Methods to deposit controlled thin layers of transition metal dichalcogenides
11447862 · 2022-09-20
Assignee
Inventors
- Anil U. Mane (Naperville, IL)
- Jeffrey W. Elam (Elmhurst, IL)
- Steven Letourneau (Naperville, IL, US)
- Elton Graugnard (Boise, ID, US)
Cpc classification
C23C16/45529
CHEMISTRY; METALLURGY
C23C16/45531
CHEMISTRY; METALLURGY
C23C16/52
CHEMISTRY; METALLURGY
C23C16/45527
CHEMISTRY; METALLURGY
International classification
C23C16/455
CHEMISTRY; METALLURGY
C23C16/30
CHEMISTRY; METALLURGY
Abstract
Transition metal dichalcogenides (TMDs) are deposited as thin layers on a substrate. The TMDs may be grown on oxide substrates and may have a tunable TMD-oxide interface.
Claims
1. A method of preparing a substrate comprising: performing an a atomic layer deposition cycle exposure for a transition metal precursor at a first deposition temperature between 50° C. and 300° C. above a sublimation temperature of the transition metal precursor; performing a b atomic layer deposition cycle exposure for a sulfur precursor at a second deposition temperature between 50° C. and 300° C. above a sublimation temperature of the sulfur precursor; performing z supercycles of the a atomic layer deposition cycle and of the b atomic layer deposition cycle; and forming a transition metal dichalcogenide coating; wherein the transition metal precursor comprises MoF.sub.6 and the sulfur precursor is H.sub.2S with the transition metal dichalcogenide being MoS.sub.2 or wherein the transition metal precursor is tetrakis(dimethylamido) hafnium or HfCl.sub.4 and the sulfur precursor is H.sub.2S, with the transition metal dichalcogenide being HfS.sub.2.
2. The method of claim 1, wherein the a cycles each comprise: a 1 second dose followed by a gas purge.
3. The method of claim 1, wherein the b cycle depositions each comprise: a 1 second dose followed by a second gas purge.
4. The method of claim 1, wherein the first deposition temperature and the second disposition temperature are the same.
5. The method of claim 1, wherein the first deposition temperature is between 100° C. and 300° C.
6. The method of claim 1, wherein the second deposition temperature is between 50° C. and 300° C.
7. The method of claim 1, further comprising, after forming the transition metal dichalcogenide: performing a c atomic layer deposition cycle of a second transition metal precursor at a third deposition temperature between 100° C. and 300° C.; performing a d atomic layer deposition cycle of a second reducing precursor at a fourth deposition temperature between 100° C. and 300° C., and performing y supercycles of the c atomic layer deposition cycle and of the d atomic layer deposition cycle, forming a transition metal coating on the transition metal dichalcogenide.
8. A method of forming a transition metal oxide and transition metal dichalcogenide stack comprising: exposing a first transition metal precursor at a first deposition temperature between 50° C. and 400° C.; exposing an oxidizing precursor at a second deposition temperature between 50° C. and 400° C.; depositing a layer of transition metal oxide; exposing a second transition metal precursor at a third deposition temperature between 50° C. and 400° C.; exposing a sulfur precursor at a fourth deposition temperature between 50° C. and 400° C.; and depositing a transition metal dichalcogenide on the transition metal oxide; wherein the second transition metal precursor is tetrakis(dimethylamido) hafnium or HfCl.sub.4 and the sulfur precursor is H.sub.2S, with the transition metal dichalcogenide being HfS.sub.2.
9. The method of claim 8, wherein the first transition metal precursor and the second transition metal precursor are different.
10. The method of claim 8, wherein the first transition metal precursor and the second transition metal precursor are the same.
Description
BRIEF DESCRIPTION OF DRAWINGS
(1) The foregoing and other features of the present disclosure will become more fully apparent from the following description and appended claims, taken in conjunction with the accompanying drawings. Understanding that these drawings depict only several implementations in accordance with the disclosure and are therefore, not to be considered limiting of its scope, the disclosure will be described with additional specificity and detail through use of the accompanying drawings.
