CN204175534U - A kind of elastic supporting mechanism - Google Patents

A kind of elastic supporting mechanism Download PDF

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Publication number
CN204175534U
CN204175534U CN201420594964.9U CN201420594964U CN204175534U CN 204175534 U CN204175534 U CN 204175534U CN 201420594964 U CN201420594964 U CN 201420594964U CN 204175534 U CN204175534 U CN 204175534U
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CN
China
Prior art keywords
round steel
starting taper
supporting mechanism
elastic supporting
collet
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
CN201420594964.9U
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Chinese (zh)
Inventor
盖秀春
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.)
Eulikind Tianjin Technology Co Ltd
Original Assignee
Eulikind Tianjin Technology Co Ltd
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Filing date
Publication date
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Priority to CN201420594964.9U priority Critical patent/CN204175534U/en
Application granted granted Critical
Publication of CN204175534U publication Critical patent/CN204175534U/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02PCLIMATE CHANGE MITIGATION TECHNOLOGIES IN THE PRODUCTION OR PROCESSING OF GOODS
    • Y02P70/00Climate change mitigation technologies in the production process for final industrial or consumer products
    • Y02P70/50Manufacturing or production processes characterised by the final manufactured product

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  • Moulds For Moulding Plastics Or The Like (AREA)

Abstract

The utility model provides a kind of elastic supporting mechanism, comprise integrated support collet, elastometric lining and tapped round steel, described elastometric lining is placed in and supports collet, tapped round steel is located in elastometric lining, and the upper end of round steel and elastometric lining upper end flush, this device upper end is connected with engine room cover connecting base, and lower end is connected with mainframe tie-beam.The beneficial effects of the utility model are: the setting of integrated support collet, elastometric lining and tapped round steel, eliminate the rigid collision between engine room cover connecting base and mainframe tie-beam that wind-driven generator by wind effect in the running causes, improve the working life of product, this approach simplify operation, reduce fabricating cost.

Description

A kind of elastic supporting mechanism
Technical field
The utility model belongs to wind-driven generator manufacturing technology field, especially relates to a kind of elastic supporting mechanism.
Background technique
In existing technology, cabin cover of wind power generator and mainframe are all the tie-beam assembly and connections by engine room cover connecting base and mainframe, for being rigidly connected.When wind-driven generator operates, engine room cover connecting base and the mainframe tie-beam of by wind impact collide mutually, increase mutual damage wearing and tearing, reduce working life.
Model utility content
The purpose of this utility model is to provide a kind of collision, the wearing and tearing that overcome the existing generation that is rigidly connected, improve the working life of connecting base and tie-beam, improve the elastic supporting mechanism in the overall operation life-span of wind-driven generator, be especially applicable to being arranged between engine room cover connecting base and mainframe tie-beam.
The technical solution of the utility model is: a kind of elastic supporting mechanism, comprise integrated support collet, elastometric lining and tapped round steel, described elastometric lining is placed in and supports collet, tapped round steel is located in elastometric lining, and the upper end of round steel and elastometric lining upper end flush, this device upper end is connected with engine room cover connecting base, and lower end is connected with mainframe tie-beam.
Further, described support collet comprises and is connected with starting taper, lower starting taper and support platform from top to bottom in turn, the heavy caliber end of described upper starting taper is connected with the heavy caliber end of lower starting taper, the small-caliber end of lower starting taper is put in support platform, support in collet and be cast with elastometric lining, upper starting taper small-caliber end is connected with engine room cover connecting base, and lower starting taper small-caliber end is connected with mainframe tie-beam.
Further, the small-caliber end of described tapped round steel upper end and upper starting taper flushes, and the lower end of round steel extend in lower starting taper inner chamber.
Further, four corners of described support platform are provided with tapped hole.
Further, the small-bore of described upper starting taper is less than the small-bore of lower starting taper.
Further, the described round steel be connected with engine room cover is cast in elastometric lining by rubber injection mold.
Further, described elastometric lining and round steel integrated poured support collet in.
Further, the material of described support collet is rubber.
The advantage that the utility model has and good effect are: owing to adopting technique scheme, the setting of integrated support collet, elastometric lining and tapped round steel, eliminate the rigid collision between engine room cover connecting base and mainframe tie-beam that wind-driven generator by wind effect in the running causes, improve the working life of product, this approach simplify operation, reduce fabricating cost.
Accompanying drawing explanation
Fig. 1 is stereogram of the present utility model.
Fig. 2 is front view of the present utility model.
Fig. 3 is B-B direction of the present utility model sectional view.
Fig. 4 is plan view of the present utility model.
Structural representation when Fig. 5 is the utility model installation.
Front view when Fig. 6 is the utility model installation.
A-A direction sectional view when Fig. 7 is the utility model installation.
In figure:
1, collet is supported 2, elastometric lining 3, round steel
4, upper starting taper 5, lower starting taper 6, support platform
7, engine room cover connecting base 8, mainframe tie-beam 9, tapped hole
Embodiment
As shown in figs. 1-7,
The technical solution of the utility model is: a kind of elastic supporting mechanism, comprise integrated support collet 1, elastometric lining 2 and tapped round steel 3, described support collet 1, the material of elastometric lining 2 is rubber, described elastometric lining 2 is cast in and supports in collet 1, tapped round steel 3 is cast in elastometric lining 2 by rubber injection mold, described support collet 1 comprises and is connected with starting taper 4 from top to bottom in turn, lower starting taper 5 and support platform 6, the heavy caliber end of described upper starting taper 4 is connected with the heavy caliber end of lower starting taper 5, and the small-bore of upper starting taper 4 is less than the small-bore of lower starting taper 5, the small-caliber end of lower starting taper 5 is put in support platform 6, support in collet 1 and be cast with elastometric lining 2, upper starting taper 4 small-caliber end supporting collet 1 is connected with engine room cover connecting base 7, and bolt is located in threaded round steel 3 through engine room cover connecting base 7, lower starting taper 5 small-caliber end supporting collet 1 is connected with mainframe tie-beam 8, described tapped round steel 3 upper end flushes with the small-caliber end of the upper starting taper 4 supporting collet 1, the lower end of round steel 3 extend in lower starting taper 5 inner chamber, in order to be connected with mainframe tie-beam 8, four corners of described support platform 6 are provided with tapped hole 9.
The working procedure of this example and principle: utilize rubber injection process by pre-for tapped round steel 3 in elastometric lining 2, elastometric lining 2 is cast in simultaneously and supports in collet, reach the once-through of product with this.Eliminate by elastic supporting mechanism the rigid collision between engine room cover connecting base 7 and mainframe tie-beam 8 that wind-driven generator by wind effect in the running causes, improve the working life of product, this approach simplify operation, reduce fabricating cost.
Above an embodiment of the present utility model has been described in detail, but described content being only preferred embodiment of the present utility model, can not being considered to for limiting practical range of the present utility model.All equalizations done according to the utility model application range change and improve, and all should still belong within patent covering scope of the present utility model.

