|
gptkbp:instanceOf
|
nickel-based superalloy
|
|
gptkbp:aluminiumContent
|
1.0-1.8%
|
|
gptkbp:application
|
aerospace
automotive
power generation
|
|
gptkbp:boronContent
|
max 0.006%
|
|
gptkbp:carbonContent
|
max 0.1%
|
|
gptkbp:chromiumContent
|
19-21%
|
|
gptkbp:containsElement
|
gptkb:sulfur
carbon
copper
iron
boron
nickel
aluminium
manganese
silicon
titanium
zirconium
chromium
|
|
gptkbp:copperContent
|
max 0.2%
|
|
gptkbp:developedBy
|
gptkb:Henry_Wiggin_&_Co_Ltd
|
|
gptkbp:form
|
gptkb:Cyclops
gptkb:bar
sheet
rod
strip
|
|
gptkbp:heatTreatment
|
solution treated and aged
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Nimonic 80A
|
|
gptkbp:introducedIn
|
1940s
|
|
gptkbp:ironContent
|
max 3%
|
|
gptkbp:manganeseContent
|
max 1%
|
|
gptkbp:maxOperatingTemperature
|
up to 815°C
|
|
gptkbp:nickelContent
|
balance
|
|
gptkbp:property
|
oxidation resistance
creep resistance
good corrosion resistance
high-temperature strength
|
|
gptkbp:siliconContent
|
max 1%
|
|
gptkbp:standardizedBy
|
BS HR1
BS HR401
BS HR601
UNS N07080
W. Nr. 2.4631
W. Nr. 2.4952
|
|
gptkbp:sulfurContent
|
max 0.015%
|
|
gptkbp:titaniumContent
|
1.8-2.7%
|
|
gptkbp:usedFor
|
turbine blades
exhaust valves
high-temperature components
|
|
gptkbp:zirconiumContent
|
max 0.08%
|
|
gptkbp:bfsParent
|
gptkb:Nimonic
|
|
gptkbp:bfsLayer
|
7
|