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(23) Reference is made to the accompanying drawings throughout the following detailed description. In the drawings, similar symbols typically identify similar components, unless context dictates otherwise. The illustrative implementations described in the detailed description, drawings, and claims are not meant to be limiting. Other implementations may be utilized, and other changes may be made, without departing from the spirit or scope of the subject matter presented here. It will be readily understood that the aspects of the present disclosure, as generally described herein, and illustrated in the figures, can be arranged, substituted, combined, and designed in a wide variety of different configurations, all of which are explicitly contemplated and made part of this disclosure.
DETAILED DESCRIPTION OF VARIOUS EMBODIMENTS
(24) Embodiments described herein relate generally to formation of TMDs by ALD. ALD offers the best combination of a layer-by-layer growth of the material with highest conformality and integration with other oxides such as high-K dielectrics (e.g., Al.sub.2O.sub.3, HfO.sub.2, etc.) to realize 3D heterojunctions. The ability to control the synthesis of films over large areas will be important for future large-scale manufacturing for integrating into complex device structures.
(25) ALD is a vapor-phase, thin film deposition method based on alternating self-limiting surface reactions. ALD typically uses gaseous precursors to react with the exposed surface (of a substrate, then of preceding layers). The precursors are selected such that the first precursor binds to the substrate and then is modified by reaction with the second precursor to leave the desired element or compound. The precursor may be applied as a continuous exposure for a period of time or may be applied as micropulses of very short duration extending over a period of time. A purge gas may be used to clear the reaction chamber of a precursor, both to ensure termination of the reaction and prevent undesired reactions with the other precursor is injected. The nature of ALD lends itself to be a unique deposition method capable of precise control over thin film thickness and stoichiometry, as well as the ability to deposit conformal coatings over high surface area morphologies.
(26) TMD can be represented as MX.sub.2 where M is a transition metal and X is a chalcogenide. TMDs have a layered structure where each layer consists of an X-M-X unit. TMD crystals are typically described as having trigonal or octahedral prismatic coordination to help describe the material in a single layer, where each M atom has six X atoms forming a hexagon above and below it. These atomic trilayers feature strong in-plane covalent bonding but weak van der Waals bonding between layers. This dichotomy of bonding characteristics facilitates the synthesis and isolation of single layer TMDs. MoS.sub.2 in the bulk crystalline form has three stable phases under standard conditions: 2H, 3R and 1T.
(27) One embodiment relates to a method of forming TMDs on a substrate via ALD by performing a atomic layer deposition exposures of a transition metal precursor at a first deposition temperature between 100° C. and 300° C. and b) atomic layer deposition exposures of a sulfur precursor at a second deposition temperature between 50° C. and 300° C., and forming a transition metal dichalcogenide coating on the substrate. It should be appreciated that the ALD TMD growth, as well as optimal temperature, will vary based on the precursor sublimation temperature and the stability. Deposition temperature is based on thermodynamics of the precursors reaction at elevated temperature. In one embodiment, the temperature for deposition is between 100° C. and 400° C. In one embodiment, the growth temperature range for the ALD process is 50° C.-300° C.
(28) The a and b exposures constitute one ALD cycle. The TMD film can be made thicker by performing additional ALD cycles. The resultant deposited material may be further processed by annealing. In one embodiment the annealing temperature range for the ALD process is 400° C.-800° C.
(29) ALD cycle duration will be based on precursor vapor pressure and its subsequent saturation behavior and the depositing object surface area. For example, in one embodiment using a 300 mm Si wafer substrate, one ALD cycle duration can be (MoF.sub.6—N.sub.2—H.sub.2S—N.sub.2)=(1-10-1-10 s). However, using porous glass (8″×8″) as a substrate with surface area ˜10 m.sup.2, one ALD cycle duration can be (MoF.sub.6—N.sub.2—H.sub.2S—N.sub.2)=(10-30-10-30 s).
(30) The general recipe for ALD will be based on many factors known to those skilled in the art, such as the nature of ALD cycles, precursor functional group, vapor pressure, substrate temperature, reactor geometry, ALD reaction chamber pressure, and, most importantly, the combination of precursors. CVD-type precursors may not be compatible due to the difference in the processes. For example, MoS.sub.2 using MoF.sub.6—H.sub.2S by ALD is feasible but MoS.sub.2 using (Mo(CO.sub.5)—H.sub.2S is not feasible by ALD (but could be for CVD).
