CN204098980U - A kind of Novel valve rotor - Google Patents

A kind of Novel valve rotor Download PDF

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Publication number
CN204098980U
CN204098980U CN201420431733.6U CN201420431733U CN204098980U CN 204098980 U CN204098980 U CN 204098980U CN 201420431733 U CN201420431733 U CN 201420431733U CN 204098980 U CN204098980 U CN 204098980U
Authority
CN
China
Prior art keywords
seat
valve rotator
valve
honour
spring
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
Application number
CN201420431733.6U
Other languages
Chinese (zh)
Inventor
罗胜凯
陈小敏
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Anhui Tianli Engine Co Ltd
Original Assignee
Anhui Tianli Engine Co Ltd
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Anhui Tianli Engine Co Ltd filed Critical Anhui Tianli Engine Co Ltd
Priority to CN201420431733.6U priority Critical patent/CN204098980U/en
Application granted granted Critical
Publication of CN204098980U publication Critical patent/CN204098980U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Abstract

The utility model discloses a kind of Novel valve rotor, comprise seat under the valve rotator seat of honour and valve rotator, it is characterized in that: under the described valve rotator seat of honour and valve rotator, seat is combined to form inner-cavity structure, be provided with valve rotator spring in described inner-cavity structure, above described valve rotator spring, be provided with valve rotator spring thrust plate; Described upper and lower seat forms an inner chamber, is provided with valve rotator spring and valve rotator spring thrust plate in inner chamber.Close up in lower end, the seat of honour, lower seat and thrust plate freely rotate in the lumen and do not come off, and thrust plate has certain activity vertically relative to the seat of honour.The utility model structure is simple, easy for installation, low cost of manufacture, valve limit working edge in rugged environment can be made to rotate, make it avoid the phenomenon occurring one direction concentrated wear, shorten service life of aeroengine.

Description

A kind of Novel valve rotor
Technical field
The utility model relates to a kind of valve rotator, is specifically related to a kind of Novel valve rotor.
Background technique
Diesel engine spiracle be everlasting high temperature, high pressure gas in work, especially the heat load suffered by exhaust valve is larger, and lubrication effect is not fine, this can cause exhaust valve to occur one direction concentrated wear, valve and service life of aeroengine are shortened, thus design, manufacture valve rotator solve this problem.
Model utility content
The purpose of this utility model is to overcome prior art Problems existing, provides a kind of Novel valve rotor, and the utility model structure is simple, and valve limit working edge in rugged environment can be made to rotate.
For realizing above-mentioned technical purpose, reach above-mentioned technique effect, the utility model is achieved through the following technical solutions:
A kind of Novel valve rotor, comprise seat under the valve rotator seat of honour and valve rotator, it is characterized in that: under the described valve rotator seat of honour and valve rotator, seat is combined to form inner-cavity structure, be provided with valve rotator spring in described inner-cavity structure, above described valve rotator spring, be provided with valve rotator spring thrust plate.
Described upper and lower seat forms an inner chamber, is provided with valve rotator spring and valve rotator spring thrust plate in inner chamber.Close up in lower end, the seat of honour, lower seat and thrust plate freely rotate in the lumen and do not come off, and thrust plate has certain activity vertically relative to the seat of honour.
Compared with prior art, the beneficial effects of the utility model are:
The utility model structure is simple, easy for installation, low cost of manufacture, valve limit working edge in rugged environment can be made to rotate, make it avoid the phenomenon occurring one direction concentrated wear, shorten service life of aeroengine.
Accompanying drawing explanation
Fig. 1 is the utility model overall structure schematic diagram.
The 1. valve rotator seats of honour, 2. seat under valve rotator, 3. inner-cavity structure, 4. valve rotator spring, 5. valve rotator spring thrust plate in figure.
Embodiment
Below in conjunction with accompanying drawing, the utility model is further illustrated.
As shown in Figure 1, seat 2 under the valve rotator seat of honour 1 and valve rotator, under the described valve rotator seat of honour 1 and valve rotator, seat 2 is combined to form inner-cavity structure 3, valve rotator spring 4 is provided with in described inner-cavity structure 3, valve rotator spring thrust plate 5 is provided with above described valve rotator spring 4, when machine operation, other are by valve rotator inner chamber 3, valve rotator spring 4 is started working, continuous exchanging gas under the active force of valve rotator spring 4 and valve rotator spring thrust plate 5, the continuous operation of realization.

Claims (2)

1. a Novel valve rotor, comprise seat under the valve rotator seat of honour and valve rotator, it is characterized in that: under the described valve rotator seat of honour and valve rotator, seat is combined to form inner-cavity structure, be provided with valve rotator spring in described inner-cavity structure, above described valve rotator spring, be provided with valve rotator spring thrust plate.
2. a kind of Novel valve rotor according to claim 1, it is characterized in that: close up in lower end, the described valve rotator seat of honour, under valve rotator, seat and thrust plate freely rotate in the lumen and do not come off, and thrust plate has certain activity vertically relative to the valve rotator seat of honour.
CN201420431733.6U 2014-08-01 2014-08-01 A kind of Novel valve rotor Expired - Fee Related CN204098980U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201420431733.6U CN204098980U (en) 2014-08-01 2014-08-01 A kind of Novel valve rotor

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201420431733.6U CN204098980U (en) 2014-08-01 2014-08-01 A kind of Novel valve rotor

Publications (1)

Publication Number Publication Date
CN204098980U true CN204098980U (en) 2015-01-14

Family

ID=52267416

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201420431733.6U Expired - Fee Related CN204098980U (en) 2014-08-01 2014-08-01 A kind of Novel valve rotor

Country Status (1)

Country Link
CN (1) CN204098980U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111706416A (en) * 2020-05-14 2020-09-25 浙江锋锐发动机有限公司 Valve seat ring mounting structure, adjusting method and engine

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111706416A (en) * 2020-05-14 2020-09-25 浙江锋锐发动机有限公司 Valve seat ring mounting structure, adjusting method and engine
CN111706416B (en) * 2020-05-14 2021-08-24 浙江锋锐发动机有限公司 Valve seat ring mounting structure, adjusting method and engine

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Legal Events

Date Code Title Description
C14 Grant of patent or utility model
GR01 Patent grant
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20150114

Termination date: 20170801

CF01 Termination of patent right due to non-payment of annual fee