CN108642358A - A kind of corrosion resistant magnesium alloy materials of unmanned plane - Google Patents
A kind of corrosion resistant magnesium alloy materials of unmanned plane Download PDFInfo
- Publication number
- CN108642358A CN108642358A CN201810560420.3A CN201810560420A CN108642358A CN 108642358 A CN108642358 A CN 108642358A CN 201810560420 A CN201810560420 A CN 201810560420A CN 108642358 A CN108642358 A CN 108642358A
- Authority
- CN
- China
- Prior art keywords
- parts
- unmanned plane
- corrosion resistant
- magnesium alloy
- alloy materials
- 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.)
- Withdrawn
Links
- 230000007797 corrosion Effects 0.000 title claims abstract description 21
- 238000005260 corrosion Methods 0.000 title claims abstract description 21
- 239000000956 alloy Substances 0.000 title claims abstract description 18
- 229910000861 Mg alloy Inorganic materials 0.000 title claims abstract description 16
- 229910021484 silicon-nickel alloy Inorganic materials 0.000 claims abstract description 9
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 claims abstract description 7
- 229910052749 magnesium Inorganic materials 0.000 claims abstract description 7
- 239000011777 magnesium Substances 0.000 claims abstract description 7
- OAICVXFJPJFONN-UHFFFAOYSA-N Phosphorus Chemical compound [P] OAICVXFJPJFONN-UHFFFAOYSA-N 0.000 claims abstract description 5
- ATJFFYVFTNAWJD-UHFFFAOYSA-N Tin Chemical compound [Sn] ATJFFYVFTNAWJD-UHFFFAOYSA-N 0.000 claims abstract description 5
- HCHKCACWOHOZIP-UHFFFAOYSA-N Zinc Chemical compound [Zn] HCHKCACWOHOZIP-UHFFFAOYSA-N 0.000 claims abstract description 5
- 239000004411 aluminium Substances 0.000 claims abstract description 5
- 229910052782 aluminium Inorganic materials 0.000 claims abstract description 5
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims abstract description 5
- 229910052797 bismuth Inorganic materials 0.000 claims abstract description 5
- JCXGWMGPZLAOME-UHFFFAOYSA-N bismuth atom Chemical compound [Bi] JCXGWMGPZLAOME-UHFFFAOYSA-N 0.000 claims abstract description 5
- 229910052793 cadmium Inorganic materials 0.000 claims abstract description 5
- BDOSMKKIYDKNTQ-UHFFFAOYSA-N cadmium atom Chemical compound [Cd] BDOSMKKIYDKNTQ-UHFFFAOYSA-N 0.000 claims abstract description 5
- 229910017052 cobalt Inorganic materials 0.000 claims abstract description 5
- 239000010941 cobalt Substances 0.000 claims abstract description 5
- GUTLYIVDDKVIGB-UHFFFAOYSA-N cobalt atom Chemical compound [Co] GUTLYIVDDKVIGB-UHFFFAOYSA-N 0.000 claims abstract description 5
- WPBNNNQJVZRUHP-UHFFFAOYSA-L manganese(2+);methyl n-[[2-(methoxycarbonylcarbamothioylamino)phenyl]carbamothioyl]carbamate;n-[2-(sulfidocarbothioylamino)ethyl]carbamodithioate Chemical compound [Mn+2].[S-]C(=S)NCCNC([S-])=S.COC(=O)NC(=S)NC1=CC=CC=C1NC(=S)NC(=O)OC WPBNNNQJVZRUHP-UHFFFAOYSA-L 0.000 claims abstract description 5
- 229910052698 phosphorus Inorganic materials 0.000 claims abstract description 5
- 239000011574 phosphorus Substances 0.000 claims abstract description 5
- 229910052706 scandium Inorganic materials 0.000 claims abstract description 5
- SIXSYDAISGFNSX-UHFFFAOYSA-N scandium atom Chemical compound [Sc] SIXSYDAISGFNSX-UHFFFAOYSA-N 0.000 claims abstract description 5
- 229910052712 strontium Inorganic materials 0.000 claims abstract description 5
- CIOAGBVUUVVLOB-UHFFFAOYSA-N strontium atom Chemical compound [Sr] CIOAGBVUUVVLOB-UHFFFAOYSA-N 0.000 claims abstract description 5
- 229910052725 zinc Inorganic materials 0.000 claims abstract description 5
- 239000011701 zinc Substances 0.000 claims abstract description 5
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 claims description 8
- 229910052759 nickel Inorganic materials 0.000 claims description 4
- 229910052710 silicon Inorganic materials 0.000 claims description 4