(31) For example, ALD MoS.sub.2 can grow at 100° C. using MoF.sub.6—H.sub.2S. In a second example, ALD HfS.sub.2 can grow at 150° C. with TDMA-Hf and H.sub.2S. HfS.sub.2 can also be prepared at >200° C. with HfCl.sub.4 and H.sub.2S. In the HfCl.sub.4 precursor case, the sublimation temperature for HfCl.sub.4 is 150° C.; therefore, the deposition temperature must be higher to avoid condensation of the HfCl.sub.4.
(32) Mixed TMDs can be prepared by alternating between the ALD chemistries of the component materials. For instance, mixed MoS.sub.2—HfS.sub.2 can be prepared by performing c MoS.sub.2 ALD cycles followed by d HfS.sub.2 cycles. The composition of the film is dictated by the c/d ratio, while the thickness is determined by the total cycle number c+d.
(33) Doped TMDs can be prepared by interposing one or more cycles of a second TMD material during the process of growing a first TMD material. For instance, Mg-doped HfS.sub.2 can be prepared by interrupting the ALD chemistry for HfS.sub.2 (TDMA-Hf/H.sub.2S) and performing one or more cycles of Mg(Cp).sub.2/H.sub.2S, and then returning to the HfS.sub.2 chemistry. The doping level of Mg is controlled by the ratio of MgS.sub.2 cycles to the total number of TMD cycles, and the thickness is determined by the total number of ALD TMD cycles.
(34) Doping of the TMD can tune the bandgap and other properties. For example, MoS.sub.2 can be doped with W using tungsten hexafluoride (WF.sub.6) to form a compound described as WxMoyS.sub.2. In one embodiment, the doping is accomplished by selection of a compatible precursor (e.g., MoF.sub.6 and H.sub.2S for MoS.sub.2 growth and WF.sub.6 for dopant, and vice versa), which can give good material and only F can be impurity. The dopant precursor may be selected such that the waste material after ALD reaction includes the same elements or materials as for the primary ALD reaction (MoS.sub.2 formation, in one example). In other cases, one can deposit MoS.sub.2 using MoF.sub.6 and H.sub.2S and then dope W with other precursor (e.g., W(CO).sub.5); in that case, W-doped MoS.sub.2 material can deposit but now we may have F and C as impurity.
(35) In particular, described herein are two examples of TMDs deposited by ALD: MoS.sub.2 ALD using MoF.sub.6 and H.sub.2S and HfS.sub.2 using Hf(TMAH).sub.4 and H.sub.2S. Notably, while CVD processes have used a wired range of precursors, such cannot be expected to simply be usable directly in ALD. As those in the art will appreciate, CVD relies upon a reaction of two precursors in their gaseous or vapor form with the resultant material deposited on the surface of the underlying substrate. In contrast, ALD proceeds via the saturated surface reactions of first one precursor and then the other.
(36) MoF.sub.6 is reduced readily by both Si and H.sub.2:
2MoF.sub.6(g)+3Si(s).fwdarw.2Mo(s)+3SiF.sub.4(g) (1)
MoF.sub.6(g)+3H.sub.2(g).fwdarw.Mo(s)+6HF(g) (2)
The free energy changes for these reactions are −450 and −237 kJ/mol Mo, respectively, at 200° C., indicating that both reactions are thermodynamically highly favorable. In a previous report of Mo layers by ALD using MoF.sub.6 and disilane, the authors reported self-limiting behavior but measured a higher than predicted growth per cycle which they attributed to CVD (i.e., MoF.sub.6.fwdarw.Mo+3F.sub.2) promoted by local, transient heating from the very exothermic ALD surface reactions.
(37) In, examples described below, x-ray amorphous molybdenum sulfide films were grown by ALD using MoF.sub.6 and H.sub.2S. In situ QCM measurements revealed that both half-reactions are self-limiting at 200° C. Crystalline films were achieved after annealing at 350° C. in a hydrogen environment. The growth rate could be enhanced using diethyl zinc without changing the optical band gap of the material.
EXAMPLES
(38) ALD of MoS.sub.2
(39) In one experimental embodiment, a MoS.sub.2 coating was fabricated using the parameters listed in Table 1 below.
