CN202165681U - Linear thrustor for actuator - Google Patents

Linear thrustor for actuator Download PDF

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Publication number
CN202165681U
CN202165681U CN2011202355556U CN201120235555U CN202165681U CN 202165681 U CN202165681 U CN 202165681U CN 2011202355556 U CN2011202355556 U CN 2011202355556U CN 201120235555 U CN201120235555 U CN 201120235555U CN 202165681 U CN202165681 U CN 202165681U
Authority
CN
China
Prior art keywords
force moment
linear
axle sleeve
thrust device
moment protection
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
CN2011202355556U
Other languages
Chinese (zh)
Inventor
冯群
王超
石慧
闫正杰
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.)
Sim Automation Engineering Technology (dalian) Co Ltd
Original Assignee
王远鸣
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 王远鸣 filed Critical 王远鸣
Priority to CN2011202355556U priority Critical patent/CN202165681U/en
Application granted granted Critical
Publication of CN202165681U publication Critical patent/CN202165681U/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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Abstract

The utility model belongs to a linear thrustor for an actuator, which comprises a linear thrustor housing, an input shaft, a lead screw, a moment protection shaft sleeve, a sliding block, a spring and an output shaft, and is characterized in that the output end of the actuator drives the input shaft of the linear thrustor to rotate via a key, wherein inner threads formed on the input shaft of the liner thrustor are meshed with the lead screw; the lead screw is mounted on the moment protection shaft sleeve; the sliding block is mounted on the moment protection shaft sleeve, and performs linear motion along the linear thrustor housing; the output shaft drives a valve to perform the linear motion; and when the valve generates moment during the opening/closing, the output shaft protects the moment by compressing the spring.

Description

Final controlling element linear thrust device
Technical field
The utility model belongs to valve actuator, particularly a kind of final controlling element linear thrust device.
Background technique
The final controlling element linear thrust device of present domestic use is the thruster for copying Europe to make mostly, its complex structure, and difficulty of processing is big, and the quality of fit of requirement is also quite high, causes cost too high, and reject rate is high.Do not have the force moment protection function in the structure of its design, cause when moment is excessive, damaging valve or transmission shaft.
Summary of the invention
The objective of the invention is to overcome above technical deficiency, a kind of final controlling element linear thrust device is provided, the implementation structure advantages of simple, with low cost and have a brand-new linear thrust device of force moment protection measure.
The technological scheme that the utility model technical solution problem is adopted is: a kind of final controlling element linear thrust device comprises linear thrust device housing, input shaft, leading screw, force moment protection axle sleeve, slide block, spring and output shaft.It is characterized in that the final controlling element output terminal drives the rotation of linear thrust device input shaft by key; The internal thread of the input shaft of linear thrust device is meshed with leading screw, and leading screw is installed on the force moment protection axle sleeve, on the force moment protection axle sleeve slide block is housed; Make it do straight line motion along linear thrust device housing; Drive valve by output shaft output and do straight line motion, when valve produced moment in open/close process, then output shaft plays pressure spring the effect of force moment protection.
The beneficial effect of the utility model is: this final controlling element linear thrust device is simple in structure, component seldom and difficulty of processing low, very high cost performance is arranged, and has high reliability, have the force moment protection function.
Description of drawings
Specify with embodiment below in conjunction with accompanying drawing.
Fig. 1 is the sectional front view of final controlling element linear thrust device.
1-fixing bolt among the figure; 2-linear thrust device housing; The 3-socket head screw; 4-gland 1; The 5-spring washer; 6-oil sealing 1; 7-pin 1; The 8-lubricating cup; The 9-thrust-bearing; The 10-shaft block ring; 11-oil sealing 2; The 12-seal ring; 13-gland 2; The 14-key; 15-pin 2; The 16-input shaft; The 17-leading screw; The 18-slide block; 19-force moment protection axle sleeve; The 20-nut; The 21-spring support; The 22-spring; The 23-spring capping; The 24-output shaft.
Embodiment
Embodiment, with reference to accompanying drawing, a kind of final controlling element linear thrust device; Comprise linear thrust device housing (2), input shaft (16), leading screw (17), force moment protection axle sleeve (19), slide block (18), spring (22) and output shaft (24), be characterized in that input shaft (16) outside is equipped with 2 by the fixing thrust-bearings (9) of shaft block ring (10), internal whorl and leading screw (17) mesh; Screw-internal thread fit on outside thread on the leading screw (17) and the force moment protection axle sleeve (19) is also fixing with pin 1 (7); Pack into spring support (21) and lock of the shaft shoulder place of output shaft (24) spring (22) of packing into, upper end with 2 nuts (20), and together be installed on the interior platform of force moment protection axle sleeve (19); Screw-internal thread fit in outside thread on the spring capping (23) and the force moment protection axle sleeve (19) is used for fixing output shaft (24); The slide block (18) of packing in the outside square groove of force moment protection axle sleeve (19) wholely is installed in the linear thrust device housing (2) through the inner track of slide block (18) property thruster housing (2) along the line, and is located by interior platform; Oil sealing 2 (11) is installed on the input shaft (16); And 2 (15) be fixed on the linear thrust device housing (2) through pin by gland 2 (13), sealing with seal ring (12), oil sealing 1 (6) is fixed on linear thrust device housing (2) and the force moment protection axle sleeve (19); Compress and be fixed on the linear thrust device housing (2) through socket head screw (3) by gland 1 (4); 1 lubricating cup (8) is housed on the linear thrust device housing (2), and input shaft (16) cooperates with the output shaft of final controlling element through key (14), and fixing by fixing bolt (1); Output shaft (24) matches with the input shaft of valve, and fixing by fixing bolt (1).
This final controlling element linear thrust device mainly is by input shaft (16) and leading screw (17) engagement, and utilizes the track of slide block (18) property thruster housing along the line to do linear movement, and circular movement is transformed into linear motion, adds spring (22) as force moment protection at output terminal.This thruster has simple in structure, and is cheap, superior performance, and reliability is high, characteristics such as band force moment protection.