- 239000010703 silicon Substances 0.000 claims description 4
- 229910045601 alloy Inorganic materials 0.000 abstract description 4
- 238000013016 damping Methods 0.000 abstract description 3
- 230000000116 mitigating effect Effects 0.000 abstract description 3
- 230000035939 shock Effects 0.000 abstract description 3
- 208000020442 loss of weight Diseases 0.000 abstract description 2
- 239000000463 material Substances 0.000 description 3
- 229910000838 Al alloy Inorganic materials 0.000 description 1
- 239000003513 alkali Substances 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 230000017525 heat dissipation Effects 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 239000005416 organic matter Substances 0.000 description 1
Classifications
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C23/00—Alloys based on magnesium
- C22C23/02—Alloys based on magnesium with aluminium as the next major constituent
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C23/00—Alloys based on magnesium
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C30/00—Alloys containing less than 50% by weight of each constituent
- C22C30/04—Alloys containing less than 50% by weight of each constituent containing tin or lead
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C30/00—Alloys containing less than 50% by weight of each constituent
- C22C30/06—Alloys containing less than 50% by weight of each constituent containing zinc
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Prevention Of Electric Corrosion (AREA)
- Vibration Dampers (AREA)
Abstract
The invention discloses a kind of corrosion resistant magnesium alloy materials of unmanned plane, including following each component to be prepared by weight：45 65 parts of magnesium, 10 30 parts of aluminium, 27 parts of manganese, 12 18 parts of nickel silicon alloy, 13 parts of strontium, 0.5 1.5 parts of zinc, 0.005 0.2 parts of scandium, 0.02 1.5 parts of cobalt, 1.5 5 parts of tin, 1.5 2.5 parts of bismuth, 0.01 0.5 parts of cadmium, 0.01 0.8 parts of phosphorus, this kind of unmanned plane is low with corrosion resistant magnesium alloy materials alloy density, it is better than performance, damping performance is good, corrosion resisting property is good, light weight, rigidity is good, with certain corrosion resistance and stability, shock resistance, it is applied in unmanned plane structure can be with loss of weight 25% 30%, it directly applies in unmanned plane structure to mitigating fuselage weight, increase payload, it improves safety and stealth plays an important role.
Description
Technical field
The present invention relates to air vehicle technique fields, and more specifically, more particularly to a kind of unmanned plane is closed with corrosion resistant magnesium
Golden material.
Background technology
Magnesium alloy is the alloy that other elements composition is added based on magnesium.Its main feature is that：Density is small, and specific strength is high, than
Elasticity modulus is big, good heat dissipation, and absorb shock resistance is good, absorbs impact that load-carrying ability is bigger than aluminium alloy, the corrosive nature of resistance to organic matter and alkali
It is good.The production material of existing unmanned plane.Therefore, a kind of much all to use magnesium alloy machine material in nobody, but due to nothing
Man-machine flight environment of vehicle is complicated, and in existing magnesium alloy materials, corrosion resistance is poor, it would be highly desirable to improve.For this purpose, it is proposed that one
The kind corrosion resistant magnesium alloy materials of unmanned plane.
Invention content
The technical problem to be solved by the present invention is to overcome the defects of the prior art, provide a kind of unmanned plane corrosion resistant magnesium
Alloy material.
