US4331497A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Composite shell
Assignee: Honeywell International Inc
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Filing: 1980-12-01
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Granted: 1982-05-25
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Expires: 2000-12-01
Abstract
Abstract A thin-walled annular shell of high rigidity relative to its unit weight is provided. The wall of the shell is a composite material built up layerwise of glassy alloy strips of high transverse aspect ratio such that each layer is a strip wrapped at a substantially 45° helix with respect to the elongate axis of the shell and with adjacent layers having alternating directions of wrap. Bonding between adjacent layers and between strips within each layer is accomplished in a selected manner such that the composite wall is structurally monolithic for thin-walled applications thereby taking substantially full advantage of the extraordinary strength properties of glassy alloy strip.
Inventors
- 👤 John J. Gilman
- 👤 Ralph R. Saunders
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-24 11:29
CPC Classifications
F; F16; F16L; F16L9/00; F16L9/16; Y; Y10; Y10T; Y10T428/00; Y10T428/13
Claims Analysis
Total Claims: 6
Claim 1
Independent Claim
114 words
A method for making a composite thin-walled shell, comprising the steps of: (a) helically wrapping a plurality of layers of glassy alloy strip about an axis of concentricity to form a plurality of substantially orthogonally wrapped layers, each of the layers having a high transverse aspect ratio, adjacent layers having alternating directions of wraps and the ratio of the inner radius to the combined thickness of the layers being at least about 10; b. applying bonding material between said layers to provide a joining shear strength between said layers and said strip within each layer at least about equal to the tensile strength of the glassy alloy strip divided by the transverse aspect ratio.
Claim 2
Independent Claim
114 words
A method for making a composite thin-walled shell, comprising the steps of: (a) helically wrapping a plurality of layers of glassy alloy strip about an axis of concentricity to form a plurality of substantially orthogonally wrapped layers, each of the layers having a high transverse aspect ratio, adjacent layers having alternating directions of wraps and the ratio of the inner radius to the combined thickness of the layers being at least about 10; b. applying bonding material between said layers to provide a joining shear strength between said layers and said strip within each layer at least about equal to the tensile strength of the glassy alloy strip divided by the transverse aspect ratio.
Claim 3
Dependent Claim
29 words
A method as recited in claim 1, comprising the step of helically wrapping said layers at about 40° to 50° angular pitch with respect to the axis of concentricity.
Claim 4
Dependent Claim
12 words
A method as recited in claim 1, wherein layers are bonded adhesively.
Claim 5
Dependent Claim
28 words
A method as recited in claim 1, wherein said bonding step comprises brazing said layers at a temperature less than the glass transition temperature of the glassy alloy.
Claim 6
Dependent Claim
28 words
A method as recited in claim 1, wherein said bonding step comprises soldering said layers at a temperature less than the glass transition temperature of the glassy alloy.
References Cited (Backward Citations)
US3856513A
Cited
US4126287A
Cited
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1985-05-24 | 1985-11-23 | 1986-05-25 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1989-05-24 | 1989-11-23 | 1990-05-25 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1993-05-24 | 1993-11-23 | 1994-05-25 | $7700.00 | Window Closed / Lapsed |