Claims
- 1. A method for preparing a removable system on a mother substrate comprising the steps of:
depositing a high surface to volume sacrificial layer on a mother substrate, stabilizing the sacrificial layer by a) removing volatile chemical species in and on the sacrificial layer and/or b) modifying the surface of the layer, coating over the sacrificial layer with a capping medium fabricating a system on the capping medium, and providing through holes to access the sacrificial layer.
- 2. A method of claim 1, wherein said high surface to volume material is a column-void film or beads.
- 3. A method of claim 2, wherein said column-void film is selected from the group consisting of silicon, silicon oxide, germanium, germanium oxide, and a silicon alloy optionally containing hydrogen, chlorine, or fluorine.
- 4. A method of claim 1, wherein the stabilizing step comprises removing hydrogen from the sacrificial layer, modifying the surface of the sacrificial layer by partial oxidation, and/or nitridation; and the coating step comprises applying a capping medium comprising a stacked film structure of SiO2 and Si3N4 over the sacrificial layer.
- 5. A method of claim 1, further comprising, after the fabricating step, the step of applying a polymer, glass, organic, plastic, semiconductor, quartz, oxide, nitride, insulator, conductor, metal or ceramic top layer onto the system to form a covered system.
- 6. A method of claim 5, wherein said through holes to access the sacrificial layer are provided through the top layer, system, capping layer and/or mother substrate.
- 7. A method of claim 1, wherein the mother substrate contains through holes to access the sacrificial layer.
- 8. A method of claim 7, wherein the through holes in the mother substrate constitute a network in the plane of the substrate or through the thickness of the substrate.
- 9. A method of claim 1, further comprising, after the fabricating step, the step of:
conditioning the exposed surface of the system to enhance bonding of a top layer to the system surface.
- 10. A method of claim 1, further comprising, after the fabricating step, the steps of:
applying onto the system a polymer layer to form a covered system, conditioning the exposed surface of the polymer top layer to enhance bonding, and applying polymer, glass, organic, plastic, semiconductor, quartz, oxide, nitride, insulator, conductor, metal or ceramic top layer to the conditioned polymer surface.
- 11. A method of claim 5 or 10 wherein said top layer is the permanent substrate of the system.
- 12. A method of claim 11, wherein the resulting system is flexible.
- 13. A method of claim 5 or 10, further comprising, during or after the fabricating step but prior to application of the top layer, and prior to providing any top through holes, the steps of:
selectively removing a portion of the system and capping layers to form void regions defining an array of islands composed of device, structure, or system and capping layer regions, and optionally filling the island-defining void region with a sacrificial material.
- 14. A method of claim 13, after application of any top layer and after providing any top through holes, further comprising the step of removing the sacrificial material and the high surface to volume sacrificial layer to release the system from the mother substrate.
- 15. A method of claim 13, wherein the filling step comprises depositing a high surface area to volume material into the void regions.
- 16. A method of claim 1, 2, or 4 further comprising, during or after the fabricating step but the step of providing any through holes, the steps of:
selectively removing a portion of the system and capping layers to form void regions defining an array of islands composed of device, structure, or system and capping layer regions, and filling the island-defining void region with a sacrificial material.
- 17. A method for preparing a sacrificial release layer on mother substrate comprising the steps of:
depositing a high surface to volume sacrificial layer on a mother substrate, stabilizing the sacrificial layer by a) removing volatile chemical species in and on the sacrificial layer and/or b) modifying the surface of the layer.
- 18. A method of claim 17, further comprising coating over the sacrificial layer with a capping medium.
- 19. A method of claim 1, 2, 3, 4, 5, 6, 7, 8, 9, or 10 further comprising the step of removing the sacrificial layer to release the system.
- 20. A method of claim 19, further comprising after the removal step, adhering the system to a permanent substrate.
- 21. A method of claim 20, wherein the permanent substrate is flexible.
- 22. A method of claim 21, further comprising the step of applying a layer to the capping material side of the released system to form a configuration wherein the system is substantially within a bending-stress reduced neutral plane.
- 23. A system prepared by the method of claim 19.
- 24. A system of claim 23, wherein the system comprises at least one device selected from the group consisting of a transistor, a diode, an electron device, a chemical device, a biological device, a bio-chemical device, a fluidic device, a MEM, a sensor, a fuel cell, an opto-electronic device, a photovoltaic cell, an optical structure, and a microelectronic devices, a display, a circuit board system and combinations thereof.
- 25. A system prepared by the method of claim 21.
- 26. A system of claim 25, wherein the system comprises at least one device selected from the group consisting of a transistor, a diode, an electron device, a chemical device, a biological device, a bio-chemical device, a fluidic device, a MEM, a sensor, a fuel cell, an opto-electronic device, a photovoltaic cell, an optical structure, and a microelectronic devices, a display, a circuit board system and combinations thereof.
- 27. A method of claim 20, wherein the adhering step applies at least two system to the permanent substrate in a tiled pattern.
- 28. A method of claim 12 further comprising the step of removing the sacrificial layer to release the system.
PRIORITY CLAIM
[0001] This application claims benefit under 35 U.S.C. §119 to provisional applications serial Nos. 60/347,850, 60/348,259, 60/348,258, all filed Jan. 11, 2002, and 60/408,235, filed Sep. 4, 2002; all of which are incorporated herein by reference.
GOVERNMENT RIGHTS
[0002] The United States Government has rights in this invention under DARPA Grant No. S33615-98-1-5164.
Provisional Applications (4)
|
Number |
Date |
Country |
|
60347850 |
Jan 2002 |
US |
|
60348258 |
Jan 2002 |
US |
|
60348259 |
Jan 2002 |
US |
|
60408235 |
Sep 2002 |
US |