(40) TABLE-US-00001 TABLE 1 Parameters Values Precursor MoF.sub.6 and H.sub.2S Number of ALD cycles up to 1000 ALD cycles duration (MoF.sub.6—N.sub.2—H.sub.2S—N.sub.2) Optimized (1-5-1-5 s) Deposition temperature 200° C. Purge gas (N.sub.2) flow 300 sccm Thermal annealing (1Torr H.sub.2) 350° C.
(41) MoS.sub.2 ALD was performed using a custom viscous flow, hot-walled reactor, which was detailed previously. Deposition was performed on ˜1″×1″ coupons of Si with the native oxide intact and fused silica. The reactor temperature was maintained at 200° C. for all samples. During growth, ultra-high purity N.sub.2 (99.999%) was adjusted so the system process pressure was approximately 1 Torr. Molybdenum hexafluoride (MoF.sub.6 98%, Sigma Aldrich) and hydrogen disulfide (H.sub.2S 99.5%, Matheson Trigas) were sequentially pulsed into the reactor with purges of N.sub.2 between each exposure. The MoF.sub.6 and H.sub.2S partial pressures were 20 mTorr and 150 mTorr during dosing of the respective precursor. The delivery pressure in the reactor for both precursors was regulated with both an inline 200 μm aperture (Lenox Laser) and a metering valve. Both gases are extremely dangerous and special precautions are needed due to the flammability/toxicity of H.sub.2S and the corrosive nature of MoF.sub.6. The ALD timing can be described as t.sub.1-t.sub.2-t.sub.3-t.sub.4, where t.sub.1 and t.sub.3 are the MoF.sub.6 and H.sub.2S exposure times, respectively, and t.sub.2 and t.sub.4 are the corresponding purge times, with all times in seconds (s). For the MoS.sub.2 growth, t.sub.1 and t.sub.3 were both 1 s, while the purge times (t.sub.2 and t.sub.4) were kept at 5 s. In some experiments, the samples were annealed in situ after deposition on a temperature-controlled hot stage. The sample annealing was performed in ultrahigh purity hydrogen at 350° C. holding for 15 min. The samples were then cooled quickly back to room temperature. In addition to the binary chemistry of MoF.sub.6 and H.sub.2S, the MoS.sub.2 ALD was promoted/doped with ZnS using two successive ZnS ALD cycles composed of DEZ (99% Sigma Aldrich) and H.sub.2S.
(42) Experiments deposited MoS.sub.2 on variety of substrates, such as Silicon, SiO.sub.2, polyamide, quartz, anodic aluminum oxide (AAO), trench wafer, ITO, W, Mo, TiN, etc. This ALD grown MoS.sub.2 layers was characterized by various method and confirms the desire material growth.
(43) The MoS.sub.2 ALD was investigated by in situ QCM measurements using a modified Maxtek Model BSH-150 sensor head. An RC-cut quartz crystal (Phillip Technologies) with an alloy coating was used as the sensor due to its broad temperature range. To prevent deposition on the back side of the crystal, silver paste was used to seal the crystal and sensor head. A backside N.sub.2 purge was adjusted to approximately 0.5% of the process pressure.
(44) XPS measurements were carried out at the KECKII/NUANCE facility at Northwestern University on a Thermo Scientific ESCALAB 250 Xi (Al Kα radiation, hv=S5 1486.6 eV) equipped with an electron flood gun. Lower resolution survey scans and high resolution scans of the 3d, 2s, and 2p electron energies were performed. The XPS data were analyzed using THERMO ADVANTAGE 5.97 software, and all spectra were referenced to the C1s peak (284.8 eV). Peak deconvolution in the high-resolution spectra (Mo 3d, S 2p) was performed using the Powell fitting algorithm with 30% mixed Gaussian-Lorentzian fitted peaks in all cases. Fitting procedures were based on constraining the spinorbit split doublet peak areas and FWHM according to the relevant core level (e.g., 3d.sub.5/2 and 3d.sub.3/2 is constrained to 3:2 peak area).
