Claims
- 63. A method of forming a (Ga, Al, In)N material, comprising carrying out the growth of said (Ga, Al, In)N material on a substrate by an HVPE epitaxial growth process, under low surface mobility growth conditions and for sufficient time to form a low defect density, large area, substantially crack-free (Ga, Al, In)N material having a defect density of 107 defects/cm2 or lower, wherein the defects comprise threading dislocations having a tilt angle substantially greater than 0.1 degree and the HVPE epitaxial growth process is carried out to grow said low defect density, large area, substantially crack-free (Ga, Al, In)N material to a thickness of at least 10 μm.
- 64. A method according to claim 63, wherein the HVPE epitaxial growth process is carried out at a temperature in a range of from about 985° C. to about 1010° C.
- 65. A method according to claim 63, wherein the (Ga, Al, In)N material has a defect density below 106 defects/cm2.
- 66. A method according to claim 63, wherein the (Ga, Al, In)N material is grown on a lattice-mismatched template material.
- 67. A method of forming a (Ga, Al, In)N material, comprising carrying out the growth of said (Ga, Al, In)N material on a substrate by an HVPE epitaxial growth process, under low surface mobility growth conditions and for sufficient time to form a low defect density, large area, substantially crack-free (Ga, Al, In)N material, wherein the (Ga, Al, In)N material includes dislocations that are predominantly angled with respect to the growth direction at a tilt angle substantially greater than 0.1 degree, said (Ga, Al, In)N material has a defect density of 107 defects/cm2 or lower, and the HVPE epitaxial growth process is carried out to grow said low defect density, large area, substantially crack-free (Ga, Al, In)N material to a thickness of at least 10 μm.
- 68. A method according to claim 67, wherein the (Ga, Al, In)N material includes dislocations that are predominantly angled with respect to the growth direction by a tilt angle less than about 40°.
- 69. A method according to claim 67, wherein the dislocations are at least 5 micrometers from the substrate in the growth direction of the (Ga, Al, In)N material.
- 70. A method according to claim 63, wherein the (Ga, Al, In)N material includes dislocations that are predominantly mixed-type threading dislocations.
- 71. A method of forming a (Ga, Al, In)N material, comprising carrying out the growth of said (Ga, Al, In)N material on a substrate by an HVPE epitaxial growth process, under low surface mobility growth conditions and for sufficient time to form a low defect density, large area, substantially crack-free (Ga, Al, In)N material having a defect density of 107 defects/cm2 or lower, wherein the defects comprise threading dislocations having a tilt angle substantially greater than 0.1 degree and the HVPE epitaxial growth process is carried out to grow said low defect density, large area, substantially crack-free (Ga, Al, In)N material to a thickness of at least 10 μm, wherein the growth of the (Ga, Al, In)N material is conducted on a substrate devoid of buffer layers or nucleation layers thereon.
- 72. A method according to claim 63, wherein the (Ga, Al, In)N material is grown on (0001) sapphire.
- 73. A method according to claim 71, wherein the (Ga, Al, In)N material is grown directly on (0001) sapphire.
- 74. A method according to claim 73, wherein the (Ga, Al, In)N material has dislocations that are angled with respect to the [0001] growth direction.
- 75. A method according to claim 63, wherein the growth process includes a first relatively lower temperature stage producing a (Ga, Al, In)N material that includes a relatively rougher growth surface and a relatively higher background carrier concentration, followed by a second relatively higher temperature stage producing a (Ga, Al, In)N material that includes a relatively smoother top surface and a relatively lower background carrier concentration in the (Ga, Al, In)N material.
- 76. A method according to claim 75, wherein the first and second stages are separated by a period of time during which the temperature is ramped from a temperature level of the first stage to a second higher temperature level of the second stage.
- 77. A method according to claim 76, wherein growth of the (Ga, Al, In)N material is continued during the period of time between the first and second stages.
