US5152060A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Process for manufacturing fine-structured bodies
Assignee: Airbus Defence and Space GmbH
•
Filing: 1991-05-31
•
Granted: 1992-10-06
•
Expires: 2011-05-31
Abstract
Abstract A method of producing a finely structured body comprised of a plurality of stacked, cut sections of foil at least one of which is provided with grooves. A machinable foil is wrapped around a cylindrical mandrel of a lathe to overlap opposing edges. The overlapped edges are clamped into an axial recess of the cylindrical mandrel by means of a clamping means and a plurality of grooves cut into the surface of the foil by means of at least one shaping diamond positioned in a feed which is finely adjustable. The plurality of grooves each have a groove length, a groove width, and a cross-sectional shape that is constant over the groove length and is freely selectable. Then, the grooved machinable foil is cut into cut sectoins and the cut sections are stacked. 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. Alternately, the machinable foil may be stretched over a vacuum clamping means comprised of a ground, sintered metal plate positioned on a work table which is movable in two mutually perpendicular directions X and Y and a plurality of grooves cut 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.
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
2026-10-23 14:34
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; C; C02; C02F; C02F3/00; C02F3/02; C02F3/10; C02F3/101; F; F28; F28D; F28D9/00; F28D9/0031; F28D9/0037; B01D2201/00; B01D2201/46; B01J2219/00; B01J2219/00781; B01J2219/00783; B01J2219/00819; B01J2219/00833; B01J2219/00835; B01J2219/00873; B01J35/00; B01J35/50; B01J35/56; F28F; F28F2260/00; F28F2260/02; Y; Y02; Y02W; Y02W10/00; Y02W10/10; Y10; Y10T; Y10T29/00; Y10T29/49; Y10T29/4935; Y10T29/49366; Y10T29/51; Y10T29/5183; Y10T82/00; Y10T82/10; Y10T82/26; Y10T82/266
Claims Analysis
Total Claims: 10
Claim 1
Independent Claim
279 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 grove 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. wrapping a machinable foil to be grooved around a cylindrical mandrel of a lathe so as to overlap opposing edges of the machinable foil and cause the overlapped opposing edges to extend transversely to the selected groove direction, which cylindrical mandrel has an axial recess and is provided with a clamping means; b. clamping the overlapped opposing edges of the machinable foil into the axial recess of the cylindrical mandrel by means of the clamping means, which clamping means lies within the axial recess; c. cutting a plurality of parallel grooves into the surface of the machinable foil by means of at least one shaping diamond positioned in a feed which is finely adjustable, which plurality of grooves each have a groove length, a groove width, and a cross-sectional shape that is constant over the groove length and is 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.
Claim 2
Independent Claim
279 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 grove 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. wrapping a machinable foil to be grooved around a cylindrical mandrel of a lathe so as to overlap opposing edges of the machinable foil and cause the overlapped opposing edges to extend transversely to the selected groove direction, which cylindrical mandrel has an axial recess and is provided with a clamping means; b. clamping the overlapped opposing edges of the machinable foil into the axial recess of the cylindrical mandrel by means of the clamping means, which clamping means lies within the axial recess; c. cutting a plurality of parallel grooves into the surface of the machinable foil by means of at least one shaping diamond positioned in a feed which is finely adjustable, which plurality of grooves each have a groove length, a groove width, and a cross-sectional shape that is constant over the groove length and is 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.
Claim 3
Dependent Claim
36 words
The method according to claim 1, wherein the abutted edges of the machinable foil are retained radially in the axial recess of the mandrel and wherein the at least one shaping diamond is a turning tool.
Claim 4
Dependent Claim
22 words
The method according to claim 2, wherein the stacked foils are connected to one another by one of diffusion soldering or welding.
Claim 5
Dependent Claim
14 words
The method according to claim 2, wherein the machinable foil is a metal foil.
Claim 6
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.
Claim 7
Dependent Claim
29 words
The method according to claim 1, wherein the overlapped opposing edges of the machinable foil are pressed into the axial recess of the cylindrical mandrel by the clamping means.
Claim 8
Dependent Claim
22 words
The method according to claim 6, wherein the overlapped opposing edges of the machinable foil are connected by welding prior to clamping.
Claim 9
Dependent Claim
22 words
The method according to claim 1, wherein the overlapped opposing edges of the machinable foil are connected by welding prior to clamping.
Claim 10
Dependent Claim
14 words
The method according to claim 1, wherein the machinable foil is a metal foil.
References Cited (Backward Citations)
DE232933C
Cited
US1215775A
Cited
US1662870A
Cited
FR2279514A1
Cited
US4053969A
Cited
US4277966A
Cited
JPS5836149A
Cited
JPS58209430A
Cited
US4655738A
Cited
US4735019A
Cited
US4620463A
Cited
US4828437A
Cited
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1995-10-06 | 1996-04-06 | 1996-10-06 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1999-10-06 | 2000-04-06 | 2000-10-06 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 2003-10-06 | 2004-04-06 | 2004-10-06 | $7700.00 | Window Closed / Lapsed |