CN106609802A - Anti-deformation thrusting force bearing seat - Google Patents
Anti-deformation thrusting force bearing seat Download PDFInfo
- Publication number
- CN106609802A CN106609802A CN201510726076.7A CN201510726076A CN106609802A CN 106609802 A CN106609802 A CN 106609802A CN 201510726076 A CN201510726076 A CN 201510726076A CN 106609802 A CN106609802 A CN 106609802A
- Authority
- CN
- China
- Prior art keywords
- heat dissipation
- thrusting force
- bearing
- reducing area
- dissipation weight
- 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.)
- Pending
Links
Abstract
The invention discloses an anti-deformation thrusting force bearing seat, which comprises a bearing base, a fixation block, a heat dissipation weight reducing area, a reinforcing rib and a thrusting force surface alloy liner, wherein the fixation block is fixed above the bearing base, the center of the fixation block is provided with a positioning hole, the thrusting force surface alloy liner is arranged on a bearing seat thrusting force surface and is fixedly connected to the thrusting force surface, the heat dissipation weight reducing area is arranged between the thrusting force surface alloy liner on the middle portion of the bearing seat and the bearing base and is hollow, and the reinforcing rib is arranged between the heat dissipation weight reducing area. According to the present invention, the heat dissipation weight reducing area is arranged on the middle portion of the traditional thrusting force bearing seat, and the Babbitt metal liner is arranged on the thrusting force surface, such that the stress in the bearing is effectively reduced, the internal heat dissipation function is enhance, the crack generation in the bearing is effectively prevented, the thrusting force surface is wear-resistant, and the service life is prolonged with the heat dissipation weight reducing area and the Babbitt metal liner.
Description
Technical field
The present invention relates to a kind of bearing block, the thrust metal on more particularly to a kind of ships.
Background technology
Ships thrust metal is installed in the core foundry goods in ships gear housing, bear compared with
Big moment of face.
Traditional thrust metal easily causes in use loss, causes inside bearing block
Abrasion, needs Jing often to carry out Bead weld repair, and built-up welding can make parts surface reach very high temperature
Degree, causes part distortion or cracks.
The content of the invention
The present invention provides a kind of durable wear-resistant, resistance to deformation, effectively prevents Bearing inner from producing
A kind of resistance to deformation thrust metal of wrinkle.
The technical solution used in the present invention is：
A kind of resistance to deformation thrust metal, including bearing base, fixed block, heat dissipation weight-reducing
Area, reinforcement, thrust face alloy inner bag, bearing base is fixedly arranged above fixed block, Gu
Ding Kuai centers are provided with location hole, and thrust face alloy inner bag is provided with bearing block thrust face,
Thrust face alloy inner bag is fixedly connected with thrust face, the thrust face alloy in the middle part of bearing block
Heat dissipation weight-reducing area is provided between inner bag and bearing base, heat dissipation weight-reducing area is hollow, is being dissipated
Reinforcement is provided between hot loss of weight area.
It is 300- that there are the distance between 4-10 area, each area in the heat dissipation weight-reducing area
600mm。
The reinforcement is 500mm.
The present invention sets heat dissipation weight-reducing area in the middle part of traditional thrust metal, in the thrust
Face sets babbit inner bag, by heat dissipation weight-reducing area, babbit inner bag, effectively reduces
Stress in bearing, strengthens the heat sinking function of inside, effectively prevents Bearing inner from producing
Crackle, thrust face is more wear-resisting, increases the service life.
Description of the drawings
Fig. 1 is the structural representation of the present invention.
Specific embodiment
Referring to Fig. 1, a kind of resistance to deformation thrust metal, including bearing base 1, fixed block
2nd, heat dissipation weight-reducing area 3, reinforcement 4, thrust face alloy inner bag 5.The top of bearing base 1
Fixed block 2 is fixed with, the center of fixed block 2 is provided with location hole.Thrust face is provided with thrust face
Alloy inner bag 5, thrust face alloy inner bag 5 is fixedly connected with thrust face.In the middle part of bearing block
Thrust face alloy inner bag 5 and bearing base 1 between be provided with heat dissipation weight-reducing area 3, radiating subtracts
For hollow, heat dissipation weight-reducing area 3 is 6 areas in weight area 3, and the distance between each area is
500mm.Reinforcement 4 is provided between heat dissipation weight-reducing area, the thickness of reinforcement 4 is 500mm.
