CN208203793U - The dedicated centreless miniature bearing of pneumatic turbine - Google Patents
The dedicated centreless miniature bearing of pneumatic turbine Download PDFInfo
- Publication number
- CN208203793U CN208203793U CN201721855576.1U CN201721855576U CN208203793U CN 208203793 U CN208203793 U CN 208203793U CN 201721855576 U CN201721855576 U CN 201721855576U CN 208203793 U CN208203793 U CN 208203793U
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- CN
- China
- Prior art keywords
- outer ring
- centreless
- ball
- dedicated
- bearing
- 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.)
- Expired - Fee Related
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Abstract
The dedicated centreless miniature bearing of pneumatic turbine, including flange outer ring, flange outer ring side is equipped with confined planes, flange outer ring inner wall is equipped with raceway, ball retainer and ball, the raceway is the circular arc to a side opening, and the ball is arranged in the retainer, and the retainer unilateral side is evenly equipped with the ball limiting slot for setting ball.Bearing directlys adopt centreless design and greatly reduces production cost.The utility model greatly reduces the cost of bearing, to reduce the cost of pneumatic turbine;Air-flow during operation is avoided to take away greasing substance to influence bearing service life;It is easy for installation while reducing noise that O-ring is arranged using the design of flange outer ring;Reduce the diameter jump during bearing operation.
Description
Technical field
The utility model relates to the bearings of pneumatic turbine, especially centreless bearing.
Background technique
Pneumatic turbine internal pressure is big, is easy in long-term operation process by internal lubrication using current existing bearing
Substance washes out, and reduces bearing service life.Pneumatic turbine special bearing production difficulty small in size is big, and assembling is inconvenient, at high cost,
Close-fitting is needed to install during the installation process, it is abnormal that tiny deviation will cause bearing rotation;In pneumatic turbine operation process
The internal unavoidable air-flow that has is excessive, and bearing faces air-flow directly to currently used bearing when in use, thus will lead to lubrication
Substance is directly brought away from, into oral cavity.
On the other hand, pneumatic turbine production cost is high, wherein it is excessively high to be primarily due to bearing cost, using quality
The bearing of difference is easy to wear during rotation, and revolving speed is not high, using causing high effort for.In addition at present outside independent bearing inner race
The production of circle needs to polish raceway in the middle part of bearing outer ring inner wall and in the middle part of interior ring outer wall, and required precision is high, and bistrique needs
Often replacement, significantly increases production cost.
Summary of the invention
In order to overcome the shortcomings of that existing pneumatic turbine bearing volume your pupil production difficulty is big, the utility model provides one kind
The dedicated centreless miniature bearing of pneumatic turbine.
The technical scheme in the invention for solving the technical problem is: the dedicated centreless miniature bearing of pneumatic turbine, including
Flange outer ring, flange outer ring side are equipped with confined planes, and flange outer ring inner wall is equipped with raceway, ball retainer and rolling
Pearl, the raceway are the circular arc to a side opening, and the ball is arranged in the retainer, and the retainer unilateral side is evenly equipped with
For setting the ball limiting slot of ball.Bearing directlys adopt centreless design and greatly reduces production cost.
Preferably, further including that lid is located at the flange outer ring other side for limiting the ring washer of ball.It is solid using retaining ring
Determine ball, lid is located at bearing side, prevent gas shock directly impact in bearing to take away greasing substance.
Preferably, side through hole edge is equipped with flange collar in the retaining ring, the flange collar section is triangular in shape, side wall and through-hole
Inner wall is consistent, and angle is formed between flange collar and retaining ring, plays certain guiding function to air-flow, prevents the direct contact bearing rolling of air-flow
Pearl prevents greasing substance to be entrained by the flow of air.
Preferably, the raceway outer is equipped with chamfering, the raceway outer after the retaining ring lid is located on flange outer ring
Chamfering and retaining ring form the angle gap being detained for lubricating fluid.
Preferably, being equipped with the chimb for setting up O-ring on the outside of the flange outer ring, the chimb is with side angle
It is arc-shaped.Chimb and the arc-shaped angle in side can be convenient O-ring setting on the outside of flange outer ring, greatly facilitate in bearing group
The control of dress process intermediate gap.
