CN201613676U - High elastic metal composite structure - Google Patents
High elastic metal composite structure Download PDFInfo
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- CN201613676U CN201613676U CN2010201092188U CN201020109218U CN201613676U CN 201613676 U CN201613676 U CN 201613676U CN 2010201092188 U CN2010201092188 U CN 2010201092188U CN 201020109218 U CN201020109218 U CN 201020109218U CN 201613676 U CN201613676 U CN 201613676U
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- metal
- upper plate
- composite structure
- metal substrate
- metal upper
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Abstract
The utility model discloses a high elasticity metal composite construction, it is including metal upper plate and metal substrate, wherein, the metal upper plate combine on the metal substrate with the mode of brazing, the toper bump has on the brazing faying face of metal upper plate or metal substrate. The utility model discloses a structure both can alleviate product weight, improve product strength, can increase the elasticity of product again in finite space, make metal upper plate or metal substrate do the elastic deformation motion in yield strength, avoid because of the fracture that plastic deformation leads to, the performance is very improved.
Description
Technical field:
The utility model relates to a kind of metal structure technical field, especially relates to a kind of metal composite structure.
Background technology:
The high resiliency metal function of demand design in the market is many to be main mode with material selection, for example the carbon steel material of the low toughness of low-intensity is changed to the precipitation hardenable material of high-intensity high-tenacity, this mode is except raising the cost, and the elasticity of product increases limited.
And if also need more high resiliency and high-strength functional, except changing material, it is very necessary that material is carried out the structural elasticity design, for example tabular shock absorber and ware type spring are mainstream product.
The utility model content:
The purpose of this utility model is to provide a kind of high resiliency metal composite structure, it can make workpiece produce higher spring effect in the confined space, can reach the high resiliency effect not gaining in weight or changing under the prerequisite of design, be fit to be applied to the environment of various high-elastic gonosomes.
For achieving the above object, high resiliency metal composite structure of the present utility model includes metal upper plate and metal substrate, wherein, described metal upper plate is incorporated on the metal substrate with brazing mode, has the taper salient point on the soldering faying face of metal upper plate or metal substrate.
As preferable selection, described metal upper plate is steel, stainless steel, titanium alloy, nickel alloy or memorial alloy.
As preferable selection, the thickness of described metal upper plate is between 0.3mm~3.0mm.
As preferable selection, described metal substrate is steel, stainless steel, titanium alloy, nickel alloy or memorial alloy.
As preferable selection, described taper salient point is a quadrangle cone shape.
The beneficial effects of the utility model are: its metal upper plate is incorporated on the metal substrate with brazing mode, and has the taper salient point on the soldering faying face of metal upper plate or metal substrate, not only can alleviate product weight, improved product strength, but also can in the confined space, increase the elasticity of product, make metal upper plate or metal substrate in yield strength, do the strain motion, avoid because of breaking that plastic deformation causes, performance is greatly improved.
Description of drawings:
Below in conjunction with accompanying drawing the utility model is described further:
Fig. 1 is a structural representation of the present utility model;
Fig. 2 is the cutaway view of Fig. 1;
Fig. 3 is the cutaway view of another embodiment of the utility model;
The critical piece symbol description:
Metal upper plate-10 metal substrate-20 taper salient point-30
Macromolecular material-40 brazing material-50
The specific embodiment:
Therefore the following stated only for embodying the preferred embodiment of the utility model principle, does not limit protection domain of the present utility model.
See that accompanying drawing 1 and accompanying drawing 2 show: high resiliency metal composite structure of the present utility model has metal upper plate 10 and metal substrate 20, in the present embodiment, it is ASTM 630 sheet materials of 1.0mm that metal upper plate 10 adopts thickness, metal substrate 20 adopts the ASTM CF-8 foundry goods of 3.5mm, and the surface is processed with the taper salient point 30 of densely covered quadrangle cone shape with milling mode.
Need to prove: metal upper plate 10 and metal substrate 20 all can be any one in steel, stainless steel, titanium alloy, nickel alloy or the memorial alloy, and the processing mode of taper salient point 30 can be modes such as machining, casting, forging, punching press.
During actual production, can select suitable brazing material 50, adopt brazing mode that metal upper plate 10 and metal substrate 20 are combined as a whole.
See shown in the accompanying drawing 3: but between taper salient point 30 filled high polymer material 40 also, to reach shock-absorbing noise abatement or heat insulation function.
Product of the present utility model can be applicable to all kinds of sporting goods, the athletic injury that makes the user bring into play bigger effect or avoid high vibrations to produce; Be applied to then can reach on the building materials light weight and quiet heat insulation effect.