(45) Raman spectroscopy (inVia, Renishaw) was used to probe the layered structure. The E.sub.2g and A.sub.1g vibrational modes arise from the in-plane and out-of-plane modes, respectively. Measurements were performed in reflection using an excitation wavelength of 514 nm on all samples. To prevent sample damage, a neutral density filter of 5%-10% transmission was used. A D2 Phaser x-ray diffractometer (XRD) (Bruker) using a Cu Kα source in Bragg-Brentano geometry was used to probe the crystallinity and crystal structure of the MoS.sub.2. A J. A. Woollam, Inc. α-SE Ellipsometer (Lincoln, Nebr.) was used to measure the thickness of the bulk films using a Cauchy model.
(46) The optical properties of the ALD molybdenum sulfide were measured using a Cary 5000 spectrophotometer (Varian) in transmission mode on films deposited on fused silica substrates. Kapton tape was placed on the backside of the quartz substrates during ALD and removed prior to measurement to mask off the region probed by the Cary 5000 beam. Prior to each measurement, a background reference was recorded to ensure accuracy. Linear regression of Tauc-plots was used to determine the optical band-gap of the films.
(47) Thermodynamic calculations (HSC Chemistry, Outotec Oy) of the Gibbs free energies of reaction (ΔG) were performed to evaluate possible chemical reactions occurring during the molybdenum sulfide ALD. Two plausible chemical pathways were identified: direct and indirect. In the direct pathway, MoF.sub.6 and H.sub.2S react to form MoS.sub.2, HF, and elemental S (Eq. (3)), with ΔG=−379 kJ/mol at 200° C. In the indirect pathway, the initial solid-phase product is MoS.sub.3 (Eq. (4)), with ΔG=−402 kJ/mol at 200° C. Subsequent H.sub.2 reduction (Eq. (5)) yields MoS.sub.2, with ΔG=−24 kJ/mol at 350° C. We compute ΔG at 350° C. for Eq. (5) to match the experimental conditions used in the postdeposition annealing. We note that the indirect pathway has a greater thermodynamic driving force (ΔG=−426 kJ/mol) compared to the direct pathway (ΔG=−379 kJ/mol). Moreover, the direct pathway might have a larger activation energy given the requirement for Mo reduction (+6 to +4) in Eq. (3), and so the indirect pathway might be kinetically favored as well. These mechanistic considerations will come into play later in our data analysis.
MoF.sub.6(g)+3H.sub.2S(s).fwdarw.MoS.sub.2(s)+6HF(g)+S(s) (3)
MoF.sub.6(g)+3H.sub.2S(s).fwdarw.MoS.sub.3(s)+6HF(g) (4)
MoS.sub.3(s)+H.sub.2(g).fwdarw.MoS.sub.2(s)+H.sub.2S(g) (5)
(48) Initial QCM studies were performed to probe the degree of self-limitation for the MoF.sub.6 and H.sub.2S half-reactions.
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(50) The data in
(51) The relative mass changes produced by the MoF.sub.6 and H.sub.2S exposures can be used to evaluate the molybdenum sulfide growth mechanism. If we assume that the molybdenum sulfide ALD proceeds via the direct route (Eq. (3)) and, furthermore, that the sulfur product sublimes from the surface, then we can propose the following surface reactions:
(SH)*.sub.x+MoF.sub.6(g).fwdarw.(S).sub.xMoF*.sub.(6-x)+xHF(g) (6)
(S).sub.xMoF*.sub.(6-x)+3H.sub.2S(g).fwdarw.S.sub.2Mo(SH)*.sub.x+S(s)+(6−x)HF(g) (7)
where surface species are designated with “*,” and all other species are in the gas phase. In Eq. (6), MoF.sub.6 reacts with x surface thiol (SH) groups liberating x HF molecules, so that (6−x) F atoms remain bound to the Mo. In Eq. (7), the new surface reacts with H.sub.2S to release the remaining (6−x) F atoms as HF and solid S. We hypothesize sulfur subsequently becomes a volatile species, probably in the form of S.sub.8, while the surface has the newly formed MoS.sub.2 species and is terminated with x SH groups so that the original surface functionality is restored. We note that the hypothesis of S sublimation is reasonable given that the vapor pressure of S is ˜2 Torr at 200° C. We can define the QCM step ratio as R=Δm.sub.A/Δm, where Δm.sub.A is the mass change from reaction Eq. (6) and Δm is the mass change for one complete ALD cycle minus the sulfur species we assumed has entered the gas phase after the reaction. Given the atomic weights of the surface species, we can write
