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US3989602A Expired / Lapsed US ⏱️ 0.0 years remaining

Method of making reinforced composite structures

Assignee: National Aeronautics and Space Administration
•
Filing: 1974-04-19
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Granted: 1976-11-02
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Expires: 1994-04-19
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Abstract

Abstract A process for making composite structures built up on a mandrel having a smooth outer surface by winding a filament having at least one flat side as viewed in cross-section upon that surface with the flat side against it, and then electroforming matrix material on the wire and on the surface between spaced convolutions until the matrix material builds out beyond the level of the wound convolutions at all points, and then machining away the matrix material until a new smooth surface is attained on which to precision-wind the next filament convolutions with their flat sides in close contact therewith and with the spacings between convolutions very closely controlled.

Inventors

  • 👤 Lee C. McCandless
  • 👤 Glenn E. Weber

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-23 14:42
CPC Classifications
C; C25; C25D; C25D1/00; C25D1/02; Y; Y10; Y10S; Y10S428/00; Y10S428/922; Y10S428/9335; Y10S428/934; Y10S428/935; Y10T; Y10T29/00; Y10T29/49; Y10T29/49801; Y10T29/4998; Y10T29/49982; Y10T428/00; Y10T428/12; Y10T428/12465; Y10T428/12486

Claims Analysis

Total Claims: 7
Claim 1
Independent Claim 138 words
The process of making a composite structure on a mandrel having a smooth outer surface, said structure including multiple layers of reinforcing filaments spaced at different levels and embedded in a metallic matrix material, including the steps of: a. winding a filament having at least one flat side as viewed in cross-section onto said smooth outer surface with the flat side thereagainst and precision spacing successive convolutions; b. depositing metallic matrix material by electroforming onto the convolutions of the filament and onto said outer surface exposed therebetween, and continuing such electroforming until the matrix material between the convolutions builds up above the level of the wound filament; c. machining the structure by removing matrix material until a new smooth outer surface is exposed above the level of the filament; and d. repeating said steps to produce another layer.
Claim 2
Dependent Claim 138 words
The process of making a composite structure on a mandrel having a smooth outer surface, said structure including multiple layers of reinforcing filaments spaced at different levels and embedded in a metallic matrix material, including the steps of: a. winding a filament having at least one flat side as viewed in cross-section onto said smooth outer surface with the flat side thereagainst and precision spacing successive convolutions; b. depositing metallic matrix material by electroforming onto the convolutions of the filament and onto said outer surface exposed therebetween, and continuing such electroforming until the matrix material between the convolutions builds up above the level of the wound filament; c. machining the structure by removing matrix material until a new smooth outer surface is exposed above the level of the filament; and d. repeating said steps to produce another layer.
Claim 3
Dependent Claim 15 words
The process as set forth in claim 1, wherein said filament is D-shaped in cross-section.
Claim 4
Dependent Claim 36 words
The process as set forth in claim 2, wherein said filament is semicircular in cross-section and said convolutions are spaced apart no less than one-half the width of the filament as measured across its flat side.
Claim 5
Dependent Claim 24 words
The process as set forth in claim 3, wherein said width of the filament is substantially within the range of 8 to 200 mils.
Claim 6
Dependent Claim 15 words
The process as set forth in claim 1, wherein the filament is stainless steel wire.
Claim 7
Dependent Claim 64 words
The process as set forth in claim 5, wherein the matrix material is nickel electroformed onto the filament and the exposed surface between convolutions, and wherein between each winding step and the subsequent electroforming step there is interposed the step of treating the wound convolutions and the surface therebetween by degreasing and reactivating them to insure bonding of the matrix material subsequently electroformed thereon.

References Cited (Backward Citations)

DE85173C Cited
US3505177A Cited
US3763001A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1979-11-02 1980-05-03 1980-11-02 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1983-11-02 1984-05-03 1984-11-02 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1987-11-02 1988-05-03 1988-11-02 $7700.00 Window Closed / Lapsed

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