An apparatus for growing semiconductor wafers, in particular of silicon carbide, wherein a chamber houses a collection container and a support or susceptor arranged over the container. The support is formed by a frame surrounding an opening accommodating a plurality of arms and a seat. The frame has a first a second surface, opposite to each other, with the first surface of the frame facing the support. The arms are formed by cantilever bars extending from the frame into the opening, having a maximum height smaller than the frame, and having at the top a resting edge. The resting edges of the arms define a resting surface that is at a lower level than the second surface of the frame. The seat has a bottom formed by the resting surface.

Provided is a SiC chemical vapor deposition apparatus including: a furnace body inside of which a growth space is formed; and a placement table which is positioned in the growth space and has a placement surface on which a SiC wafer is placed, in which the furnace body comprises a first hole which is positioned on an upper portion which faces the placement surface and through which a raw material gas is introduced into the growth space, a second hole which is positioned on a side wall of the furnace body and through which a purge gas flows into the growth space, a third hole which is positioned on the side wall of the furnace body at a lower position than the second hole and discharges the gases in the growth space, and a protrusion which is protrudes towards the growth space from a lower end of the second hole to adjust a flow of the raw material gas.

Provided is a SiC chemical vapor deposition apparatus including: a furnace body inside of which a growth space is formed; and a placement table which is positioned in the growth space and has a placement surface on which a SiC wafer is placed, in which the furnace body comprises a first hole which is positioned on an upper portion which faces the placement surface and through which a raw material gas is introduced into the growth space, a second hole which is positioned on a side wall of the furnace body and through which a purge gas flows into the growth space, a third hole which is positioned on the side wall of the furnace body at a lower position than the second hole and discharges the gases in the growth space, and a protrusion which is protrudes towards the growth space from a lower end of the second hole to adjust a flow of the raw material gas.

A method for producing a p-type 4H—SiC single crystal includes sublimating a nitrided aluminum raw material and a SiC raw material. Further, there is a stacking of a SiC single crystal, which is co-doped with aluminum and nitrogen, on one surface of a seed crystal.

A method for producing a p-type 4H—SiC single crystal includes sublimating a nitrided aluminum raw material and a SiC raw material. Further, there is a stacking of a SiC single crystal, which is co-doped with aluminum and nitrogen, on one surface of a seed crystal.

A process for manufacturing a composite structure comprises: a) providing an initial substrate made of monocrystalline silicon carbide, b) epitaxially growing a monocrystalline silicon carbide donor layer on the initial substrate to form a donor substrate 111, c) implanting ions into the donor layer to form a buried brittle plane defining the the donor layer, d) depositing, using liquid injection-chemical vapor deposition at a temperature below 1000° C., a carrier layer on the donor layer, the carrier layer comprising an at least partially amorphous SiC matrix, e) separating the donor substrate along the brittle plane to form an intermediate composite structure comprising the donor layer on the carrier layer f) heat treating the intermediate composite structure at a temperature of between 1000° C. and 1800° C. to crystallize the carrier layer and form the polycrystalline carrier substrate, and g) applying mechanical and/or chemical treatment(s) of the composite structure.

A process for manufacturing a composite structure comprises: a) providing an initial substrate made of monocrystalline silicon carbide, b) epitaxially growing a monocrystalline silicon carbide donor layer on the initial substrate to form a donor substrate 111, c) implanting ions into the donor layer to form a buried brittle plane defining the the donor layer, d) depositing, using liquid injection-chemical vapor deposition at a temperature below 1000° C., a carrier layer on the donor layer, the carrier layer comprising an at least partially amorphous SiC matrix, e) separating the donor substrate along the brittle plane to form an intermediate composite structure comprising the donor layer on the carrier layer f) heat treating the intermediate composite structure at a temperature of between 1000° C. and 1800° C. to crystallize the carrier layer and form the polycrystalline carrier substrate, and g) applying mechanical and/or chemical treatment(s) of the composite structure.

The present invention relates to a susceptor including a substrate including a carbon material and having one main surface on which a silicon water is to be placed, and another main surface facing the one main surface, in which an entire surface of the substrate is covered with a thin film including silicon carbide, the one main surface has an emissivity variation of 3% or less, and a ratio of an average emissivity between the one main surface and the another main surface facing the one main surface is from 1:1 to 1:0.8.

In a case where a detector is positioned in a [11-20] direction, and where a first measurement region including a center of a main surface is irradiated with an X ray in a direction within ±15° relative to a [−1-120] direction, a ratio of a maximum intensity of a first intensity profile is more than or equal to 1500. In a case where the detector is positioned in a direction parallel to a [−1100] direction, and where the first measurement region is irradiated with an X ray in a direction within ±6° relative to a [1-100] direction, a ratio of a maximum intensity of a second intensity profile is more than or equal to 1500. An absolute value of a difference between maximum value and minimum value of energy at which the first intensity profile indicates a maximum value is less than or equal to 0.06 keV.

In a case where a detector is positioned in a [11-20] direction, and where a first measurement region including a center of a main surface is irradiated with an X ray in a direction within ±15° relative to a [−1-120] direction, a ratio of a maximum intensity of a first intensity profile is more than or equal to 1500. In a case where the detector is positioned in a direction parallel to a [−1100] direction, and where the first measurement region is irradiated with an X ray in a direction within ±6° relative to a [1-100] direction, a ratio of a maximum intensity of a second intensity profile is more than or equal to 1500. An absolute value of a difference between maximum value and minimum value of energy at which the first intensity profile indicates a maximum value is less than or equal to 0.06 keV.