnetic
Ferrum II (33) and described external magnet III (34) is constituted.See Fig. 3.
Described internal magnet assembly (4) mainly by three blocks of identical described internal magnets (41), described mandrel (42) and described
Circular magnet (43) is constituted.See Fig. 4.
Described end face assembly (5) is mainly made up of described set shape Magnet (51) and described end face seat (52).See Fig. 5.
Described mandrel (42) has three uniform described groove I (7) and described hole I (8).See Fig. 6.
The external cylindrical surface of described set shape Magnet (51) and the inner hole of described end face seat (52).Described circular magnet (43)
Coordinate with described hole I (8).Three pieces of described internal magnet (41) groove Is (7) described with three of described mandrel (42) coordinate.
Described external magnet I (32), described external magnet II (33), described external magnet III (34) length equal, described external magnet
The arc length of I (32) and described external magnet II (33) is equal and longer than the arc length of described external magnet III (34).Described external magnet
After I (32), described external magnet II (33), described external magnet III (34) coordinate with described external magnet seat (31), described
External magnet I (32), described external magnet II (33), the intrados of described external magnet III (34) be cone, its tapering with
Three described groove I (7) of three pieces of described internal magnets (41) and described mandrel (42) coordinate rear three pieces of described internal magnets (41)
Extrados tapering equal.
The external cylindrical surface magnetic of three pieces of described internal magnets (41) and described external magnet I (32), described external magnet II (33),
The inner cylinder face magnetic of described external magnet III (34) is identical.
The magnetic of the end face that described circular magnet (43) is corresponding with described set shape Magnet (51) is identical.
Owing to the arc length of described external magnet I (32) and described external magnet II (33) is equal and than described external magnet III (34)
Arc length long, therefore the action of gravity of described internal magnet assembly (4) can be offset, make described internal magnet assembly (4) be positioned at described outside
The endoporus center of magnetic assembly (3).
Three pieces of described internal magnets (41) respectively with described external magnet I (32), described external magnet II (33), described
Under the action of a magnetic field of external magnet III (34), under the described circular magnet (43) the action of a magnetic field with described set shape Magnet (51),
Under gravity, stress balance, described internal magnet assembly (4) is static, it is achieved position in the air.
During use, described flexible pipe (6) is under the guiding of described guide ring (2), constantly through described external magnet assembly (3),
Thus described flexible pipe (6) is progressively strutted and holds round.
Claims (1)
1. an aerial positioner, mainly by frame, guide ring, external magnet assembly, internal magnet assembly and end face assembly
Constitute；Described external magnet assembly is mainly made up of external magnet seat, external magnet I, external magnet II and external magnet III；Described internal magnet
Assembly is mainly made up of internal magnet, mandrel and circular magnet；Described end face assembly is mainly made up of set shape Magnet and end face seat；Its
Feature is: described mandrel has three uniform groove I and hole I；The external cylindrical surface of described set shape Magnet and the endoporus of described end face seat
Coordinate；Described circular magnet coordinates with described hole I；Described uniform with the three of described mandrel of three blocks of identical described internal magnets
Groove I coordinates；Described external magnet I, described external magnet II, described external magnet III length equal, described external magnet I and described
Equal and than described external magnet III the arc length of the arc length of external magnet II is long；Described external magnet I, described external magnet II, described outer magnetic
After ferrum III coordinates with described external magnet seat, described external magnet I, described external magnet II, the intrados of described external magnet III are circular cone
The extrados tapering of shape, its tapering and three blocks of described internal magnets and the described mandrel rear three blocks of described internal magnets of cooperation is equal.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620286829.7U CN205465857U (en) | 2016-03-31 | 2016-03-31 | Aerial positioner |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620286829.7U CN205465857U (en) | 2016-03-31 | 2016-03-31 | Aerial positioner |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205465857U true CN205465857U (en) | 2016-08-17 |
Family
ID=56643425
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620286829.7U Withdrawn - After Issue CN205465857U (en) | 2016-03-31 | 2016-03-31 | Aerial positioner |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205465857U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105666370A (en) * | 2016-03-31 | 2016-06-15 | 金华职业技术学院 | Aerial positioning device |
-
2016
- 2016-03-31 CN CN201620286829.7U patent/CN205465857U/en not_active Withdrawn - After Issue
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105666370A (en) * | 2016-03-31 | 2016-06-15 | 金华职业技术学院 | Aerial positioning device |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| AV01 | Patent right actively abandoned | ||
| AV01 | Patent right actively abandoned |
Granted publication date: 20160817 Effective date of abandoning: 20170929 |