In order to solve the above technical problem, the present invention provides the following technical solutions：
A kind of corrosion resistant magnesium alloy materials of unmanned plane, including following each component are prepared by weight：Magnesium 45-65
Part, 10-30 parts of aluminium, 2-7 parts of manganese, 12-18 parts of nickel silicon alloy, 1-3 parts of strontium, 0.5-1.5 parts of zinc, 0.005-0.2 parts of scandium, cobalt
0.02-1.5 parts, 1.5-5 parts of tin, 1.5-2.5 parts of bismuth, 0.01-0.5 parts of cadmium, 0.01-0.8 parts of phosphorus.
Preferably, in the nickel silicon alloy, nickel, silicon the ratio between content be 2：3.
Compared with the prior art, the advantages of the present invention are as follows：This kind of unmanned plane is close with corrosion resistant magnesium alloy materials alloy
Spend that low, better than performance, damping performance is good, corrosion resisting property is good, light weight, rigidity be good, with certain corrosion resistance and stability, resists
It is applied in unmanned plane structure to directly apply in unmanned plane structure to mitigating fuselage with loss of weight 25%-30% by impact
Weight, increase payload, raising safety and stealth play an important role.
Specific implementation mode
The preferred embodiment of the present invention is described in detail below so that advantages and features of the invention can be easier to by
It will be appreciated by those skilled in the art that so as to make a clearer definition of the protection scope of the present invention.
Embodiment 1
A kind of corrosion resistant magnesium alloy materials of unmanned plane, including following each component are prepared by weight：Magnesium 45-65
Part, 10-30 parts of aluminium, 2-7 parts of manganese, 12-18 parts of nickel silicon alloy, 1-3 parts of strontium, 0.5-1.5 parts of zinc, 0.005-0.2 parts of scandium, cobalt
0.02-1.5 parts, 1.5-5 parts of tin, 1.5-2.5 parts of bismuth, 0.01-0.5 parts of cadmium, 0.01-0.8 parts of phosphorus, in the nickel silicon alloy, nickel,
The ratio between content of silicon is 2：3.
Embodiment 2
A kind of corrosion resistant magnesium alloy materials of unmanned plane, including following each component are prepared by weight：55 parts of magnesium,
26 parts of aluminium, 5 parts of manganese, 14 parts of nickel silicon alloy, 1 part of strontium, 1 part of zinc, 0.1 part of scandium, 0.3 part of cobalt, 5 parts of tin, 2 parts of bismuth, 0.1 part of cadmium, phosphorus
0.2 part, in the nickel silicon alloy, nickel, silicon the ratio between content be 2：3.
This kind of unmanned plane is low with corrosion resistant magnesium alloy materials alloy density, better than performance, damping performance is good, corrosion resisting property
Good, light weight, rigidity be good, with certain corrosion resistance and stability, it is applied to subtract in unmanned plane structure by shock resistance
Weight 25%-30% is directly applied in unmanned plane structure to mitigating fuselage weight, increasing payload, improve safety and hidden
Body plays an important role.
Although describing embodiments of the present invention, patent owner can be within the scope of the appended claims
Various deformations or amendments are made, it as long as it does not exceed the scope of protection described in the claims to the invention, all should be in the present invention
Protection domain within.
Claims (2)
1. a kind of corrosion resistant magnesium alloy materials of unmanned plane, it is characterised in that：Prepared by weight including following each component and
At：45-65 parts of magnesium, 10-30 parts of aluminium, 2-7 parts of manganese, 12-18 parts of nickel silicon alloy, 1-3 parts of strontium, 0.5-1.5 parts of zinc, scandium 0.005-
0.2 part, 0.02-1.5 parts of cobalt, 1.5-5 parts of tin, 1.5-2.5 parts of bismuth, 0.01-0.5 parts of cadmium, 0.01-0.8 parts of phosphorus.
