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US5609288A Expired / Lapsed US ⏱️ 0.0 years remaining

Honeycomb core structure and method and apparatus relating thereto

Assignee: Benecor Inc
•
Filing: 1995-06-06
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Granted: 1997-03-11
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Expires: 2015-06-06
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Abstract

Abstract "A method for fabricating a sheet assemblage ultimately extensible into a honeycomb core structure, including the steps of locating upper and lower metallic foil sheets with their confronting surfaces in uniform continuous engagement with each other and forming successive, staggered laser welded patterns as successive sheets are added to the assemblage."

Inventors

  • 👤 Jeffrey D. Johnson

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-11-05 02:28
CPC Classifications
B; B21; B21D; B21D47/00; B21D39/00; B23; B23K; B23K26/00; B23K26/08; B23K26/0869; B23K26/20; B23K26/21; B23K26/24; B23K26/244; B23K26/26; B23K2101/00; B23K2101/02; B23K2103/00; B23K2103/02; B23K2103/04; B23K2103/05; B23K2103/16; B23K2103/166; Y; Y10; Y10T; Y10T428/00; Y10T428/12; Y10T428/1234; Y10T428/12347; Y10T428/1241

Claims Analysis

Total Claims: 11
Claim 1
Independent Claim 127 words
In a method for fabricating a sheet assemblage ultimately expansible into a honeycomb core structure, the steps of: locating first and second metallic foil sheets with their confronting surfaces in uniform, continuous engagement with each other; forming a plurality of first laser weld patterns between said first and second sheets, said weld patterns being characterized by longitudinal spacing and by termination of the weldments above the bottom surface of said first sheet; placing a third sheet in overlying and contacting relationship with said second sheet, creating longitudinally spaced second weld patterns between said third and second sheets, said second weld patterns being located between said first weld patterns and terminating above the bottom of said second sheet; and expanding said sheets to create a honeycomb core structure.
Claim 2
Dependent Claim 127 words
In a method for fabricating a sheet assemblage ultimately expansible into a honeycomb core structure, the steps of: locating first and second metallic foil sheets with their confronting surfaces in uniform, continuous engagement with each other; forming a plurality of first laser weld patterns between said first and second sheets, said weld patterns being characterized by longitudinal spacing and by termination of the weldments above the bottom surface of said first sheet; placing a third sheet in overlying and contacting relationship with said second sheet, creating longitudinally spaced second weld patterns between said third and second sheets, said second weld patterns being located between said first weld patterns and terminating above the bottom of said second sheet; and expanding said sheets to create a honeycomb core structure.
Claim 3
Dependent Claim 15 words
The method of claim 1 in which said sheets are 0.002 to 0.010 in thickness.
Claim 4
Dependent Claim 14 words
The method of claim 1 in which said sheets are fabricated from aluminum alloys.
Claim 5
Dependent Claim 28 words
The method of claim 1 in which a third weld pattern is formed between a transitional sheet having an altered cell size and the previously formed honeycomb core.
Claim 6
Dependent Claim 22 words
The method of claim 4 in which said third weld pattern reduces the size of said honeycomb cells in said honeycomb core.
Claim 7
Dependent Claim 22 words
The method of claim 4 in which said third weld pattern enlarges the size of said honeycomb cells in said honeycomb core.
Claim 8
Dependent Claim 22 words
The method of claim 4 in which said third weld pattern changes the size of said honeycomb cells in said honeycomb core.
Claim 9
Dependent Claim 15 words
The method of claim 1 in which said sheets are fabricated from stainless steel alloys.
Claim 10
Dependent Claim 14 words
The method of claim 1 in which said sheets are fabricated from titanium alloys.
Claim 11
Dependent Claim 14 words
The method of claim 1 in which said sheets are fabricated from aluminum alloys.

References Cited (Backward Citations)

US3200489A Cited
US3924793A Cited
US4603089A Cited
US4755652A Cited
US5306890A Cited
US5263638A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 2000-03-10 2000-09-09 2001-03-11 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 2004-03-10 2004-09-09 2005-03-11 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 2008-03-10 2008-09-09 2009-03-11 $7700.00 Window Closed / Lapsed

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