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US4336292A Expired / Lapsed US ⏱️ 0.0 years remaining

Multi-layer honeycomb thermo-barrier material

Assignee: Rohr Inc
•
Filing: 1980-07-11
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Granted: 1982-06-22
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Expires: 2000-07-11
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Abstract

Abstract A thermal barrier material comprising at least four vertically stacked cellular cores separated with septum sheets and enclosed at the outer periphery by facing sheets. The components making up the thermal barrier material may be constructed of titanium alloy, TD nickel, niobium, or the like. In one embodiment, one outer facing sheet is highly polished for use as a reflective surface.

Inventors

  • 👤 Winford Blair

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-11-02 22:09
CPC Classifications
B; B32; B32B; B32B3/00; B32B3/10; B32B3/12; B32B15/00; B32B15/01; E; E04; E04C; E04C2/00; E04C2/30; E04C2/34; E04C2/36; E04C2/365; B32B2250/00; B32B2250/40; Y; Y10; Y10T; Y10T428/00; Y10T428/12; Y10T428/1234; Y10T428/24; Y10T428/24149

Claims Analysis

Total Claims: 13
Claim 1
Independent Claim 157 words
Thermal barrier material for use on space type vehicles to insulate during launch and re-entry comprising: at least four metal honeycomb cellular cores; a first and second metal facing sheet having exposed surfaces; and at least three metal septum sheets; said metal honeycomb cellular cores are stacked in the direction of the cell openings with the septum sheets positioned between and physically bonded to their adjacent cellular cores and said facing sheets are positioned and physically attached on the cell surfaces of the outer cores to provide closures therefor whereby when the exposed surface of said first metal facing sheet is subjected to an operating temperature of 1000° F. to 2500° F., said thermal barrier material insulates said second metal facing sheet from said first metal facing sheet wherein the exposed surface temperature of said second metal facing sheet is a maximum of from 25% to 10% of the surface temperature of said first metal facing sheet.
Claim 2
Dependent Claim 157 words
Thermal barrier material for use on space type vehicles to insulate during launch and re-entry comprising: at least four metal honeycomb cellular cores; a first and second metal facing sheet having exposed surfaces; and at least three metal septum sheets; said metal honeycomb cellular cores are stacked in the direction of the cell openings with the septum sheets positioned between and physically bonded to their adjacent cellular cores and said facing sheets are positioned and physically attached on the cell surfaces of the outer cores to provide closures therefor whereby when the exposed surface of said first metal facing sheet is subjected to an operating temperature of 1000° F. to 2500° F., said thermal barrier material insulates said second metal facing sheet from said first metal facing sheet wherein the exposed surface temperature of said second metal facing sheet is a maximum of from 25% to 10% of the surface temperature of said first metal facing sheet.
Claim 3
Dependent Claim 25 words
The invention as defined in claim 1, wherein said first facing sheet has a highly polished outer surface to thereby provide a mirror like surface.
Claim 4
Dependent Claim 21 words
The invention as defined in claim 1 wherein said cellular cores, septum sheets and facing sheets are constructed of titanium alloys.
Claim 5
Dependent Claim 20 words
Invention as defined in claim 1 where said cellular cores, septum sheets and facing sheets are constructed of TD nickel.
Claim 6
Dependent Claim 20 words
The invention as defined in claim 1, wherein said cellular cores, septum sheets and facing sheets are constructed of columbium.
Claim 7
Dependent Claim 15 words
The invention as defined in claim 1, wherein said cores are substantially two inches thick.
Claim 8
Dependent Claim 31 words
The invention as defined in claim 1 wherein one surface of the facing sheets and all surfaces of the septum sheets are sequentially plated with layers of silver, copper and nickel.
Claim 9
Dependent Claim 25 words
The invention as defined in claim 1 wherein the faying edges of the cellular cores are sequentially plated with layers of silver, copper and nickel.
Claim 10
Dependent Claim 36 words
The invention as defined in claim 1 wherein one surface of the facing sheets, all surfaces of the septum sheets and the faying edges of the cellular cores are sequentially plated with silver, copper and nickel.
Claim 11
Dependent Claim 29 words
The invention as defined in claim 1, wherein one surface of the facing sheets and all surfaces of the septum sheets are coated with a layer of braze material.
Claim 12
Dependent Claim 34 words
The invention as defined in claim 1, wherein one surface of the facing sheets, all surfaces of the septum sheets and the faying edges of the cellular cores are coated with a braze material.
Claim 13
Dependent Claim 61 words
The invention as defined in claim 1, wherein a portion of the surface of the facing sheets, septum sheets and the faying edges of the cellular cores are coated with layers of silver, copper and nickel, and the remaining surfaces of the facing sheets and septum sheets and the faying edges of the cellular core are coated with a braze material.

References Cited (Backward Citations)

US2501180A Cited
US2609068A Cited
US2839442A Cited
US3030703A Cited
US3427706A Cited
US3854194A Cited
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US4042238A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1985-06-21 1985-12-21 1986-06-22 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1989-06-21 1989-12-21 1990-06-22 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1993-06-21 1993-12-21 1994-06-22 $7700.00 Window Closed / Lapsed

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