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US5249359A Expired / Lapsed US ⏱️ 0.0 years remaining

Process for manufacturing finely structured bodies such as heat exchangers

Assignee: Airbus Defence and Space GmbH
•
Filing: 1992-03-19
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Granted: 1993-10-05
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Expires: 2012-03-19
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Abstract

Abstract A method of producing a finely structured body which includes a plurality of stacked, cut sections of foil at least one of which is provided with grooves in a selected groove direction on at least one surface thereof, and which has a plurality of closely juxtaposed, channel-like perforations with high shape accuracy, true dimensions and high surface quality. The method includes: a. providing a vacuum clamping means comprised of a ground, sintered metal plate which is connected to a vacuum source and which is positioned on a work table which is movable in two mutually perpendicular directions X and Y; b. positioning a machinable foil on the ground, sintered metal plate and clamping the machinable foil thereto by applying an effective amount of vacuum; c. cutting a plurality of parallel grooves into the surface of the machinable foil by means of at least one shaping diamond positioned on a cutting spindle and adjustable in a direction Z, each groove of the plurality of grooves having a groove length, a groove width, and a cross-sectional shape that is constant over the groove length and freely selectable; d. cutting the grooved machinable foil into cut sections having selected lengths and widths; and e. stacking the cut sections, wherein the plurality of grooves have a form precision such that, for groove lengths of more than 1000 μm, the groove width has an accuracy of about +1 μm for land widths which equal or exceed about 15 μm.

Inventors

  • 👤 Klaus Schubert
  • 👤 Wilhelm Bier
  • 👤 Gerd Linder
  • 👤 Peter Schmid
  • 👤 Peter Bichler
  • 👤 Winfried Brunner
  • 👤 Wolfgang Simon

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-11-01 15:40
CPC Classifications
G; G02; G02B; G02B5/00; G02B5/18; G02B5/1847; G02B5/1852; B; B01; B01D; B01D25/00; B01D25/001; B01D25/22; B01D25/26; B01J; B01J19/00; B01J19/0093; B23; B23B; B23B1/00; B23C; B23C3/00; B23P; B23P15/00; B23P15/26; F; F28; F28D; F28D9/00; F28D9/0031; F28D9/0037; F28F; F28F13/00; F28F13/18; F28F13/185; B01D2201/00; B01D2201/46; B01J35/00; B01J35/50; B01J35/56; C; C02; C02F; C02F3/00; C02F3/02; C02F3/10; C02F3/101; F28F2260/00; Y; Y02; Y02W; Y02W10/00; Y02W10/10; Y10; Y10T; Y10T29/00; Y10T29/30; Y10T29/301; Y10T29/307; Y10T29/49; Y10T29/4935; Y10T29/49366; Y10T29/49826

Claims Analysis

Total Claims: 3
Claim 1
Independent Claim 261 words
A method of producing a finely structured body which is useful as a heat exchanger, a mechanical fine filter or an optical grating, which is comprised of a plurality of stacked, cut sections of foil at least one of which is provided with grooves in a selected groove direction on at least one surface thereof, and which has a plurality of closely juxtaposed, channel-like perforations with high shape accuracy, true dimensions and high surface quality, the method comprising: a. providing a vacuum clamping means comprised of a ground, sintered metal plate which is connected to a vacuum source and which is positioned on a work table which is movable in two mutually perpendicular directions X and Y; b. positioning a machinable foil on the ground, sintered metal plate and clamping the machinable foil thereto by applying an effective amount of vacuum; c. cutting a plurality of parallel grooves into the surface of the machinable foil by means of at least one shaping diamond positioned on a cutting spindle and adjustable in a direction Z, each groove of the plurality of grooves having a groove length, a groove width, and a cross-sectional shape that is constant over the groove length and freely selectable; d. cutting the grooved machinable foil into cut sections having selected lengths and widths; and e. stacking the cut sections, wherein the plurality of grooves have a form precision such that, for groove length of more than 1000 μm, the groove width has an accuracy of about +1 μm for land widths which euqal or exceed about 15 μm.
Claim 2
Independent Claim 261 words
A method of producing a finely structured body which is useful as a heat exchanger, a mechanical fine filter or an optical grating, which is comprised of a plurality of stacked, cut sections of foil at least one of which is provided with grooves in a selected groove direction on at least one surface thereof, and which has a plurality of closely juxtaposed, channel-like perforations with high shape accuracy, true dimensions and high surface quality, the method comprising: a. providing a vacuum clamping means comprised of a ground, sintered metal plate which is connected to a vacuum source and which is positioned on a work table which is movable in two mutually perpendicular directions X and Y; b. positioning a machinable foil on the ground, sintered metal plate and clamping the machinable foil thereto by applying an effective amount of vacuum; c. cutting a plurality of parallel grooves into the surface of the machinable foil by means of at least one shaping diamond positioned on a cutting spindle and adjustable in a direction Z, each groove of the plurality of grooves having a groove length, a groove width, and a cross-sectional shape that is constant over the groove length and freely selectable; d. cutting the grooved machinable foil into cut sections having selected lengths and widths; and e. stacking the cut sections, wherein the plurality of grooves have a form precision such that, for groove length of more than 1000 μm, the groove width has an accuracy of about +1 μm for land widths which euqal or exceed about 15 μm.
Claim 3
Dependent Claim 22 words
The method according to claim 1, wherein the stacked foils are connected to one another by one of diffusion soldering or welding.

References Cited (Backward Citations)

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US1215775A Cited
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US4053969A Cited
US4277966A Cited
JPS5836149A Cited
JPS58209430A Cited
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USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1996-10-04 1997-04-05 1997-10-05 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 2000-10-04 2001-04-05 2001-10-05 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 2004-10-04 2005-04-05 2005-10-05 $7700.00 Window Closed / Lapsed

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