- 78. A method of forming a (Ga, Al, In)N material, comprising carrying out the growth of said (Ga, Al, In)N material on a substrate by an HVPE epitaxial growth process, under low surface mobility growth conditions and for sufficient time to form a low defect density, large area, substantially crack-free (Ga, Al, In)N material having a defect density of 107 defects/cm2 or lower, wherein the defects comprise threading dislocations having a tilt angle substantially greater than 0.1 degree and the HVPE epitaxial growth process is carried out to grow said low defect density, large_area, substantially crack-free (Ga, Al, In)N material to a thickness of at least 10 μm, and removing the substrate from the (Ga, Al, In)N material.
- 79. A method according to claim 78, wherein removal of the substrate from the (Ga, Al, In)N material is carried out from a (Ga,Al,In)N material with thickness in excess of 100 μm.
- 80. A method according to claim 78, wherein removal of the substrate from the (Ga, Al, In)N material is carried out in situ in a growth reactor in which the growth process is conducted.
- 81. A method according to claim 78, wherein removal of the substrate from the (Ga, Al, In)N material is carried out ex situ with respect to the growth process.
- 82. A method according to claim 78, wherein removal of the substrate from the (Ga, Al, In)N material is carried out by an optically induced thermal separation technique.
- 83. A method according to claim 78, wherein removal of the substrate from the (Ga, Al, In)N material is carried out by mechanically rubbing off, grinding off and/or polishing off the substrate from the (Ga, Al, In)N material.
- 84. A method according to claim 78, wherein removal of the substrate from the (Ga, Al, In)N material is carried out by etching away the substrate from the (Ga, Al, In)N material.
- 85. A method according to claim 84, wherein the etching comprises wet etching.
- 86. A method according to claim 84, wherein the etching comprises dry etching.
- 87. A method according to claim 78, wherein removal of the substrate from the (Ga, Al, In)N material is carried out by a thermal fracture technique.
- 88. A method according to claim 78, wherein removal of the substrate from the (Ga, Al, In)N material is carried out by an implanted species fracture technique.
- 95. A method according to claim 63, wherein the growth of the (Ga, Al, In)N material is carried out for sufficient time to form a (Ga, Al, In)N material of sufficient thickness to eliminate cracking in (Ga, Al, In)N material grown thereon.
- 96. A method according to claim 63, wherein the growth of the (Ga, Al, In)N material is carried out for sufficient time to form a (Ga, Al, In)N material having a thickness of at least 25 μm.
- 97. A method according to claim 63, wherein the growth of the (Ga, Al, In)N material is carried out for sufficient time to form a (Ga, Al, In)N material having a thickness of at least 50 μm.
- 98. A method according to claim 63, wherein the growth of the (Ga, Al, In)N material is carried out for sufficient time to form a (Ga, Al, In)N material having a thickness of at least 100 μm.
- 99. A method according to claim 63, wherein the growth of the (Ga, Al, In)N material is carried out for sufficient time to form a (Ga, Al, In)N material having a thickness of at least 200 μm.
- 100. A method of forming a low defect density (Ga, Al, In) N material, comprising growing a (Ga, Al, In) N material on a substrate by HVPE under growth conditions yielding a (Ga, Al, In) N film in which the defects are predominantly threading dislocations that are angled with respect to the growth direction at a tilt angle substantially greater than 0.1 degree, wherein the (Ga, Al, In)N film has a defect density of 107 defects/cm2 or lower, and the HVPE is carried out to grow said (Ga, Al, In)N material to a thickness of at least 10 μm.
- 101. A method according to claim 100, comprising reacting vapor-phase (Ga, Al, In) chloride with a vapor-phase nitrogenous compound in the presence of the substrate, to grow the (Ga, Al, In) nitride layer on the substrate.
- 102. A method according to claim 101, wherein the nitrogenous compound is selected from the group consisting of ammonia, hydrazine, amines, and polyamines.
- 103. A method according to claim 101, wherein the vapor-phase (Ga, Al, In) chloride is formed by contacting vapor-phase hydrogen chloride with molten (Ga, Al, In) to yield the vapor-phase (Ga, Al, In) chloride.
