CN110406146A - A kind of new type of cam drive-type multiple position press flywheel support construction - Google Patents
A kind of new type of cam drive-type multiple position press flywheel support construction Download PDFInfo
- Publication number
- CN110406146A CN110406146A CN201910810852.XA CN201910810852A CN110406146A CN 110406146 A CN110406146 A CN 110406146A CN 201910810852 A CN201910810852 A CN 201910810852A CN 110406146 A CN110406146 A CN 110406146A
- Authority
- CN
- China
- Prior art keywords
- flywheel
- fuselage
- unloading sleeve
- clutch
- multiple position
- 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
- 238000010276 construction Methods 0.000 title claims abstract description 14
- 238000010586 diagram Methods 0.000 description 2
- 230000005484 gravity Effects 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000012797 qualification Methods 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B30—PRESSES
- B30B—PRESSES IN GENERAL
- B30B1/00—Presses, using a press ram, characterised by the features of the drive therefor, pressure being transmitted directly, or through simple thrust or tension members only, to the press ram or platen
- B30B1/26—Presses, using a press ram, characterised by the features of the drive therefor, pressure being transmitted directly, or through simple thrust or tension members only, to the press ram or platen by cams, eccentrics, or cranks
- B30B1/261—Presses, using a press ram, characterised by the features of the drive therefor, pressure being transmitted directly, or through simple thrust or tension members only, to the press ram or platen by cams, eccentrics, or cranks by cams
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Press Drives And Press Lines (AREA)
Abstract
A kind of new type of cam drive-type multiple position press flywheel support construction.It is related to press machine more particularly to a kind of new type of cam drive-type multiple position press flywheel support construction.It provides that a kind of structure is simple, improves the new type of cam drive-type multiple position press flywheel support construction of stability and service life.Including fuselage, gear shaft, clutch, unloading sleeve and flywheel, the flywheel is connected on unloading sleeve, the unloading sleeve is fixedly connected on fuselage, the gear shaft passes through gear, unloading sleeve and clutch, the clutch is for connecting flywheel, the gear is located at the outside of fuselage, and the unloading sleeve, flywheel and clutch are sequentially arranged at the inside of fuselage.The present invention facilitates processing, and operation is reliable.
Description
Technical field
The present invention relates to press machine more particularly to a kind of new type of cam drive-type multiple position press flywheel support constructions.
Background technique
New type of cam drive-type multiple position press flywheel support construction is that one kind is mainly used for using flywheel and tooth
Wheel is cantilevered drive mechanism.
Conventional cam drive-type multiple position press primary flywheel support construction is as shown in Fig. 2, mainly by gear shaft 2, flywheel
5, the part such as support sleeve 12 forms.Flywheel is mounted on gear shaft, the cantilevers such as clutch 3, flywheel 5, gear shaft 2, support sleeve 12
Formula is mounted on 1 outside of fuselage.When work, flywheel high speed rotation, clutch and flywheel junction belt movable gear shaft rotate.
Conventional cam drive-type multiple position press primary flywheel support construction disadvantage is as follows:
1. flywheel is mounted on gear shaft by deep groove ball bearing, the main function of flywheel is storage energy, so flywheel itself
There are certain quality and speed with higher.The gravity and high speed rotation of flywheel have higher requirement to the rigidity of gear shaft.
Gear shaft, which can generate bounce, makes the bearing heating even locking of high speed, and facewidth direction is dropped from normally engaging when engaging gear
The low service life of gear.
2. the cantilevereds such as clutch, flywheel, gear shaft, support sleeve are mounted on fuselage outer side.It is stretched on gear shaft equipped with cantilever
Distance is longer out.Biggish vibration can be generated to lathe when work, the precision of lathe operation is had an impact, the conjunction of product is reduced
Lattice rate.
Summary of the invention
The present invention improves the new type of cam of stability and service life in view of the above problems, provide that a kind of structure is simple
Drive-type multiple position press flywheel support construction.