R=Δm.sub.A/Δm=(210−20x)/160 (8)
(52) The average step ratio from the QCM data in
(53) Alternatively, the molybdenum sulfide ALD may proceed via the indirect route (Eq. (4)), which suggests the following half-reactions:
(SH)*.sub.x+MoF.sub.6(g).fwdarw.(S).sub.xMoF*.sub.(6-x)+xHF(g) (9)
(S).sub.xMoF*.sub.(6-x)+3H.sub.2S(g).fwdarw.S.sub.3Mo(SH)*.sub.x+(6−x)HF(g) (10)
These reactions are identical to Eqs. (6) and (7), with the exception that all of the S remains on the surface and the ALD film has the composition MoS.sub.3. Eqs. (9) and (10) yield the following QCM mass ratio:
R=ΔM.sub.A/ΔM=(210−20x)/192 (11)
(54) Eq. (11) predicts R=1.09 for x=0, and R=0.47 for x=6. In other words, there is no x value that yields the experimental QCM step ratio R=1.32(±0.05), implying that the indirect pathway (Eq. (4)) is not correct. Given that the QCM data are consistent with the direct pathway (Eq. (3)), then a plausible interpretation for the gradual mass loss during the MoF.sub.6 purge time is the slow sublimation of S from the surface.
(55) Next, the growth rate and physical properties of the deposited TMD coating was investigated.
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(57) A series of films were deposited on silicon and fused silica substrates using the 1-5-1-5 timing sequence at 200° C., varying the number of ALD cycles between 100 and 1000. The thicknesses of the films deposited on silicon were determined using spectroscopic ellipsometry, and these data are shown as the solid symbols in
(58) One explanation for this phenomenon can be found in the SEM image for the 600 ALD cycle film on silicon shown in
(59) Raman spectroscopy is a common method for identifying and characterizing MoS.sub.2.
(60) Pre-annealed samples showed an amorphous film when measured by XRD; however, after annealing, MoS.sub.2 could be seen, featuring the (002) reflection, which arises from the layered structure. The XRD data from MoS.sub.2 are consistent with the Inorganic Crystal Structure Database PDF 01-073-1508 for the interplanar spacing.
(61) XPS measurements were performed on both the as deposited films and the films annealed in H.sub.2 to investigate the chemical composition. These films were prepared using 600 ALD cycles with a thickness of 45 nm.
(62) High-resolution XPS data from the Mo 3d and S 2p regions before and after H.sub.2 anneal are shown in
(63) TABLE-US-00002 TABLE 2 Atomic percentages as determined by XPS. Sample Mo S F O As-deposited 34.03 37.61 4.37 16.2 Annealed 36.54 48.9 1.22 12.7
(64) To summarize, XRD suggests that the as-deposited film is amorphous whereas the SEM image shows what appear to be nanocrystals. It is likely that the diffraction peaks from these nanocrystals are too weak or broad to be detected by our XRD. The Raman measurements do not indicate crystalline MoS.sub.2 as-deposited, and this may result from the residual F detected in the films by XPS. Finally, XPS indicates predominantly Mo(IV), and this agrees with the in situ QCM measurements that suggested MoS.sub.2 is the reaction product.
(65) To measure the optical properties of the films, we used fused silica substrates that were masked with Kapton tape preventing deposition from occurring on one side. This process simplified the optical measurements since the beam was only interacting with a single film.
(66) Further, an average steady state growth rather was observed.
(67) We have shown that when using MoF.sub.6 and H.sub.2S as ALD precursors, self-limiting growth of x-ray amorphous MoS.sub.2 is attainable. Two routes of growth were proposed: indirect (MoS.sub.3) and direct (MoS.sub.2). The MoS.sub.3 route is thermodynamically favorable; however, QCM measurement showed that the direct route was the most plausible route. Moreover, XPS data confirmed the as-deposited films were MoS.sub.2. While molybdenum oxide was present, this was attributed to air exposure of the samples upon removal from the reactor at elevated temperature. After hydrogen annealing, crystalline MoS.sub.2 x-ray peaks and Raman peaks were visible.
