CN102367769A - Flying hammer bracket - Google Patents
Flying hammer bracket Download PDFInfo
- Publication number
- CN102367769A CN102367769A CN2011102621402A CN201110262140A CN102367769A CN 102367769 A CN102367769 A CN 102367769A CN 2011102621402 A CN2011102621402 A CN 2011102621402A CN 201110262140 A CN201110262140 A CN 201110262140A CN 102367769 A CN102367769 A CN 102367769A
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- Prior art keywords
- hole
- flying hammer
- hammer bracket
- circular columns
- sides
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Abstract
The invention discloses a flying hammer bracket. The flying hammer bracket comprises an upright circular column through hole; two metal base plates are respectively arranged at two sides of the lower end of a circular column; two cylinder-shaped through holes are arranged at two sides of the middle of the circular column; two metal bulged blocks are respectively arranged at the front side and the rear side of the upper end of the circular column. Through arranging through holes at fixing positions of the bracket and arranging threads in the through holes, the flying hammer bracket can exert more stable fixing and supporting functions in parts.
Description
Technical field
The present invention relates to a kind of automobile component, be specifically related to a kind of flying hammer bracket.
Background technique
Flying hammer bracket is widely used at mechanical engineering field, such as all receiving extensive utilization at driving parts of wind power generating set, vehicle transmission part, ship etc.
Power diesel engine generally adopts omnidistance formula mechanical governor at present; Its flying hammer bracket parts are through the assembling of screw thread pretension and implement vacuum brazing or assembling stopping pin reaches the purpose of " on-dismountable " by the rack body of two support shafts and an abnormally-structured complicacy; But the performance of " on-dismountable " that the key problem that exists is to exist is limited, and has been difficult to improve.Trace it to its cause, the size of anti-removal torque is mainly derived from the pre-fastening moment of scyewed joint assembling, and pre-fastening moment receives the restriction of screw strength.Cause the reliability of the diesel engine on the equipments such as being installed on automobile, engineering machinery can not satisfy Equipment Requirement; Although the probability of happening of its fault is not high; But in case generation all is a little critical failures, flying hammer bracket occurs and separate with flyweight shaft, flyball loses the confined equilibrium governor housing and damages; It is dangerous or cause oil-fired system to be scrapped to cause oil-burning machine to produce driving, sometimes even cause whole diesel engine to be scrapped.
Summary of the invention
The object of the present invention is to provide a kind of flying hammer bracket of good stability.
Technological scheme of the present invention is; A kind of flying hammer bracket; Described flying hammer bracket comprises the circular columns through hole of a setting; Be respectively arranged with a metal base plate in the both sides of circular columns lower end, the both sides in the middle of circular columns offer two cylindrical holes, are provided with a metal coupling in the both sides, front and back of circular columns upper end.
In preferred embodiment of the present invention, the symmetrical position of described two metal base plate front ends offers a through hole on the fore-and-aft direction, offers a through hole on the above-below direction in the symmetrical position above the metal base plate, is provided with screw thread in the through hole.
In preferred embodiment of the present invention, described circular columns through hole inboard is provided with screw thread.
In preferred embodiment of the present invention, the below of described metal coupling is provided with a through hole, and the external diameter of through hole is greater than internal diameter.
According to the invention is a kind of flying hammer bracket, on the fixed position of support, offers through hole and screw thread is set in through hole, makes flying hammer bracket in part, play more stable fixed support effect.
Description of drawings
Fig. 1 is the front view of flying hammer bracket one preferred embodiment of the present invention.
Fig. 2 is the plan view of flying hammer bracket one preferred embodiment of the present invention.
Among the figure: 1, flying hammer bracket, 2, circular columns, 3, metal base plate, 4, cylindrical hole, 5, metal coupling.
Embodiment
Below in conjunction with accompanying drawing preferred embodiment of the present invention is set forth in detail, thereby protection scope of the present invention is made more explicit defining so that advantage of the present invention and characteristic can be easier to it will be appreciated by those skilled in the art that.
According to the invention is a kind of flying hammer bracket; Referring to Fig. 1 and Fig. 2; Shown flying hammer bracket 1 comprises the circular columns 2 of a setting; Be respectively arranged with a metal base plate 3 in the both sides of circular columns 2 lower ends, the both sides in the middle of circular columns 2 offer two cylindrical holes 4, are provided with a metal coupling 5 in the both sides, front and back of circular columns 2 upper ends.