Preferably, improving ball degree of lubrication, ball limiting slot side offers oil storage tank on the retainer.
Preferably, being equipped with the holding tank for accommodating retainer on the inside of the flange outer ring.
Preferably, the retaining ring outer extends the convex edge being equipped with for wrapping up bearing.
Preferably, the flange outer ring is made of outer ring and housing, the raceway is arranged in the outer ring inner wall, institute
Stating coat part includes confined planes, is wrapped in outer ring sidewall sections and chimb.
Further, the retaining ring face ball is equipped with groove, and the groove is arranged concentrically with retaining ring.The groove also can be used
Greasing substance is received in storage.
Can be set up directly on shell when in use also can be by O-ring sandwiched inside the shell, then only need to be by pneumatic whirlpool
Taking turns bearings at both ends insertion middle part can be used.
The utility model has the beneficial effects that: 1: the cost of bearing is greatly reduced, to reduce air impeller
The cost of machine;2: avoiding air-flow during operation and take away greasing substance to influence bearing service life;3: using method
It is easy for installation while reducing noise that the design of blue outer ring is arranged O-ring;Reduce the diameter jump during bearing operation.
Detailed description of the invention
Fig. 1 is the utility model perspective view.
Fig. 2 is the utility model explosive view.
Fig. 3 is one structural schematic diagram of the utility model embodiment.
Fig. 4 is two structural schematic diagram of the utility model embodiment.
Fig. 5 is three structural schematic diagram of the utility model embodiment.
Specific embodiment
The utility model is described in further detail with reference to the accompanying drawings and detailed description.
Embodiment one: as shown in Figure 1, 2, 3: the dedicated centreless miniature bearing of pneumatic turbine, including flange outer ring 1, it is described
1 side of flange outer ring is equipped with confined planes 2, and 1 inner wall of flange outer ring is equipped with raceway 3, ball retainer 4 and ball 5, described
Raceway 3 is the circular arc to a side opening, and the ball 5 is arranged in the retainer 4, and the retainer 4 is unilateral uniformly distributed useful
In the ball limiting slot 6 for setting ball 5.Bearing directlys adopt centreless design and greatly reduces production cost.
It further include that lid is located at 1 other side of flange outer ring for limiting the ring washer 7 of ball in the present embodiment.Using gear
The fixed balls 5 of circle 7, lid are located at bearing side, prevent gas shock directly impact in bearing to take away greasing substance.
In the present embodiment, in the retaining ring 7 side through hole edge be equipped with flange collar 8, the flange collar section is triangular in shape, side wall with
Through-hole wall is consistent, and angle 9 is formed between flange collar 8 and retaining ring 7, plays certain guiding function to air-flow, prevents air-flow from directly contacting
Bearing ball prevents greasing substance to be entrained by the flow of air.
In the present embodiment, 3 outer of raceway is equipped with chamfering 10, the rolling after the lid of retaining ring 7 is located on flange outer ring
Road outer chamfering and retaining ring form the angle gap 11 being detained for lubricating fluid.
The chimb 12 for setting up O-ring, the chimb 12 and side are equipped in the present embodiment, on the outside of the flange outer ring 1
Face angle is arc-shaped.1 outside chimb of flange outer ring and the arc-shaped angle in side can be convenient the setting of O-ring 16, greatly side
Bearing assembling during gap control.
In the present embodiment, ball degree of lubrication is improved, ball limiting slot side offers oil storage tank 13 on the retainer.
The holding tank 14 for accommodating retainer is equipped in the present embodiment, on the inside of the flange outer ring 1.
In the present embodiment, the 7 face ball 5 of retaining ring is equipped with groove 15, and the groove is arranged concentrically with retaining ring.It is described recessed
Slot 15, which also can be used for storing up, receives greasing substance.
