Summus euismod Nickel Alloy GH4133/GH4133B postulandi Applications

TRACTUS

%

In

C

Cr

Mo

IN'

Al

Nb

Of

Fe

And

Mn

P

S

B

Hoc

cum

Mg

Zr

Cum a*

Sn

Sb*

Pb

As

GH4133

MIN

statera

-

19.00

-

-

0.7

1.15

2.5

-

-

-

-

-

-

-

-

-

-

-

-

-

-

-

MAX

statera

0.07

22.00

-

-

1.2

1.65

3

1.50

0.65

0.35

0.014

0.007

0.01

0.01

0.07

-

-

-

-

-

-

-

GH4133B

MIN

statera

-

19.0

-

-

0.75

1.30

2.50

-

-

-

-

-

-

-

-

0.001

0.01

-

-

-

-

-

MAX

statera

0.06

22.0

-

-

1.15

1.70

3.0

1.50

0.65

0.35

0.014

0.007

0.013

0.01

0.07

0.01

0.1

0.0001

0.0012

0.003

0.001

0.0025

Exemplar

density

Liquefaciens temperatus range

GH4133

8.8g/cm3

1325-1390℃

GH4133B

8.21g/cm3

-

GH4133

GH4133B

GB/T 14992 Classificationis et gradus altae temperaturae mixtionum et intermetallicarum compositorum materias summus temperatus

GJB 3165A Specificatio pro vectibus calidis involutis et fictis admixtis caliditatis caliditatis ad partes aerospace portantes.

GJB 5301 Specificationis anuli temperaturae stannum pro applicationibus aerospace

HB/Z 140 Processus curationis caloris admixtus caliditatis admixtis aerospace applicationibus

HB/Z CXL Calor curatio processus caliditas mixturae ad usum aviation

GB/T 14997 High temperatura mixturae placentae rotundae composuerunt

GJB/T 1953A Aircraft Engine Verto

GB 1953A Specificatio pro vectibus calidis revolutis caliditatis mixturae mixturae ad aero-machinam partium rotationis

GJB 3782A Specificatio ad componendos discorum summus temperaturas mixtorum pro aerospace

GJB 3782A Specificatio ad summos temperaturas mixturae discorum fictorum ad aero-machinam partium rotationis.

GJB 5280 Specification for summus temperatus stannum discus machinationis ad aircraft machinam convertendi

GJB 5280 Specificatio ad fabricandum mixturae mixturae supremi temperatae pro partibus aero-machinis rotato

YB 4093 GH4133B mixturae discus argenteorum longitudinalium humilium temporum ordo vexillum