Thermal control of selective laser sintering via control of the laser scan

• US 5,352,405 A
• Filed: 12/18/1992
• Issued: 10/04/1994
• Est. Priority Date: 12/18/1992
• Status: Expired due to Term

• Current Assignee: 3D Systems, Inc. (3D Systems Corporation)
• Original Assignee: DTM Corporation (3D Systems Corporation)
• Inventors: Prioleau, Frost R. R., McGrath, Joseph C., Beaman, Joseph J.
• Primary Examiner(s): Walsh, Donald P.
• Assistant Examiner(s): Greaves, John N.
• Application Number:
  US07/992,926
• Time in Patent Office: 655 Days
• Field of Search: 156/62.2, 219/121.6, 219/121.63, 219/121.64, 219/121.85, 264/22, 264/219, 419/45, 425/174.4, 428/551
• US Class Current: 419/45
• CPC Class Codes: B22F 10/28 Powder bed fusion, e.g. selective laser melting [SLM] or electron beam melting [EBM]
• CPC Class Codes: B22F 10/366 Scanning parameters, e.g. hatch distance or scanning strategy
• CPC Class Codes: B22F 10/368 Temperature or temperature gradient, e.g. temperature of the melt pool
• CPC Class Codes: B22F 12/90 Means for process control, e.g. cameras or sensors
• CPC Class Codes: B29C 2037/90 Measuring, controlling or regulating
• CPC Class Codes: B29C 64/153 using layers of powder being selectively joined, e.g. by selective laser sintering or melting
• CPC Class Codes: B29C 64/171 specially adapted for manufacturing multiple 3D objects
• CPC Class Codes: B33Y 10/00 Processes of additive manufacturing
• CPC Class Codes: B33Y 30/00 Apparatus for additive manufacturing; Details thereof or accessories therefor
• CPC Class Codes: B33Y 40/20 Post-treatment, e.g. curing, coating or polishing
• CPC Class Codes: C23C 24/10 with intermediate formation of a liquid phase in the layer
• CPC Class Codes: G05B 19/4099 Surface or curve machining, making 3D objects, e.g. desktop manufacturing
• CPC Class Codes: G05B 2219/49018 Laser sintering of powder in layers, selective laser sintering SLS
• CPC Class Codes: G05B 2219/49209 Compensation by using temperature feelers on slide, base, workhead
• CPC Class Codes: G05B 2219/49387 Limiting scanning region
• CPC Class Codes: Y02P 10/25 Process efficiency

Abstract

A method and apparatus for fabricating three-dimensional objects according to the selective laser sintering process are disclosed. In order to reduce inconsistencies in structural and textural integrity, and in thermal effects that can cause distortion, methods for ensuring that overlapping laser scans are accomplished in a consistent manner relative to the thermal flow from the sintered locations are utilized. Methods are disclosed for achieving this by limiting the extent to which the laser scans object areas in the powder layers so that the time-to-return for adjacent overlapping scans is minimized; such minimization results in significantly less variation in the time-to-return overall.

Claims

1. A method of producing an object by selective laser sintering, comprising the steps of:

dispensing a first layer of heat-fusible powder over a target surface having a width in a first direction;

defining a first scanning region of the target surface for a first cross-section of the object to be formed in the first layer of powder, said first scanning region having a width, in the first direction, substantially equal to the maximum width of the first cross-section in the first direction, and substantially smaller than the width of the target surface in the first direction;

scanning a directed energy beam in the first direction, beginning at a first end of said first scanning region and stopping upon reaching a second end of said first scanning region;

modulating the directed energy beam on and off during said scanning step so that the directed energy beam is turned on over selected portions of the first layer of powder corresponding to the first cross-section, to fuse the powder thereat; and

repeating said scanning and modulating steps in such a manner that adjacent scans of the directed energy beam overlap one another over the target surface.

2. The method of claim 1, further comprising:

dispensing a second layer of powder over the first layer, after said repeating step;

defining a first scanning region of the target surface for a second cross-section of the object to be formed in the second layer of powder, said first scanning region having a width, in a selected direction, substantially equal to the maximum width of the second cross-section in the selected direction, and substantially smaller than the width of the target surface in the selected direction;

scanning the directed energy beam parallel to the selected direction, beginning at a first end of said first scanning region for the second cross-section and stopping upon reaching a second end of said first scanning region for the second cross-section;

modulating the directed energy beam on and off during said scanning step so that the directed energy beam is turned on over selected portions of the second layer of powder corresponding to the second cross-section, to fuse the powder thereat, with fused portions of the second layer of powder fusing to fused portions of the first layer of powder thereunder; and

repeating said scanning and modulating steps in such a manner that adjacent scans of the directed energy beam overlap one another over the target surface.

