Aluminium Alloy pro erucae fuel cisternina
Structural materiae sunt propinqua ad seriem exitibus ut erucae corpus structuram consilium, vestibulum et dispensando technology, materia praeparatio technology, et oeconomia, et sunt clavis ad determinandum in eruca est scriptor accipere-off qualitas et payload facultatem. Secundum progressionem processus in materia ratio, progressionem processus erucae fuel cisternina materiae potest dividi in quattuor generationes. Prima generatio V-series Aluminium Alloys, id est, al-mg Alloys. Quod repraesentativa Alloys sunt 5A06 et 5A03 Alloys. Illi sunt usus ad fabrica P-II eruca fuel cisternina structuras in nuper 1950s et adhuc usus est hodie. 5A06 Alloys continet 5.8% MG ad 6.8% mg, 5A03 est an al-mg-mn-si stone. Secunda generation est al-cu-fundatur II-series alloys. Sinis scriptor Long Martii Series in Tanks Series launch vehicles fiunt ex Alloys, quae sunt al-cu-mg-mn-si alloy. from the 1970s to the present, China began to use 2219 alloy manufacturing storage tank, which is an Al-Cu-Mn-V-Zr-Ti alloy, is widely used in the manufacture of various launch vehicle storage tanks. In eodem tempore, quod etiam late in structuram telum launch humilis-temperatus cibus obterere, quod est anloy cum optimum humilis temperatus perficientur et comprehensive perficientur.
Aluminium Alloy ad Cameram structuram
Cum progressionem de launch vehicles in Sina in 1960 usque ad nunc, aluminium Alloys ad Cameram structuram de launch vehicles sunt in primo generatione et secundam generationem et intravit in generatione Cameram Structural Aluminium Alloys ((VII) LV Alloy et (VII) LXXXV Alloy), sunt late propter eorum princeps fortitudinem proprietatibus, humilis sensitivity et SCARITUDITATITUTIUNCTUS. (VII) LV est an al-zn-mg-cu-zr mox, et (VII) LXXXV est etiam an al-zn-mg-cu-zr mox, sed ejus immunditia FE et si contentus sunt valde humilis, et Zn contentus est in 7.0% ~ 8.0%. Tertium-generationem al-li alloys per 2a97, MCDLX, etc. fuisse applicari in aliena aerospace industries debitum ad altum viribus, altum modulum et altum elongationem.
Particula, confirmat aluminium matrix compositis habent commoda altum modulum et altum vires, et potest esse reponere 7a09 Alloys ad fabricantium semi-monocoque Camerers. Institute of metallum investigationis, Seres Academy of Sciences, Harbin Institute of Technology, Shanghai Jiaotong University, etc. Fecerunt multum opus in investigationis et praeparatio particula, confirmat aluminium matrice compositis, cum insigni gestis.
Al-Li Alloys in externis Aerospace
Et maxime felix application in aliena aerospace vehicles est Weldalite al-Li Alloy Developed by Constellium et Quebec RDC, inter MMCXCV, MMCXCVI, MMXCVIII, MMCXCVIII, et MMLEY. MMCXCV Alloy: 0.4ag-0.4ag-0.4ag-0,1zR-0.4mg, quod est primum al-Li commercium ad artifices in humilis-temperatus adulteribus ad artifices launches. MMCXCVI Alloy: 0.4ag-0.4ag-0.4MG-0,1zR, humilis density, princeps vires, princeps fractura fractus panel frame profiles, nunc plerumque pro extrudendo aircraft profiles. MMXCVIII Alloy: 0.4ag al-0.4ag-0,1zR-0.4MG, Primitus developed pro fabricare HSCT fuselage, quod est in F16 Pugnator Fuslage et Tank . MMCXCVIII Alloy: 0.4ag-0.4ag-0.9li 0.9li, 0,1zr-0.4mg, usus ad volvere commercii elit sheet. MML Oloy: 0.4ag-0.4ag-0.4ag-0.4Mn-0,1zr-0,1zr, ad (VII) L (VII) L) aircraft structuras et in fabricantium in manufacture components. Comparari cum MMCXCV mixta, in Cu + mn contentus de MML stanna est relative humilis ad redigendum in extinguendo sensibilitatem et ponere altum mechanica proprietatibus in crassa, quod specifica est IV% altior, in specifica est IX% altior, in specifica modulus est IV% altior, in specifica modulus est IV% altior, in specifica est IX% superiore Et fractura lenta est auctus cum princeps accentus corrosio fregisset resistentia et alta lassitudine crack incrementum resistentia, tum summus temperatus stabilitatem.
Sinis scriptor Research in Forging Annulorum in erucae structuris
Sinis scriptor launch vehiculum vestibulum basis sita est in Tianjin oeconomica et technological progressionem zona. Est composito ex eruca investigationis et productio area, an aerospace technology applicationem industria area et auxilia sustentans area. Est integrates erucae partibus productio, pars ecclesiam, ultima ecclesia tentantes.
Et erucae propellant repono tristique formatur per connectens cylindrici cum longitudinem 2m ad 5m. In adipiscing lacus fiunt ex Aluminium Alloy, ita indigent ut connected et confortatus est Aluminium Alloy Fuging Annulorum. In addition, Iungo, transitus annulos transitus tabulae et aliarum partes spatii ut launch vehicles et spatio stationes et opus ad connectens fudentesque annulos, sic fabrica sunt in ipso critica genus connectens et structural sunt valde discrimine genus et structural sunt. Southwest Aluminum (Group) Co., Ltd., Northeast Light Alloy Co., Ltd., and Northwest Aluminum Co., Ltd. have done a lot of work in the research and development, manufacturing and processing of forging rings.
In MMVII, Africum Aluminium Victus technica difficultatibus ut magna-scale casting, colaging Billet ostium, anulum volvens, et frigus deformatio, et developed est aluminium mixturae censu anulum cum diameter 5minarum. In originali Core Forging Technology repleti domestica gap et feliciter applicari ad longum March 5b. In MMXV, Africum aluminium developed primi super-magna aluminium Alloy Altiore citing anulum cum diameter de 9m, profecta est mundus recordum. In MMXVI, Africum aluminium feliciter vicit multis key Core technologiae ut volvens formatam et calor curatio, et developed a super-magna aluminium mixturae fabricans anulum cum diameter 10m, qui posuit novum mundum forsit et solvitur a major key technica forsit Nam progressionem Sinis scriptor gravibus-officium launch lorem.
Edited by May Jiang a Mat Aluminium
Post tempus: 01-2023 Dec