2. the corrosion resistant magnesium alloy materials of unmanned plane according to claim 1, it is characterised in that：The nickel silicon alloy
In, nickel, silicon the ratio between content be 2：3.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810560420.3A CN108642358A (en) | 2018-06-04 | 2018-06-04 | A kind of corrosion resistant magnesium alloy materials of unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810560420.3A CN108642358A (en) | 2018-06-04 | 2018-06-04 | A kind of corrosion resistant magnesium alloy materials of unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN108642358A true CN108642358A (en) | 2018-10-12 |
Family
ID=63759330
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810560420.3A Withdrawn CN108642358A (en) | 2018-06-04 | 2018-06-04 | A kind of corrosion resistant magnesium alloy materials of unmanned plane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN108642358A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN118124213A (en) * | 2024-05-08 | 2024-06-04 | 内蒙古工业大学 | Wear-resistant light unmanned aerial vehicle casing composite metal material |
Citations (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107815574A (en) * | 2017-09-28 | 2018-03-20 | 江苏晶王新材料科技有限公司 | A kind of corrosion resistant magnesium alloy materials |
-
2018
- 2018-06-04 CN CN201810560420.3A patent/CN108642358A/en not_active Withdrawn
Patent Citations (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107815574A (en) * | 2017-09-28 | 2018-03-20 | 江苏晶王新材料科技有限公司 | A kind of corrosion resistant magnesium alloy materials |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN118124213A (en) * | 2024-05-08 | 2024-06-04 | 内蒙古工业大学 | Wear-resistant light unmanned aerial vehicle casing composite metal material |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN105315515B (en) | Highly attenuating composition, system shake damper and exempt to shake supporter | |
| CN108642358A (en) | A kind of corrosion resistant magnesium alloy materials of unmanned plane | |
| CN109081962A (en) | A kind of wear-resisting anti-aging automobile rubber shock absorber part material | |
| US4782106A (en) | Rubber adhesive mixture containing Ca(OH)2 for direct bonding to glass or metallic articles | |
| CN106636801A (en) | Magnesium-aluminum alloy product | |
| CN104592590A (en) | Vehicle engine shock-reducing rubber | |
| CN108707781A (en) | A kind of unmanned plane high rigidity Titanium-magnesium alloy material | |
| CN109776890A (en) | A kind of yielding rubber of high-elastic wear-resistant | |
| CN108047747A (en) | The damping isolation material and preparation method of a kind of high environmental suitability | |
| CN105585977B (en) | It is a kind of to improve gluing agent prescription that EPDM rubber is bonded with polyester line and preparation method thereof | |
| CN106800678B (en) | A kind of refining process for the fatigue-resisting rubber material that vehicle vibration damping element uses | |
| CN105936993A (en) | Novel explosion-proof material | |
| CN106191581A (en) | A kind of EMU gear case body dedicated aluminium alloy material | |
| CN104945986A (en) | Wear and damp resistant engine coating | |
| KR100527414B1 (en) | Carcass compound for passenger car | |
| CN108441746A (en) | A kind of unmanned plane magnesium alloy | |
| CN109627607A (en) | A kind of high-temperature resistant rubber of damper | |
| KR100718164B1 (en) | High Damping Viscoelastic Rubber Composition | |
| CN106220907A (en) | A kind of high-damping shock isolating pedestal material | |
| CN203819353U (en) | Automobile and C-shaped column components thereof | |
| CN112280113A (en) | Rubber material for engine mount, preparation method of rubber material, engine mount and automobile | |
| CN106244056B (en) | A kind of automobile using antidetonation adhesive | |
| CN109679167A (en) | A kind of nitrile rubber of environmental protection | |
| CN104403306A (en) | Fiber adhesive-tape film composition, preparation method for fiber adhesive-tape film and fiber adhesive tape | |
| CN102206776A (en) | Honeycomb aluminium foil material |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| WW01 | Invention patent application withdrawn after publication |
Application publication date: 20181012 |
|
| WW01 | Invention patent application withdrawn after publication |