Embodiment two: as shown in Figure 4: the present embodiment other schemes and embodiment one or embodiment two in addition to flange outer ring
Identical, in the present embodiment, the flange outer ring is made of outer ring 17 and housing 18, and the raceway 3 is arranged in the outer ring
Wall, the coat part include confined planes 2, are wrapped in outer ring sidewall sections and chimb.
Embodiment three: as shown in Figure 5: the present embodiment other schemes in addition to retaining ring are identical as embodiment two, in the present embodiment,
The retaining ring outer extends the convex edge 19 being equipped with for wrapping up bearing.
Claims (10)
1. the dedicated centreless miniature bearing of pneumatic turbine, it is characterised in that: including flange outer ring, flange outer ring side is equipped with
Confined planes, flange outer ring inner wall are equipped with raceway, ball retainer and ball, and the raceway is the circle to a side opening
Arc, the ball are arranged in the retainer, and the retainer unilateral side is evenly equipped with the ball limiting slot for setting ball.
2. the dedicated centreless miniature bearing of pneumatic turbine as described in claim 1, it is characterised in that: further include described in lid is located at
The flange outer ring other side is used to limit the retaining ring of ball.
3. the dedicated centreless miniature bearing of pneumatic turbine as claimed in claim 2, it is characterised in that: side through hole in the retaining ring
Edge is equipped with flange collar.
4. the dedicated centreless miniature bearing of pneumatic turbine as claimed in claim 3, it is characterised in that: the raceway outer is equipped with
Chamfering, raceway outer chamfering and retaining ring form the angle being detained for lubricating fluid after the retaining ring lid is located on flange outer ring
Gap.
5. the dedicated centreless miniature bearing of pneumatic turbine as described in claim 1, it is characterised in that: on the outside of the flange outer ring
Equipped with the chimb for setting up O-ring.
6. the dedicated centreless miniature bearing of pneumatic turbine as described in claim 1, it is characterised in that: ball on the retainer
Limiting slot side offers oil storage tank.
7. the dedicated centreless miniature bearing of pneumatic turbine as described in claim 1, it is characterised in that: on the inside of the flange outer ring
Equipped with the holding tank for accommodating retainer.
8. the dedicated centreless miniature bearing of pneumatic turbine as claimed in claim 3, it is characterised in that: the retaining ring outer extends
Equipped with the convex edge for wrapping up bearing.
9. the dedicated centreless miniature bearing of pneumatic turbine as described in claim 1, it is characterised in that: the flange outer ring is by outer
Circle and housing composition, the raceway are arranged in the outer ring inner wall, and the coat part includes confined planes, is wrapped in outer ring side
Wall part and chimb.
10. the dedicated centreless miniature bearing of pneumatic turbine as claimed in claim 2, it is characterised in that: retaining ring face whirlpool
Wheel face is equipped with groove, and the groove is arranged concentrically with retaining ring.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201721855576.1U CN208203793U (en) | 2017-12-27 | 2017-12-27 | The dedicated centreless miniature bearing of pneumatic turbine |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201721855576.1U CN208203793U (en) | 2017-12-27 | 2017-12-27 | The dedicated centreless miniature bearing of pneumatic turbine |
Publications (1)
Publication Number | Publication Date |
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CN208203793U true CN208203793U (en) | 2018-12-07 |
Family
ID=64490786
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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CN201721855576.1U Expired - Fee Related CN208203793U (en) | 2017-12-27 | 2017-12-27 | The dedicated centreless miniature bearing of pneumatic turbine |
Country Status (1)
Country | Link |
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CN (1) | CN208203793U (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN108035970A (en) * | 2017-12-27 | 2018-05-15 | 浙江益齿星医疗器械有限公司 | The special centreless miniature bearing of pneumatic turbine |
-
2017
- 2017-12-27 CN CN201721855576.1U patent/CN208203793U/en not_active Expired - Fee Related
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN108035970A (en) * | 2017-12-27 | 2018-05-15 | 浙江益齿星医疗器械有限公司 | The special centreless miniature bearing of pneumatic turbine |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
GR01 | Patent grant | ||
GR01 | Patent grant | ||
CF01 | Termination of patent right due to non-payment of annual fee | ||
CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20181207 Termination date: 20191227 |