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US3869779A Expired / Lapsed US ⏱️ 0.0 years remaining

Duplex aluminized coatings

Assignee: National Aeronautics and Space Administration
•
Filing: 1974-01-24
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Granted: 1975-03-11
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Expires: 1994-01-24
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Abstract

Abstract The surface of a metallic base system is initially coated with a metallic alloy layer that is ductile and oxidation resistant. An aluminide coating is then applied to the metallic alloy layer. The chemistry of the metallic alloy layer is such that the oxidation resistance of the subsequently aluminized outermost layer is not seriously degraded.

Inventors

  • 👤 Michael A Gedwill
  • 👤 Salvatore J Grisaffe

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-24 02:16
CPC Classifications
C; C23; C23C; C23C28/00; C23C28/30; C23C28/34; C23C28/345; C23C28/3455; B; B23; B23K; B23K20/00; B23K20/22; B23K20/233; B23K20/2333; C23C10/00; C23C10/02; C23C28/02; C23C28/023; C23C28/32; C23C28/321; C23C28/3215; C23C28/341; C23C4/00; C23C4/04; C23C4/06; C23C4/073; C30; C30B; C30B21/00; C30B21/02; Y; Y10; Y10S; Y10S428/00; Y10S428/922; Y10S428/9335; Y10S428/941; Y10T; Y10T428/00; Y10T428/12; Y10T428/12431; Y10T428/12493; Y10T428/12736; Y10T428/1275; Y10T428/12771; Y10T428/12861; Y10T428/12931; Y10T428/12986

Claims Analysis

Total Claims: 11
Claim 1
Independent Claim 45 words
A COATED ARTICLE OF MANUFACTURE COMPRISING A SUPERALLOY SUBSTRATE SELECTED FROM THE GROUP CONSISTING OF NICKEL-BASE SUPERALLOYS AND COBALT-BASE SUPERALLOYS, DISPERSION-STRENGTHENED ALLOYS, COMPOSITES, AND DIRECTIONAL EUTECTICS, A DUCTILE, OXIDATION RESISTANT METALLIC ALLOY LAYER COVERING SAID SUBSTRATE, AND AN ALUMIDE COATING COVERING SAID METALLIC ALLOY LAYER.
Claim 2
Dependent Claim 45 words
A COATED ARTICLE OF MANUFACTURE COMPRISING A SUPERALLOY SUBSTRATE SELECTED FROM THE GROUP CONSISTING OF NICKEL-BASE SUPERALLOYS AND COBALT-BASE SUPERALLOYS, DISPERSION-STRENGTHENED ALLOYS, COMPOSITES, AND DIRECTIONAL EUTECTICS, A DUCTILE, OXIDATION RESISTANT METALLIC ALLOY LAYER COVERING SAID SUBSTRATE, AND AN ALUMIDE COATING COVERING SAID METALLIC ALLOY LAYER.
Claim 3
Dependent Claim 45 words
A coated article of manufacture comprising a superalloy substrate selected from the group consisting of nickel-base superalloys and coablt-base superalloys, dispersion-strengthened alloys, composites, and directional eutectics, a ductile, oxidation resistant metallic alloy layer covering said substrate, and an aluminide coating covering said metallic alloy layer.
Claim 4
Dependent Claim 45 words
A coated article of manufacture comprising a superalloy substrate selected from the group consisting of nickel-base superalloys and coablt-base superalloys, dispersion-strengthened alloys, composites, and directional eutectics, a ductile, oxidation resistant metallic alloy layer covering said substrate, and an aluminide coating covering said metallic alloy layer.
Claim 5
Dependent Claim 17 words
An article of manufacture is claimed in claim 1 wherein the metallic alloy layer comprises a cladding.
Claim 6
Dependent Claim 18 words
An article of manufacture as claimed in claim 2 wherein the metallic alloy layer comprises a foil cladding.
Claim 7
Dependent Claim 33 words
An article of manufacture as claimed in claim 3 wherein the foil cladding is a NiCrAl alloy containing one or more elements selected from the group consisting of Si, Y, Mn, and Th.
Claim 8
Dependent Claim 36 words
An article of manufacture as claimed in claim 4 whereIn the foil cladding is an alloy consisting essentially of from 15 to 25% chromium, 3 to 6% aluminum, 0.5 to 1.5% silicon, and the balance nickel.
Claim 9
Dependent Claim 28 words
An article of manufacture as claimed in claim 5 wherein the alloy consists essentially of about 18% chromium, about 4% aluminum, about 1% silicon, and the balance nickel.
Claim 10
Dependent Claim 33 words
An article of manufacture as claimed in claim 3 wherein the foil cladding is a FeCrAl alloy containing one or more elements selected from the group consisting of Y, Si, Mn, and Ta.
Claim 11
Dependent Claim 36 words
An article of manufacture as claimed in claim 7 wherein the foil cladding is an alloy consisting essentially of from 15 to 25% chromium, 3 to 6% aluminum, 0.1 to 1% yttrium, and the balance iron.

References Cited (Backward Citations)

US3542530A Cited
US3620693A Cited
US3649225A Cited
US3754903A Cited
US3676085A Cited
US3741791A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1978-03-10 1978-09-09 1979-03-11 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1982-03-10 1982-09-09 1983-03-11 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1986-03-10 1986-09-09 1987-03-11 $7700.00 Window Closed / Lapsed

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