(68) Enhancement of MoS.sub.2 ALD Using ZnS
(69) As previously discussed, WS.sub.2 ALD using WF.sub.6 and H.sub.2S can be accelerated by periodically dosing DEZ and H.sub.2S to form a monolayer of ALD ZnS. To explore whether this same phenomenon occurs during MoS.sub.2 ALD using MoF.sub.6 and H.sub.2S, we performed in-situ QCM measurements.
(70) Additional details can be gained from
Zns+MoF.sub.6(g).fwdarw.ZnF.sub.2+MoSF.sub.4(g)+H.sub.2S (12)
(71) This reaction produces only a 6 amu mass change. Although very little is known about MoSF.sub.4, the analogous reaction with ZnO to form ZnOF.sub.4 is thermodynamically favorable (−116 kJ/mol at 200° C.), and the ZnOF.sub.4 is highly volatile (>1000 Torr at 200° C.). This etching reaction would explain the ZnF.sub.2 residue in the previous papers. Additional in-situ measurements including quadrupole mass spectrometry to identify the gas phase products and Fourier transform infrared (FTIR) absorption spectroscopy to evaluate the surface functional groups directing the surface reactions would help to understand better the surface chemistry for the ZnS—MoS.sub.2 ALD.
(72) Similar to the WS.sub.2 accelerated growth on ZnS, DEZ substitution of MoF.sub.6 pulses accelerated the MoS.sub.2 growth. Our QCM measurements suggest that an etching reaction involving volatile MoSF.sub.4 species may occur and could explain earlier reports of ZnF.sub.2 residues in WS.sub.2. This work offers an alternative halogen-based process for carbon-free atomic layer deposition of MoS.sub.2 at relatively low temperatures.
(73) ALD of Other TMD Materials
(74) In a further experiments, other TMD materials were synthesized, such as MgS2 using Mg(Cp).sub.2 and H.sub.2S and HfS2 using Hf (TMAH)4 and H.sub.2S. The ALD experimental conditions are shown in Table 3. The precursor dose and purge times are understood by those skilled in the art to be equipment-specific, and the values below were selected because they provided self-limiting ALD on the ALD tool used for these measurements.
(75) TABLE-US-00003 TABLE 3 No. Parameters Values for MgS.sub.2 Values for HfS.sub.2 1 Precursor Mg(Cp).sub.2 and H.sub.2S Hf (TMAH)4 and H.sub.2S 2 ALD cycles Optimized Optimized duration (metal (1-5-1-5 s) (1-5-1-5 s) precursor —N.sub.2—H.sub.2S—N.sub.2) 3 Deposition 200° C. 200° C. temperature 4 Purge gas (N.sub.2) 300 sccm 300 sccm flow 5 Thermal annealing 350° C. (1Torr H.sub.2)
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(78) The similar ALD growth methodology can be apply to the other layer structure materials using transition metals (Mo, W, Cr, Hf, Zr, Co, Pt, V, Ti, Ta, Nb, or Lathanides elements and a chalcogen (S, Se, Te)). For example, one precursor for Mo is MoF.sub.6 and one precursor for Hf is halfnium etrakis(dimethylamido)hafnium(IV). Thus, although different precursors may be used, the common aspect for the precursors is chalcogen precursor S. It is believed that having common chalcogen-rich surface for subsequent chemistry will help the next layer of material to grow, preferably with the with least nucleation delay.
(79) The metal precursors can be halides, amides, cyclopentadienyl (Cp) compounds, substituted Cp compounds, alkyls, carbonyls, alkoxydes, or heteroleptic compounds containing mixtures of these various ligands. The chalcogenide can be a hydride, amide, tris-methyl silyl amide, alkyl, or a mixture of these ligands.
(80) Compatible Deposition of Mo and MoS.sub.2
(81) Another concern for suitable TMD material on large-scale device integration is a suitable metal contact to the TMD layer. This issue can be deal with using metal Mo deposition on MoS.sub.2 layer with clean interface. To demonstrate this, we have used ALD Mo and ALD MoS.sub.2 on top of each other. The ALD experimental parameters are given in table below. It is understood by those skilled in the art that the ALD timings are instrument specific, the number of ALD cycles can be varied to suit the application, and the temperature for the metal can be varied within the ALD window for the Mo ALD. The range of MoS.sub.2 temperatures is given above.