Claims (1)

1. final controlling element linear thrust device; Comprise linear thrust device housing (2), input shaft (16), leading screw (17), force moment protection axle sleeve (19), slide block (18), spring (22) and output shaft (24); It is characterized in that the final controlling element output terminal drives linear thrust device input shaft (16) rotation by key (14); Input shaft (16) is through internal whorl and leading screw (17) engagement, and leading screw (17) is fixed on the force moment protection axle sleeve (19) through pin 1 (7), and force moment protection axle sleeve (19) is gone up slide block (18) is installed; The inner track of slide block (18) property thruster housing (2) along the line is installed in the linear thrust device housing (2); And by interior platform location, the shaft shoulder place of output shaft (24) spring (22) of packing into, pack into spring support (21) and locking of upper end with 2 nuts (20); And together be installed on the interior platform of force moment protection axle sleeve (19), the screw-internal thread fit in outside thread on the spring capping (23) and the force moment protection axle sleeve (19) is used for fixing output shaft (24).
CN2011202355556U 2011-07-04 2011-07-04 Linear thrustor for actuator Expired - Fee Related CN202165681U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN2011202355556U CN202165681U (en) 2011-07-04 2011-07-04 Linear thrustor for actuator

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN2011202355556U CN202165681U (en) 2011-07-04 2011-07-04 Linear thrustor for actuator

Publications (1)

Publication Number Publication Date
CN202165681U true CN202165681U (en) 2012-03-14

Family

ID=45801506

Family Applications (1)

Application Number Title Priority Date Filing Date
CN2011202355556U Expired - Fee Related CN202165681U (en) 2011-07-04 2011-07-04 Linear thrustor for actuator

Country Status (1)

Country Link
CN (1) CN202165681U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103883789A (en) * 2014-03-26 2014-06-25 上海奇忠控制设备有限公司 Linear thruster

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103883789A (en) * 2014-03-26 2014-06-25 上海奇忠控制设备有限公司 Linear thruster

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Legal Events

Date Code Title Description
C14 Grant of patent or utility model
GR01 Patent grant
ASS Succession or assignment of patent right

Owner name: CIMM AUTOMATION ENGINEERING TECHNOLOGY (DALIAN) CO

Free format text: FORMER OWNER: WANG YUANMING

Effective date: 20130424

C41 Transfer of patent application or patent right or utility model
TR01 Transfer of patent right

Effective date of registration: 20130424

Address after: 116001, No. 71, Renmin Road, Zhongshan District, Liaoning, Dalian, 10

Patentee after: Sim Automation Engineering Technology (Dalian) Co., Ltd.

Address before: 116001, Cheng Cheng, building 71, Renmin Road, Zhongshan District, Liaoning, Dalian, 10F

Patentee before: Wang Yuanming

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

Granted publication date: 20120314

Termination date: 20150704

EXPY Termination of patent right or utility model