The technical solution of the present invention is as follows: including fuselage, gear shaft, clutch, unloading sleeve and flywheel, the flywheel is connected to
On unloading sleeve, the unloading sleeve is fixedly connected on fuselage, the gear shaft pass through gear, unloading sleeve and clutch, it is described from
Clutch is for connecting flywheel, and the gear is located at the outside of fuselage, and the unloading sleeve, flywheel and clutch are sequentially arranged at fuselage
Inside.
The fuselage has through-hole, and the unloading sleeve is located in the through-hole of fuselage, and the unloading sleeve includes cylinder, the cylinder
The outside of body is equipped with retaining ring, and the retaining ring and fuselage are bolted.
The unloading sleeve is located at the side of fuselage and gear shaft is equipped with self-aligning bearing, and the other side and the gear shaft of unloading sleeve are set
There is Biserial cylindrical roller bearing.
The flywheel is connected on unloading sleeve by deep groove ball bearing.
At work, flywheel is mounted on unloading sleeve the present invention by deep groove ball bearing, and unloading sleeve is fixed on fuselage, tooth
Wheel is mounted on fuselage outer side, and clutch, flywheel and unloading sleeve are mounted on inboard.Flywheel high speed rotation, clutch and flywheel
In conjunction with to be rotated with movable gear shaft and gear.The weight of flywheel and the load of high-speed rotation are transmitted to fuselage by unloading sleeve
On, reduction has an impact gear shaft and gear, and it is smaller to the rigid requirements of gear shaft, guarantee that gear engagement is steady, extends
Gear life.
The present invention facilitates processing, and operation is reliable.
Detailed description of the invention
Fig. 1 is structural schematic diagram of the invention,
Fig. 2 is the structural schematic diagram of the prior art,
1 is fuselage in figure, and 2 be gear shaft, and 3 be clutch, and 4 be unloading sleeve, and 5 be flywheel, and 6 be through-hole, and 7 be retaining ring, and 8 be aligning
Bearing, 9 be Biserial cylindrical roller bearing, and 10 be deep groove ball bearing, and 11 be gear, and 12 be support sleeve.
Specific embodiment
The present invention is as shown in Figure 1, include fuselage 1, gear shaft 2, clutch 3, unloading sleeve 4 and flywheel 5, the flywheel 5 connects
It connects on unloading sleeve 4, the unloading sleeve 4 is fixedly connected on fuselage, and the gear shaft 2 passes through gear 11, unloading sleeve 4 and clutch
Device 3, for the clutch 3 for connecting flywheel 5, the gear 11 is located at the outside of fuselage, the unloading sleeve 4, flywheel 5 and clutch
Device 3 is sequentially arranged at the inside of fuselage.
At work, flywheel is mounted on unloading sleeve the present invention by deep groove ball bearing, and unloading sleeve is fixed on fuselage, tooth
Wheel is mounted on fuselage outer side, and clutch, flywheel and unloading sleeve are mounted on inboard.Flywheel high speed rotation, clutch and flywheel
In conjunction with to be rotated with movable gear shaft and gear.The weight of flywheel and the load of high-speed rotation are transmitted to fuselage by unloading sleeve
On, reduction has an impact gear shaft and gear, and it is smaller to the rigid requirements of gear shaft, guarantee that gear engagement is steady, extends
Gear life.
Gear is mounted on fuselage outer side, and clutch, flywheel and unloading sleeve are mounted on inboard, reduce hron spacing,
Stress is more reasonable, reduces machine vibration, reduces the requirement of fuselage strength and stiffness.
The fuselage has through-hole 6, and the unloading sleeve is located in the through-hole of fuselage, and the unloading sleeve includes cylinder, described
The outside of cylinder is equipped with retaining ring 7, and the retaining ring and fuselage are bolted.Easy disassembly, connection are reliable.