- 104. A method for forming a low threading dislocation (TD) density GaN material on a substrate, in which the defects in the GaN material are predominantly threading dislocations that are angled with respect to the growth direction of the GaN material, said method comprising growing a GaN film on the substrate at low surface mobility conditions.
- 105. A method according to claim 104, wherein the growth conditions favor reduced surface mobility in one or more variables selected from the group consisting of growth temperature, ratio of precursors for vapor-phase film formation, growth pressure and growth rate.
- 106. A method according to claim 104, wherein the growth conditions favor reduced surface mobility in growth temperature.
- 107. A method according to claim 104, wherein the conditions favor reduced relative surface mobility in growth rate.
- 108. A method of growing a low threading dislocation (TD) density (Ga, Al, In) N material on a substrate, comprising depositing (Ga, Al, In)N material on the substrate by an HVPE growth process under sufficient process conditions and for sufficient time so that defects in the (Ga, Al, In) N material are predominantly threading dislocations that are angled with respect to the growth direction of the material at a tilt angle substantially greater than 0.1 degree, and the HVPE growth process is carried out to deposit said (Ga, Al, In)N material to a thickness of at least 10 μm, wherein the (Ga, Al, In)N material has a defect density of 107 defects/cm2 or lower.
- 109. A method of forming a low defect density (Ga, Al, In)N material, comprising depositing a (Ga, Al, In)N material on a substrate by an HVPE process conducted at a growth temperature in the range of from about 985° C. to about 1010° C. and associated process conditions to provide the (Ga, Al, In)N material with a dislocation defect density of 106 defects/cm2 or lower, wherein the defects comprise threading dislocations having a tilt angle substantially greater than 0.1 degree, and the HVPE process is carried out to grow said low defect density (Ga, Al, In)N material to a thickness of at least 10 μm.
- 110. A method according to claim 109, wherein the growth temperature is about 1000° C.
- 111. A method according to claim 109, wherein the growth rate of the (Ga, Al, In)N material is from about 25 micrometers to about 200 micrometers per hour.
- 112. A method according to claim 109, wherein the growth process is conducted at a pressure in the range of from about 10 to about 1000 torr.
- 113. A method according to claim 109, wherein the growth process is conducted at a pressure in the range of from about 10 to about 800 torr.
- 114. A method according to claim 109, wherein the growth rate is from about 50 to about 150 microns per hour.
- 115. A method according to claim 109, wherein the (Ga, Al, In) N material is GaN and the GaN has a purity of at least 5-9s purity.
- 116. A method according to claim 109, wherein the (Ga, Al, In) N material is GaN and the GaN has a purity of at least 7-9s purity.
- 117. A method according to claim 109, wherein the growth rate is from about 100 microns per hour to about 200 microns per hour.
- 118. An HVPE process for forming a low defect density, large area (Ga, Al, In)nitride material, comprising depositing (Ga, Al, In)nitride material on a substrate at a temperature in the range of from about 950° C. to about 1020° C., and forming a (Ga, Al, In)nitride material having a dislocation defect density of 107 defects/cm2 or lower and a surface area of at least 10 cm2, wherein the defects comprise threading dislocations having a tilt angle substantially greater than 0.1 degree and the HVPE process is carried out to grow said low defect density, large area (Ga, Al, In)nitride material to a thickness of at least 10 μm.
- 130. A method of forming a (Ga, Al, In)N material, comprising carrying out the growth of said (Ga, Al, In)N material on a substrate by an HVPE epitaxial growth process, under low surface mobility growth conditions and for sufficient time to form a low defect density, large area, substantially crack-free (Ga, Al, In)N material, wherein such low surface mobility growth conditions are established so as to generate predominately threading dislocations angled with respect to growth direction of said (Ga, Al, In)N material at a tilt angle substantially greater than 0.1 degree, wherein the (Ga, Al, In)N material has a defect density of 107 defects/cm2 or lower, and the HVPE epitaxial growth process is carried out to grow said (Ga, Al, In)N material to a thickness of at least 10 μm.