Claims (8)

1. an elastic supporting mechanism, it is characterized in that: comprise integrated support collet, elastometric lining and tapped round steel, described elastometric lining is placed in and supports collet, tapped round steel is located in elastometric lining, and the upper end of round steel and elastometric lining upper end flush, this device upper end is connected with engine room cover connecting base, and lower end is connected with mainframe tie-beam.
2. a kind of elastic supporting mechanism according to claim 1, it is characterized in that: described support collet comprises and is connected with starting taper, lower starting taper and support platform from top to bottom in turn, the heavy caliber end of described upper starting taper is connected with the heavy caliber end of lower starting taper, the small-caliber end of lower starting taper is put in support platform, support in collet and be cast with elastometric lining, upper starting taper small-caliber end is connected with engine room cover connecting base, and lower starting taper small-caliber end is connected with mainframe tie-beam.
3. a kind of elastic supporting mechanism according to claim 2, is characterized in that: the small-caliber end of described tapped round steel upper end and upper starting taper flushes, and the lower end of round steel extend in lower starting taper inner chamber.
4. a kind of elastic supporting mechanism according to claim 1, is characterized in that: four corners of described support platform are provided with tapped hole.
5. a kind of elastic supporting mechanism according to claim 3, is characterized in that: the small-bore of described upper starting taper is less than the small-bore of lower starting taper.
6. a kind of elastic supporting mechanism according to claim 1, is characterized in that: the described round steel be connected with engine room cover is cast in elastometric lining by rubber injection mold.
7. a kind of elastic supporting mechanism according to claim 1, is characterized in that: described elastometric lining and round steel integrated poured support collet in.
8. a kind of elastic supporting mechanism according to claim 1, is characterized in that: the material of described support collet is rubber.
CN201420594964.9U 2014-10-15 2014-10-15 A kind of elastic supporting mechanism Expired - Fee Related CN204175534U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201420594964.9U CN204175534U (en) 2014-10-15 2014-10-15 A kind of elastic supporting mechanism

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201420594964.9U CN204175534U (en) 2014-10-15 2014-10-15 A kind of elastic supporting mechanism

Publications (1)

Publication Number Publication Date
CN204175534U true CN204175534U (en) 2015-02-25

Family

ID=52564347

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201420594964.9U Expired - Fee Related CN204175534U (en) 2014-10-15 2014-10-15 A kind of elastic supporting mechanism

Country Status (1)

Country Link
CN (1) CN204175534U (en)

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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: 20150225

Termination date: 20151015

EXPY Termination of patent right or utility model