The unloading sleeve is located at the side of fuselage and gear shaft is equipped with self-aligning bearing 8, the other side of unloading sleeve and gear shaft
Equipped with Biserial cylindrical roller bearing 9.
Two bearing support spacing are big, and stress is more reasonable, guarantee gear and axis stability of rotation, improve lathe running precision
Stability, improve the qualification rate of product.
The flywheel 5 is connected on unloading sleeve by deep groove ball bearing 10, durable reliable.
For this case disclosure of that, need to illustrate there are also the following:
(1), this case the disclosed embodiments attached drawing relates only to and structure involved by this case disclosed embodiment, other knots
Structure, which can refer to, to be commonly designed；
(2), in the absence of conflict, the feature in this case the disclosed embodiments and embodiment can be combined with each other to obtain
New embodiment；
More than, only specific embodiment disclosed in this case, but the protection scope of the disclosure is not limited thereto, and this case institute is public
The protection scope opened should be subject to the protection scope in claims.
Claims (4)
1. a kind of new type of cam drive-type multiple position press flywheel support construction, which is characterized in that including fuselage, gear shaft,
Clutch, unloading sleeve and flywheel, the flywheel are connected on unloading sleeve, and the unloading sleeve is fixedly connected on fuselage, the tooth
Wheel shaft passes through gear, unloading sleeve and clutch, and for the clutch for connecting flywheel, the gear is located at the outside of fuselage, institute
State the inside that unloading sleeve, flywheel and clutch are sequentially arranged at fuselage.
2. a kind of new type of cam drive-type multiple position press flywheel support construction according to claim 1, feature exist
In the fuselage has through-hole, and the unloading sleeve is located in the through-hole of fuselage, and the unloading sleeve includes cylinder, the cylinder
Outside is equipped with retaining ring, and the retaining ring and fuselage are bolted.
3. a kind of new type of cam drive-type multiple position press flywheel support construction according to claim 2, feature exist
In the unloading sleeve is located at the side of fuselage and gear shaft is equipped with self-aligning bearing, and the other side of unloading sleeve and gear shaft are equipped with double
Line column roller bearing.
4. a kind of new type of cam drive-type multiple position press flywheel support construction according to claim 1, feature exist
In the flywheel is connected on unloading sleeve by deep groove ball bearing.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910810852.XA CN110406146A (en) | 2019-08-30 | 2019-08-30 | A kind of new type of cam drive-type multiple position press flywheel support construction |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910810852.XA CN110406146A (en) | 2019-08-30 | 2019-08-30 | A kind of new type of cam drive-type multiple position press flywheel support construction |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN110406146A true CN110406146A (en) | 2019-11-05 |
Family
ID=68369774
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201910810852.XA Pending CN110406146A (en) | 2019-08-30 | 2019-08-30 | A kind of new type of cam drive-type multiple position press flywheel support construction |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN110406146A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112045129A (en) * | 2020-09-04 | 2020-12-08 | 宁波市富川机械有限公司 | Flywheel shaft mounting structure of press |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN201020872Y (en) * | 2007-01-06 | 2008-02-13 | 广东锻压机床厂有限公司 | Clutch braking device for press |
| KR100839524B1 (en) * | 2007-05-18 | 2008-06-19 | 주식회사 화일프레스 | Structure for automatic self aligning bearing of press driving shaft |
| CN201580000U (en) * | 2009-12-30 | 2010-09-15 | 江苏扬力集团有限公司 | Supporting mechanism of press machine clutch and flying wheel |