- 131. A method according to claim 130, wherein the epitaxial growth process comprises reacting vapor-phase (Ga, Al, In) chloride with a vapor-phase nitrogenous compound in the presence of the substrate, to grow the (Ga, Al, In)N material on the substrate.
- 132. A method according to claim 130, wherein the epitaxial growth process is carried out at a temperature in a range of from about 985° C. to about 1010° C.
- 133. A method according to claim 67, wherein the (Ga, Al, In)N material has a defect density below 106 defects/cm2.
- 134. A method according to claim 133, wherein the dislocations of said (Ga, Al, In)N material are predominantly angled with respect to the growth direction by a tilt angle less than about 40°.
- 135. A method according to claim 130, wherein the threading dislocations generated under such low surface mobility growth conditions are predominantly mixed-type threading dislocations.
- 136. A method according to claim 67, wherein the growth of the (Ga, Al, In)N material is conducted on a substrate devoid of buffer layers or nucleation layers thereon.
- 137. A method according to claim 130, wherein the (Ga, Al, In)N material is grown on (0001) sapphire.
- 138. A method according to claim 67, wherein the (Ga, Al, In)N material is grown directly on (0001) sapphire without any buffer or nucleation layer thereon.
- 139. A method according to claim 130, wherein the growth process includes a first relatively lower temperature stage producing a (Ga, Al, In)N material that includes a relatively rougher growth surface and a relatively higher background carrier concentration, followed by a second relatively higher temperature stage producing a (Ga, Al, In)N material that includes a relatively smoother top surface and a relatively lower background carrier concentration in the (Ga, Al, In)N material.
- 140. A method according to claim 139, wherein the first and second stages are separated by a period of time during which the temperature is ramped from a temperature level of the first stage to a second higher temperature level of the second stage.
- 141. A method according to claim 140, wherein growth of the (Ga, Al, In)N material is continued during the period of time between the first and second stages.
- 142. A method of forming a (Ga, Al, In)N material, comprising carrying out the growth of said (Ga, Al, In)N material on a substrate by an HVPE epitaxial growth process, under low surface mobility growth conditions and for sufficient time to form a low defect density, large area, substantially crack-free (Ga, Al, In)N material, wherein said low surface mobility growth conditions are established so as to generate predominantly threading dislocations angled with respect to growth direction of said (Ga, Al, In)N material at a tilt angle substantially greater than 0.1 degree, wherein said (Ga, Al, In)N material has a defect density of 107 defects/cm2 or lower, with the HVPE epitaxial growth process comprising growing said (Ga, Al, In)N material to a thickness of at least 10 μm, and subsequently removing the substrate from the (Ga, Al, In)N material.
- 143. A method according to claim 142, wherein removal of the substrate from the (Ga, Al, In)N material is carried out from a (Ga,Al,In)N material with thickness in excess of 100 μm.
- 144. A method according to claim 142, wherein removal of the substrate from the (Ga, Al, In)N material is carried out in situ in a growth reactor in which the growth process is conducted.
- 145. A method according to claim 142, wherein removal of the substrate from the (Ga, Al, In)N material is carried out ex situ with respect to the growth process.
- 146. A method according to claim 142, wherein removal of the substrate from the (Ga, Al, In)N material is carried out by an optically induced thermal separation technique.
- 147. A method according to claim 142, wherein removal of the substrate from the (Ga, Al, In)N material is carried out by mechanically rubbing off, grinding off and/or polishing off the substrate from the (Ga, Al, In)N material.
- 148. A method according to claim 142, wherein removal of the substrate from the (Ga, Al, In)N material is carried out by etching away the substrate from the (Ga, Al, In)N material.
- 149. A method according to claim 148, wherein the etching comprises wet etching.
- 150. A method according to claim 148, wherein the etching comprises dry etching.
