Zobrazeno 1 - 10
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pro vyhledávání: '"G. L. Shneider"'
Autor:
G. L. Shneider
Publikováno v:
Metal Science and Heat Treatment. 42:105-110
Considerable progress has been made recently in the field of production and application of aluminum alloys with lithium. The accumulated actual material and its analysis has made it possible to use successfully an aluminum-lithium alloy 1420 for the
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f90eb12cfde5defdf81d8633d8d2ebf3
https://doi.org/10.1007/bf02471344
https://doi.org/10.1007/bf02471344
Publikováno v:
Metal Science and Heat Treatment. 41:109-116
1. The susceptibility of aluminum alloys to delayed fracture is connected with the nonuniform decomposition of the solid solution and its low stability. The service life of a part is the shorter the higher the anisotropy of grain boundary fracture, t
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::123aab0adf11ce56413063cc76cf1ab3
https://doi.org/10.1007/bf02467695
https://doi.org/10.1007/bf02467695
Autor:
G. L. Shneider
Publikováno v:
Metal Science and Heat Treatment. 40:294-298
The prospects of the use of aluminum — lithium alloys in the aircaft, industry are due to their diminished density and high rigidity as compared to the similar properties of alloys without lithium. This makes it possible to diminish considerably th
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::fdcef6e685eecd756d938e7afb0e5089
https://doi.org/10.1007/bf02474896
https://doi.org/10.1007/bf02474896
Autor:
G. L. Shneider
Publikováno v:
Metal Science and Heat Treatment. 40:27-33
In recent years Al−Li alloys have become very popular in the aircraft industry. These alloys are characterized by a high specific strength and rigidity which increases substantially the load ratio and fuel efficiency of the parts. As a rule, Al−L
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::928e8f023f2ceceb238606f12dd063fd
https://doi.org/10.1007/bf02468502
https://doi.org/10.1007/bf02468502
Autor:
G. L. Shneider
Publikováno v:
Metal Science and Heat Treatment. 39:87-93
The load-bearing structure of modern airframes requires monolithic members that are produced from large forged and rolled aluminum-alloy semifinished products. These members are designed in accordance with the principle of “safe service life,” an
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::7854a77707b536a3fdd5ab6e364797f1
https://doi.org/10.1007/bf02466272
https://doi.org/10.1007/bf02466272
Autor:
G. L. Shneider
Publikováno v:
Metal Science and Heat Treatment. 38:244-247
Large stamped ribbed preforms are used for fabricating airframe sets of modern aircraft. The quality of critical stamped preforms is determined by the level of the technology of production and heat treatment and is guaranteed by fulfillment of the st
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::e6852c85cd4e05825631fdf17581311a
https://doi.org/10.1007/bf01395822
https://doi.org/10.1007/bf01395822
Autor:
G. L. Shneider
Publikováno v:
Metal Science and Heat Treatment. 37:243-247
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a47081717e2be1c96527b73f25551e1f
https://doi.org/10.1007/bf01152227
https://doi.org/10.1007/bf01152227
Publikováno v:
Metal Science and Heat Treatment. 36:381-385
1. We worked out a technology for stampings of alloy 1420 which takes into account its limited technological ductility, reduced thermal conductivity compared with aluminum alloys used in series production, special traits of the grain structure and of
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::9179f4c637d98e001b05b66acd85de20
https://doi.org/10.1007/bf01395158
https://doi.org/10.1007/bf01395158
Publikováno v:
Metal Science and Heat Treatment. 35:578-581
1. Homogenized ingots of alloy 1420 in tensile tests have considerable scatter of values for relative elongation and reduction of area in the temperature range 300–450°C which requires control of the heating temperature and cooling rate for ingots
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::fabf2ea48a69deb8a079c5be80e528e6
https://doi.org/10.1007/bf00778669
https://doi.org/10.1007/bf00778669
Publikováno v:
Metal Science and Heat Treatment. 35:314-317
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::2f15769ede6f44a44afcdb40d57c3a72
https://doi.org/10.1007/bf00780916
https://doi.org/10.1007/bf00780916