Being provided with a through hole on the fore-and-aft direction at two metal base plates 3 away from circular columns 2 one sides, is smooth surface in the through hole, is being provided with a through hole on the above-below direction above the metal base plate 3, and the through hole on the metal base plate 3 on two directions is non-intersect.
Be provided with screw thread in the outstanding cylindrical hole 4 of the both sides in the middle of circular columns 2.
Below two metal couplings 5, also be provided with a through hole, the external diameter of through hole is greater than internal diameter.
According to the invention is a kind of flying hammer bracket, on the fixed position of support, offers through hole and screw thread is set in through hole, makes flying hammer bracket in part, play more stable fixed support effect.
The above is merely embodiment of the present invention; But protection scope of the present invention is not limited thereto; Any those of ordinary skill in the art are in the technical scope that the present invention disclosed; Variation or the replacement that can expect without creative work all should be encompassed within protection scope of the present invention.Therefore, protection scope of the present invention should be as the criterion with the protection domain that claims were limited.
Claims (4)
1. flying hammer bracket; It is characterized in that: described flying hammer bracket comprises the circular columns through hole of a setting; Be respectively arranged with a metal base plate in the both sides of circular columns lower end; Both sides in the middle of circular columns offer two cylindrical holes, are provided with a metal coupling in the both sides, front and back of circular columns upper end.
2. flying hammer bracket according to claim 1; It is characterized in that: the symmetrical position of described two metal base plate front ends offers a through hole on the fore-and-aft direction; Offer a through hole on the above-below direction in the symmetrical position above the metal base plate, be provided with screw thread in the through hole.
3. flying hammer bracket according to claim 1 is characterized in that: described circular columns through hole inboard is provided with screw thread.
4. flying hammer bracket according to claim 1 is characterized in that: the below of described metal coupling is provided with a through hole, and the external diameter of through hole is greater than internal diameter.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2011102621402A CN102367769A (en) | 2011-09-06 | 2011-09-06 | Flying hammer bracket |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2011102621402A CN102367769A (en) | 2011-09-06 | 2011-09-06 | Flying hammer bracket |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN102367769A true CN102367769A (en) | 2012-03-07 |
Family
ID=45760356
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2011102621402A Pending CN102367769A (en) | 2011-09-06 | 2011-09-06 | Flying hammer bracket |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN102367769A (en) |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4289101A (en) * | 1979-04-26 | 1981-09-15 | Robert Bosch Gmbh | Centrifugal rpm governor for internal combustion engines |
| CN2644686Y (en) * | 2003-06-12 | 2004-09-29 | 江苏大学 | Fly-ball holdfast of speed regulator |
| CN201187348Y (en) * | 2008-04-17 | 2009-01-28 | 常州市莱普拉机械制造有限公司 | Small power diesel speed-regulating machine support |
| CN201486662U (en) * | 2009-08-06 | 2010-05-26 | 林春晖 | Flyweight support used for speed controller |
| CN202250405U (en) * | 2011-09-06 | 2012-05-30 | 常熟市迅达粉末冶金有限公司 | Flyweight bracket |
-
2011
- 2011-09-06 CN CN2011102621402A patent/CN102367769A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4289101A (en) * | 1979-04-26 | 1981-09-15 | Robert Bosch Gmbh | Centrifugal rpm governor for internal combustion engines |
| CN2644686Y (en) * | 2003-06-12 | 2004-09-29 | 江苏大学 | Fly-ball holdfast of speed regulator |
| CN201187348Y (en) * | 2008-04-17 | 2009-01-28 | 常州市莱普拉机械制造有限公司 | Small power diesel speed-regulating machine support |
| CN201486662U (en) * | 2009-08-06 | 2010-05-26 | 林春晖 | Flyweight support used for speed controller |
| CN202250405U (en) * | 2011-09-06 | 2012-05-30 | 常熟市迅达粉末冶金有限公司 | Flyweight bracket |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| C02 | Deemed withdrawal of patent application after publication (patent law 2001) | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20120307 |