| CN104070222A (en) * | 2013-03-28 | 2014-10-01 | 南通恒鼎重型机床有限公司 | Internal transmission device for plate shears |
| CN210733368U (en) * | 2019-08-30 | 2020-06-12 | 扬州精善达伺服成形装备有限公司 | Novel cam-driven multi-station press flywheel supporting structure |
-
2019
- 2019-08-30 CN CN201910810852.XA patent/CN110406146A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN201020872Y (en) * | 2007-01-06 | 2008-02-13 | 广东锻压机床厂有限公司 | Clutch braking device for press |
| KR100839524B1 (en) * | 2007-05-18 | 2008-06-19 | 주식회사 화일프레스 | Structure for automatic self aligning bearing of press driving shaft |
| CN201580000U (en) * | 2009-12-30 | 2010-09-15 | 江苏扬力集团有限公司 | Supporting mechanism of press machine clutch and flying wheel |
| CN104070222A (en) * | 2013-03-28 | 2014-10-01 | 南通恒鼎重型机床有限公司 | Internal transmission device for plate shears |
| CN210733368U (en) * | 2019-08-30 | 2020-06-12 | 扬州精善达伺服成形装备有限公司 | Novel cam-driven multi-station press flywheel supporting structure |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112045129A (en) * | 2020-09-04 | 2020-12-08 | 宁波市富川机械有限公司 | Flywheel shaft mounting structure of press |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US10676864B2 (en) | Stranding unit for a stranding machine and basket for a stranding unit | |
| CN110406146A (en) | A kind of new type of cam drive-type multiple position press flywheel support construction | |
| CN103206504A (en) | Buffered sheave driving mechanism | |
| CN205605741U (en) | Decide planet posture heavy load planetary gear train's for speed reducer structure | |
| CN203223529U (en) | Buffer type grooved pulley transmission mechanism | |
| CN210733368U (en) | Novel cam-driven multi-station press flywheel supporting structure | |
| CN103291766A (en) | Shaft end supporting device with convenient disassembly and assembly, and rubber roller rice huller having same | |
| JP5841662B2 (en) | Nacelle mainframe structure and drivetrain assembly for wind turbine | |
| CN101927596A (en) | Oscillating ink device of offset machine | |
| CN106015369B (en) | A kind of high-speed balancing vibrating isolation connection device for high rotating speed turbo pump rotor | |
| CN103818793B (en) | A kind of low speed anti-falling safety device | |
| CN104527968A (en) | Coaxial contra-rotation type screw propeller | |
| CN205937552U (en) | A high -speed balancing vibration isolation coupling device that is used for high rotational speed turbopump rotor | |
| CN205816407U (en) | The buffer unit of cold-rolling mill | |
| CN102562449B (en) | Stepless blade pitch transformation system of medium and small power wind-driven generator | |
| CN200988154Y (en) | Aluminum row on crystal surface grinder | |
| CN207750324U (en) | The swelling centering machine of coating machine | |
| CN103115112A (en) | Inner and outer tooth form meshing gear reducer | |
| CN208276277U (en) | High-speed hot cutting metal annular sawing machine | |
| CN102280246A (en) | Horizontal winding machine | |
| CN103122973A (en) | Rigid inside and outside tooth-profile-wrapped tooth reducer | |
| CN106025552B (en) | A kind of half turntable antenna of large size with high-precision attitude adjustment device | |
| CN209511064U (en) | Buffer unit and retarder and electromechanical equipment with the buffer unit | |
| CN204452920U (en) | A kind of coaxial contrarotating screw propeller | |
| CN104228497A (en) | Engineering vehicle hinge mechanism and engineering vehicle |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| TA01 | Transfer of patent application right |
Effective date of registration: 20240302 Address after: 315033 No. 377 Jinshan Road, Jiangbei District, Ningbo City, Zhejiang Province Applicant after: JDM JINGDA MACHINE (NINGBO) Co.,Ltd. Country or region after: China Address before: No. 108, Xinghua Road, Jianhua Village, high tech Zone, Yangzhou, Jiangsu 225127 Applicant before: YANGZHOU JINGSHANDA SERVO FORMING EQUIPMENT Co.,Ltd. Country or region before: China |
|
| TA01 | Transfer of patent application right |