3. The method of claim 2, wherein the selected direction is parallel to the first direction.

4. The method of claim 2, wherein the selected direction is not parallel to the first direction.

5. The method of claim 1, further comprising:

defining a second scanning region of the target surface for the first cross-section;

wherein said first and second scanning regions correspond to a first area and a second area, respectively, of the first cross-section;

wherein said first scanning region has a width, in the first direction, substantially equal to the maximum width, in the first direction, of the first cross-section in the first area, and substantially smaller than the width of the target surface in the first direction;

wherein said second scanning region has a width, in the first direction, substantially equal to the maximum width, in the first direction, of the first cross-section in the second area, and substantially smaller than the width of the target surface in the first direction;

and wherein, for said second scanning region, said scanning step scans also the directed energy beam in the first direction, beginning at a first end of said second scanning region and stopping upon reaching a second end of said second scanning region.

6. The method of claim 5, further comprising:

dispensing a second layer of powder over the first layer, after said repeating step;

defining first and second scanning regions of the target surface, corresponding to first and second areas, respectively, of a second cross-section of the object to be formed in the second layer of powder, said first and second scanning regions having a width, in a selected direction, substantially equal to the maximum width of the second cross-section in said first and second scanning regions, respectively, in the selected direction, and substantially smaller than the width of the target surface in the selected direction;

scanning the directed energy beam in a direction parallel to the selected direction, beginning at a first end of said first and second scanning region for the second cross-section and stopping upon reaching a second end of said first scanning region for the second cross-section;

scanning the directed energy beam in a direction parallel to the selected direction, beginning at a first end of said second scanning region for the second cross-section and stopping upon reaching a second end of said first scanning region for the second cross-section;

modulating the directed energy beam on and off during each of said scanning steps so that the directed energy beam is turned on over selected portions of the second layer of powder corresponding to the second cross-section, to fuse the powder thereat so that fused portions of the second layer of powder fusing to fused portions of the first layer of powder thereunder; and

repeating said scanning and modulating steps in such a manner that adjacent scans of the directed energy beam overlap one another over the target surface.

7. The method of claim 1, wherein a plurality of cross-sections of an object are to be formed in the first layer of powder;

and further comprising;

defining a first scanning region of the target surface for each of the plurality of cross-sections to be formed in the first layer of powder, each of said first scanning regions having a width, in the first direction, substantially equal to the maximum width, in the first direction, of its associated one of the plurality of cross-sections, and substantially smaller than the width of the target surface in the first direction;

wherein said scanning step scans the directed energy beam in a direction parallel to the first direction over each of said first scanning regions, each scan beginning at a first end of one of said first scanning regions and stopping upon reaching a second end thereof;

and wherein said modulating step is performed so that the directed energy beam is turned on over selected portions of the first layer of powder corresponding to each of the plurality of cross-sections, to fuse the powder thereat.

8. The method of claim 1, wherein adjacent scans of the directed energy beam are in the same direction as one another.

9. The method of claim 1, wherein adjacent scans of the directed energy beam are in opposite direction from one another.

10. An apparatus for fabricating a part, comprising the steps of:

a target surface, having a width in a first direction;

means for dispensing layers of a solidifiable material at said target surface; and

means for scanning an energy beam across said solidifiable material at said target surface while modulating said energy beam on and off, said energy beam of sufficient energy to fuse said solidifiable material at said target surface when on, wherein said energy beam is turned on by said scanning means at locations corresponding to a cross-section of the part;

wherein said scanning means is programmed to scan said energy beam beginning at a first end of a defined first scanning region of the target surface for the cross-section of the object to be formed and stopping at a second end of the first scanning region, said first scanning region having a width, in the first direction, substantially equal to the maximum width of a first area of the cross-section in the first direction, and substantially smaller than the width of the target surface in the first direction.

11. The apparatus of claim 10, wherein said scanning means is also programmed to scan said energy beam beginning at a first end of a defined second scanning region of the target surface for the cross-section of the part and stopping at a second end of the second scanning region;

and wherein said second scanning region has a width, in the first direction, substantially equal to the maximum width, in the first direction, of a second area of the cross-section of the part in the first direction, and substantially smaller than the width of the target surface in the first direction.

12. The apparatus of claim 10, wherein said scanning means comprises:

a laser;

a plurality of mirrors for directing said laser beam toward the target surface; and

a computer for controlling said plurality of mirrors to scan the laser beam across the target surface.