Claims (5)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN2010201092188U CN201613676U (en) | 2010-02-05 | 2010-02-05 | High elastic metal composite structure |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN2010201092188U CN201613676U (en) | 2010-02-05 | 2010-02-05 | High elastic metal composite structure |
Publications (1)
Publication Number | Publication Date |
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CN201613676U true CN201613676U (en) | 2010-10-27 |
Family
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Family Applications (1)
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CN2010201092188U Expired - Fee Related CN201613676U (en) | 2010-02-05 | 2010-02-05 | High elastic metal composite structure |
Country Status (1)
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CN (1) | CN201613676U (en) |
Cited By (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN102398387A (en) * | 2011-08-06 | 2012-04-04 | 张玉梅 | Metal lightweight multilayer composite plate |
CN103085352A (en) * | 2013-01-30 | 2013-05-08 | 沈路平 | Production technology of component-type metal composite plate |
CN104379338A (en) * | 2012-03-07 | 2015-02-25 | 丰田铁工株式会社 | Superimposed composite component |
CN104853909A (en) * | 2012-12-06 | 2015-08-19 | 丰田铁工株式会社 | Multi-layer composite part |
WO2016160188A1 (en) * | 2015-04-02 | 2016-10-06 | Baker Hughes Incorporated | Ultrahigh temperature elastic metal composites |
US9815418B2 (en) | 2013-05-15 | 2017-11-14 | Toyoda Iron Works Co., Ltd. | Laminated composite interior part |
CN110067669A (en) * | 2019-04-28 | 2019-07-30 | 滨州渤海活塞有限公司 | Two body welding type piston structures of one kind and its manufacturing method |
US10427336B2 (en) | 2014-11-20 | 2019-10-01 | Baker Hughes, A Ge Company, Llc | Periodic structured composite and articles therefrom |
US10450828B2 (en) | 2016-10-28 | 2019-10-22 | Baker Hughes, A Ge Company, Llc | High temperature high extrusion resistant packer |
US10759092B2 (en) | 2015-11-19 | 2020-09-01 | Baker Hughes, A Ge Company, Llc | Methods of making high temperature elastic composites |
CN113579236A (en) * | 2021-07-27 | 2021-11-02 | 南京工业大学 | Flexible wall plate with nickel-titanium memory multilayer composite structure, preparation method and application thereof |
-
2010
- 2010-02-05 CN CN2010201092188U patent/CN201613676U/en not_active Expired - Fee Related
Cited By (16)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN102398387A (en) * | 2011-08-06 | 2012-04-04 | 张玉梅 | Metal lightweight multilayer composite plate |
CN104379338A (en) * | 2012-03-07 | 2015-02-25 | 丰田铁工株式会社 | Superimposed composite component |
US9764696B2 (en) | 2012-03-07 | 2017-09-19 | Toyoda Iron Works Co., Ltd. | Superimposed composite interior component |
CN104379338B (en) * | 2012-03-07 | 2018-03-16 | 丰田铁工株式会社 | Overlap composite inner decoration part |
US9987819B2 (en) | 2012-03-07 | 2018-06-05 | Toyoda Iron Works Co., Ltd. | Superimposed composite interior component |
CN104853909A (en) * | 2012-12-06 | 2015-08-19 | 丰田铁工株式会社 | Multi-layer composite part |
CN103085352A (en) * | 2013-01-30 | 2013-05-08 | 沈路平 | Production technology of component-type metal composite plate |
US9815418B2 (en) | 2013-05-15 | 2017-11-14 | Toyoda Iron Works Co., Ltd. | Laminated composite interior part |
US10427336B2 (en) | 2014-11-20 | 2019-10-01 | Baker Hughes, A Ge Company, Llc | Periodic structured composite and articles therefrom |
US11225000B2 (en) | 2014-11-20 | 2022-01-18 | Baker Hughes, A Ge Company, Llc | Periodic structured composite and articles therefrom |
WO2016160188A1 (en) * | 2015-04-02 | 2016-10-06 | Baker Hughes Incorporated | Ultrahigh temperature elastic metal composites |
US9999920B2 (en) | 2015-04-02 | 2018-06-19 | Baker Hughes, A Ge Company, Llc | Ultrahigh temperature elastic metal composites |
US10759092B2 (en) | 2015-11-19 | 2020-09-01 | Baker Hughes, A Ge Company, Llc | Methods of making high temperature elastic composites |
US10450828B2 (en) | 2016-10-28 | 2019-10-22 | Baker Hughes, A Ge Company, Llc | High temperature high extrusion resistant packer |
CN110067669A (en) * | 2019-04-28 | 2019-07-30 | 滨州渤海活塞有限公司 | Two body welding type piston structures of one kind and its manufacturing method |
CN113579236A (en) * | 2021-07-27 | 2021-11-02 | 南京工业大学 | Flexible wall plate with nickel-titanium memory multilayer composite structure, preparation method and application thereof |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
C14 | Grant of patent or utility model | ||
GR01 | Patent grant | ||
C17 | Cessation of patent right | ||
CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20101027 Termination date: 20110205 |