Claims (3)
1. a kind of resistance to deformation thrust metal, including bearing base, fixed block,
Heat dissipation weight-reducing area, reinforcement, thrust face alloy inner bag, it is characterised in that：Bearing
Base is fixedly arranged above fixed block, and fixed block center is provided with location hole, in bearing block
Thrust face is provided with thrust face alloy inner bag, and thrust face alloy inner bag is consolidated with thrust face
Fixed connection, sets between the thrust face alloy inner bag and bearing base in the middle part of bearing block
There is heat dissipation weight-reducing area, heat dissipation weight-reducing area is hollow, is provided between heat dissipation weight-reducing area
Reinforcement.
2. a kind of resistance to deformation thrust metal according to claim 1, its
It is characterised by：There is 4-10 area in the heat dissipation weight-reducing area, between each area away from
From for 300-600mm.
3. a kind of resistance to deformation thrust axis according to claim 1 and 2
Bearing, its feature exists：The reinforcement is 500mm.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510726076.7A CN106609802A (en) | 2015-10-22 | 2015-10-22 | Anti-deformation thrusting force bearing seat |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510726076.7A CN106609802A (en) | 2015-10-22 | 2015-10-22 | Anti-deformation thrusting force bearing seat |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106609802A true CN106609802A (en) | 2017-05-03 |
Family
ID=58614333
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201510726076.7A Pending CN106609802A (en) | 2015-10-22 | 2015-10-22 | Anti-deformation thrusting force bearing seat |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106609802A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111483591A (en) * | 2020-04-24 | 2020-08-04 | 中国航发湖南动力机械研究所 | Tail speed reducer casing and heavy-load tail speed reducer |
| CN112218514A (en) * | 2020-10-23 | 2021-01-12 | 国信军创(岳阳)六九零六科技有限公司 | Processing device adopting inner floating ground design |
-
2015
- 2015-10-22 CN CN201510726076.7A patent/CN106609802A/en active Pending
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111483591A (en) * | 2020-04-24 | 2020-08-04 | 中国航发湖南动力机械研究所 | Tail speed reducer casing and heavy-load tail speed reducer |
| CN112218514A (en) * | 2020-10-23 | 2021-01-12 | 国信军创(岳阳)六九零六科技有限公司 | Processing device adopting inner floating ground design |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US10663023B2 (en) | Hybrid lightweight brake disk and production method | |
| KR20140129769A (en) | Composition Of Aluminum Alloy For Local Enforcement And, Aluminum Piston With Local Enforcement Layer Using The Same | |
| CN103946606B (en) | The cylinder jacket and its manufacturing method of the cylinder of internal combustion engine | |
| US20190310044A1 (en) | Metal-Metal-Matrix Composite Barrels | |
| CN106609802A (en) | Anti-deformation thrusting force bearing seat | |
| US7566504B2 (en) | Iron species preform | |
| JP5311918B2 (en) | Spring retainer and spring system | |
| EP3051158B1 (en) | Sliding member and method for producing sliding member | |
| US8261767B1 (en) | Powdered metal inlay | |
| CN113084457B (en) | Metallographic strengthening manufacturing method of piston | |
| CN207261483U (en) | A kind of resistance to deformation bearing block peculiar to vessel | |
| JP5796019B2 (en) | Barrel of clay gun equipment for metallurgical furnace | |
| CN204717206U (en) | A kind of outer overall, interior two points of double layer wear resistant and impact resistant bend pipes | |
| CN104747849A (en) | Double-layer type wear-and-shock-resisting elbow pipe with integral contour and bipartite interior | |
| CN205101413U (en) | Flagship thrust bearing foundation | |
| CN104075057A (en) | Bending pipe and manufacturing method thereof and concrete pumping device | |
| CN104411420A (en) | Method for producing a composite roll and composite roll produced thereby | |
| CN204647672U (en) | A kind of outer complete two points of double layer wear resistant and impact resistant bend pipes | |
| JP2007100122A (en) | Iron-base preform for forming metal matrix composite and journal part structure | |
| CN204717204U (en) | A kind of two points of double layer wear resistant and impact resistant bend pipes | |
| CN210068802U (en) | Automobile brake disc and vehicle | |
| CN203948850U (en) | Concrete pumping equipment and bend pipe thereof | |
| JP2011069372A (en) | Iron-base preform for forming metal matrix composite and journal part structure | |
| CN107420309B (en) | Piston for rotary compressor and preparation method thereof | |
| CN206458722U (en) | A kind of thrust block keep |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| WD01 | Invention patent application deemed withdrawn after publication | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20170503 |