- 151. A method according to claim 142, wherein removal of the substrate from the (Ga, Al, In)N material is carried out by a thermal fracture technique.
- 152. A method according to claim 142, wherein removal of the substrate from the (Ga, Al, In)N material is carried out by an implanted species fracture technique.
- 153. A method according to claim 130, wherein the growth of the (Ga, Al, In)N material is carried out for sufficient time to form a (Ga, Al, In)N material of sufficient thickness to eliminate cracking in (Ga, Al, In)N material grown thereon.
- 154. A method according to claim 130, wherein the growth of the (Ga, Al, In)N material is carried out for sufficient time to form a (Ga, Al, In)N material having a thickness of at least 25 μm.
- 155. A method according to claim 130, wherein the growth of the (Ga, Al, In)N material is carried out for sufficient time to form a (Ga, Al, In)N material having a thickness of at least 50 μm.
- 156. A method according to claim 130, wherein the growth of the (Ga, Al, In)N material is carried out for sufficient time to form a (Ga, Al, In)N material having a thickness of at least 100 μm.
- 157. A method according to claim 130, wherein the growth of the (Ga, Al, In)N material is carried out for sufficient time to form a (Ga, Al, In)N material having a thickness of at least 200 μm.
- 158. A method according to claim 67, wherein the low surface mobility growth conditions are characterized by at least one growth process variable selected from the group consisting of:
a growth temperature in the range of from about 950° C. to about 1010° C.; a growth pressure in the range of from about 10 to about 1000 torr; a growth rate in the range of 25 micrometers to about 200 micrometers per hour.
- 159. A method according to claim 158, wherein the low surface mobility growth conditions are characterized by a growth temperature in the range of from about 950° C. to about 1010° C.
- 160. A method according to claim 158, wherein the low surface mobility growth conditions are characterized by a growth temperature of about 1000° C.
- 161. A method according to claim 158, wherein the low surface mobility growth conditions are characterized by a growth pressure in the range of from about 10 to about 800 torr.
- 162. A method according to claim 158, wherein the low surface mobility growth conditions are characterized by a growth rate in the range of from about 50 to about 150 micrometers per hour.
- 163. A method according to claim 158, wherein the epitaxial growth process is carried out at a temperature in a range of from about 985° C. to about 1010° C.
- 164. A method according to claim 158, wherein the (Ga, Al, In)N material has a defect density below 106 defects/cm2.
- 165. A method according to claim 158, wherein the threading dislocations generated under such low surface mobility growth conditions are predominantly angled with respect to the growth direction by a tilt angle less than about 40°.
- 166. A method according to claim 158, wherein the threading dislocations generated under such low surface mobility growth conditions are predominantly mixed-type threading dislocations.
- 167. A method according to claim 158, wherein the growth of the (Ga, Al, In)N material is conducted on a substrate devoid of buffer layers or nucleation layers thereon.
- 168. A method according to claim 158, wherein the (Ga, Al, In)N material is grown on (0001) sapphire.
- 169. A method according to claim 158, wherein the (Ga, Al, In)N material is grown directly on (0001) sapphire without any buffer or nucleation layer thereon.
- 170. A method according to claim 158, wherein the growth process includes a first relatively lower temperature stage producing a (Ga, Al, In)N material that includes a relatively rougher growth surface and a relatively higher background carrier concentration, followed by a second relatively higher temperature stage producing a (Ga, Al, In)N material that includes a relatively smoother top surface and a relatively lower background carrier concentration in the (Ga, Al, In)N material.
- 171. A method according to claim 170, wherein the first and second stages are separated by a period of time during which the temperature is ramped from a temperature level of the first stage to a second higher temperature level of the second stage.
- 172. A method according to claim 171, wherein growth of the (Ga, Al, In)N material is continued during the period of time between the first and second stages.
- 173. A method according to claim 158, further comprising removing the substrate from the (Ga, Al, In)N material.
- 174. A method according to claim 173, wherein removal of the substrate from the (Ga, Al, In)N material is carried out from a (Ga,Al,In)N material with thickness in excess of 100 μm.
