US4124732A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Thermal insulation attaching means
Assignee: National Aeronautics and Space Administration
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Filing: 1977-04-12
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Granted: 1978-11-07
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Expires: 1997-04-12
Abstract
Abstract An improved isolation system is provided for attaching ceramic tiles of insulating material to the surface of a structure sought to be protected against extreme temperatures of the nature expected to be encountered by the space shuttle orbiter. This system isolates the fragile ceramic tiles from thermally and mechanically induced vehicle structural strains. The insulating tiles are affixed to a felt isolation pad formed of closely arranged and randomly oriented fibers by means of a flexible adhesive and in turn the felt pad is affixed to the metallic vehicle structure by an additional layer of flexible adhesive.
Inventors
- 👤 Lubert J. Leger
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-24 18:15
CPC Classifications
B; B64; B64G; B64G1/00; B64G1/22; B64G1/52; B64G1/58; Y; Y10; Y10S; Y10S428/00; Y10S428/92; Y10T; Y10T428/00; Y10T428/16; Y10T428/163; Y10T428/164; Y10T428/166; Y10T428/24; Y10T428/24752; Y10T428/24942; Y10T428/26; Y10T428/31504; Y10T428/31652; Y10T428/31663
Claims Analysis
Total Claims: 5
Claim 1
Independent Claim
156 words
In an insulating system for a space vehicle formed of a plurality of insulating tiles of substantially chemically pure rigidized silica tiles attached to a metal substrate of the space vehicle, the tiles having a coefficient of thermal expansion markedly lower than the coefficient of the metal substrate, the improvement comprising: a strain isolation pad between each tile and the metal substrate, said pad attached to each tile and the metal substrate by a separate, layer of flexible adhesive bond, having a thickness less than 10 mils, each pad being formed of a plurality of high temperature resistant, flexible, plastic fibers randomly oriented and closely arranged with respect to each other to form a needled felt configuration isolating said tile from thermal and mechanical stresses generated by deformation of said metal substrate of the space vehicle, said fibers being capable of absorbing within a temperature range of -250° F. to 500° F., said stresses by bending.
Claim 2
Dependent Claim
156 words
In an insulating system for a space vehicle formed of a plurality of insulating tiles of substantially chemically pure rigidized silica tiles attached to a metal substrate of the space vehicle, the tiles having a coefficient of thermal expansion markedly lower than the coefficient of the metal substrate, the improvement comprising: a strain isolation pad between each tile and the metal substrate, said pad attached to each tile and the metal substrate by a separate, layer of flexible adhesive bond, having a thickness less than 10 mils, each pad being formed of a plurality of high temperature resistant, flexible, plastic fibers randomly oriented and closely arranged with respect to each other to form a needled felt configuration isolating said tile from thermal and mechanical stresses generated by deformation of said metal substrate of the space vehicle, said fibers being capable of absorbing within a temperature range of -250° F. to 500° F., said stresses by bending.
Claim 3
Dependent Claim
17 words
The insulating system described in claim 1, wherein said fibers in said strain isolation pad comprise aramid.
Claim 4
Dependent Claim
36 words
The insulating system of claim 2, wherein the strain isolation pad is approximately 160 mils thick and deflects approximately 30 mils under a tensile force of 5.3 psi with a tensile strength of substantially 20 psi.
Claim 5
Dependent Claim
19 words
The insulating system of claim 3 wherein the thin layers of flexible adhesive bond are each approximately 7.5 mils.
References Cited (Backward Citations)
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1981-11-06 | 1982-05-08 | 1982-11-07 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1985-11-06 | 1986-05-08 | 1986-11-07 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1989-11-06 | 1990-05-08 | 1990-11-07 | $7700.00 | Window Closed / Lapsed |