- 175. A method according to claim 173, wherein removal of the substrate from the (Ga, Al, In)N material is carried out in situ in a growth reactor in which the growth process is conducted.
- 176. A method according to claim 173, wherein removal of the substrate from the (Ga, Al, In)N material is carried out ex situ with respect to the growth process.
- 177. A method according to claim 173, wherein removal of the substrate from the (Ga, Al, In)N material is carried out by an optically induced thermal separation technique.
- 178. A method according to claim 173, wherein removal of the substrate from the (Ga, Al, In)N material is carried out by mechanically rubbing off, grinding off and/or polishing off the substrate from the (Ga, Al, In)N material.
- 179. A method according to claim 173, wherein removal of the substrate from the (Ga, Al, In)N material is carried out by etching away the substrate from the (Ga, Al, In)N material.
- 180. A method according to claim 179, wherein the etching comprises wet etching.
- 181. A method according to claim 179, wherein the etching comprises dry etching.
- 182. A method according to claim 173, wherein removal of the substrate from the (Ga, Al, In)N material is carried out by a thermal fracture technique.
- 183. A method according to claim 173, wherein removal of the substrate from the (Ga, Al, In)N material is carried out by an implanted species fracture technique.
- 184. A method according to claim 158, wherein the growth of the (Ga, Al, In)N material is carried out for sufficient time to form a (Ga, Al, In)N material of sufficient thickness to eliminate cracking in (Ga, Al, In)N material grown thereon.
- 185. A method according to claim 158, wherein the growth of the (Ga, Al, In)N material is carried out for sufficient time to form a (Ga, Al, In)N material having a thickness of at least 25 μm.
- 186. A method according to claim 158, wherein the growth of the (Ga, Al, In)N material is carried out for sufficient time to form a (Ga, Al, In)N material having a thickness of at least 50 μm.
- 187. A method according to claim 158, wherein the growth of the (Ga, Al, In)N material is carried out for sufficient time to form a (Ga, Al, In)N material having a thickness of at least 100 μm.
- 188. A method according to claim 158, wherein the growth of the (Ga, Al, In)N material is carried out for sufficient time to form a (Ga, Al, In)N material having a thickness of at least 200 μm.
CROSS-REFERENCE TO RELATED APPLICATIONS
[0001] This claims the priority of U.S. provisional patent application No. 60/063,249 filed Oct. 24, 1997 in the names of Robert P. Vaudo, Joan M. Redwing, and Vivek Phanse for “LOW THREADING DEFECT DENSITY (Ga, Al, In)N AND HVPE PROCESS FOR MAKING SAME. This application is also a continuation-in-part of U.S. application Ser. No. 08/984,473 filed Dec. 3, 1997 which in turn claims the priority of U.S. provisional patent application No. 60/031,555 filed Dec. 3, 1996 in the names of Robert P. Vaudo, Joan M. Redwing, Michael A. Tischler and Duncan W. Brown. This application is also a continuation-in-part of U.S. application Ser. No. 08/955,168 filed Oct. 21, 1997 in the names of Michael A. Tischler, Thomas F. Kuech and Robert P. Vaudo, which in turn is a continuation-in-part of U.S. patent application Ser. No. 08/188,469 filed Jan. 27, 1994 and issued Oct. 21, 1997 as U.S. Pat. No. 5,679,152.
Provisional Applications (2)
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Date |
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60063249 |
Oct 1997 |
US |
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60031555 |
Dec 1996 |
US |
Continuations (1)
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09179049 |
Oct 1998 |
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| Child |
10103226 |
Mar 2002 |
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Continuation in Parts (3)
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08984473 |
Dec 1997 |
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| Child |
10103226 |
Mar 2002 |
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| Parent |
08955168 |
Oct 1997 |
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| Child |
10103226 |
Mar 2002 |
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| Parent |
08188469 |
Jan 1994 |
US |
| Child |
08955168 |
Oct 1997 |
US |