(82) In one embodiment, ALD of Mo and ALD MoS.sub.2 are process compatible due to use of same the same precursor for both growing metallic Mo and MoS.sub.2, for example MoF.sub.6. In addition, deposition temperature can be same or different for MoS.sub.2 and Mo growth. Table 4 shows one set of parameters for the example embodiments of MoS.sub.2 deposited and then coated with Mo by ALD:
(83) TABLE-US-00004 TABLE 4 No. Parameters Values for Mo Values for MoS.sub.2 1 Precursor MoF.sub.6 and Si.sub.2H.sub.6 MoF.sub.6 and H.sub.2S 2 ALD cycles duration (MoF.sub.6—N.sub.2—Si.sub.2H.sub.6—N.sub.2) (MoF.sub.6—N.sub.2—H.sub.2S—N.sub.2) Optimized (1-5-1-5 s) Optimized (1-5-1-5 s) 3 Deposition temperature 200° C. 200° C. 4 Purge gas (N.sub.2) flow 300 sccm 300 sccm 5 Thermal annealing (1Torr H.sub.2) Optional (350° C.)
(84) QCM data was gathered for the resultant component. As seen in
(85) It is clear that from
(86) Etching of MoS.sub.2
(87) Precisely controlled removal of thin film layers is very essential for next generation high density 3D devices fabrication. There are several ways one can perform the etching the materials. For example: A layer-by-layer etching [Atomic Layer Etching (ALEt), very precise but slow] Chemical vapor etching (CVE) [aggressive but, if controlled, fast and economical] Layer(s)-by-layer(s) etching [moderate etch rate and fast, as well as economical]
(88) As 2D-layered TMD materials are advantageous for next generation microelectronics and to integrate TMDs into 3D devices on larger scale, it is important to have both 3D conformal growth and etch process capabilities. For example, ALD is suitable for growing precisely and highly conformally materials on high aspect ratio 3D structures, whereas a well-controlled ALEt is very much suitable for etching (removing) material conformally and precisely from the 3D structure.
(89) Therefore, next we demonstrated the ALEt of MoS.sub.2 which is unique way of etching the MoS.sub.2. The developed method is very economical, well controlled, and can etch MoS.sub.2 in atomic layer-by-layer removal manner. Further, the ALEt recipe that we have used here is based on the MoF.sub.6—H.sub.2O process. This means we can grow ALD MoS.sub.2 using MoF.sub.6 and H.sub.2S (as discussed earlier in
(90)
(91)
(92)
(93)
(94)
(95) FTIR is an excellent surface sensitive technique to further investigate and monitor the growth of ALD films. Performing the technique in situ allows for the investigation of how the surface species changes after each ALD half cycle. Performing the same experiment as in
(96)
(97) Finally,
DEFINITIONS
(98) As used herein, the singular forms “a”, “an” and “the” include plural referents unless the context clearly dictates otherwise. Thus, for example, the term “a member” is intended to mean a single member or a combination of members, “a material” is intended to mean one or more materials, or a combination thereof.
(99) As used herein, the terms “about” and “approximately” generally mean plus or minus 10% of the stated value. For example, about 0.5 would include 0.45 and 0.55, about 10 would include 9 to 11, about 1000 would include 900 to 1100.
(100) It should be noted that the term “exemplary” as used herein to describe various embodiments is intended to indicate that such embodiments are possible examples, representations, and/or illustrations of possible embodiments (and such term is not intended to connote that such embodiments are necessarily extraordinary or superlative examples).
(101) The terms “coupled,” “connected,” and the like as used herein mean the joining of two members directly or indirectly to one another. Such joining may be stationary (e.g., permanent) or moveable (e.g., removable or releasable). Such joining may be achieved with the two members or the two members and any additional intermediate members being integrally formed as a single unitary body with one another or with the two members or the two members and any additional intermediate members being attached to one another.
(102) It is important to note that the construction and arrangement of the various exemplary embodiments are illustrative only. Although only a few embodiments have been described in detail in this disclosure, those skilled in the art who review this disclosure will readily appreciate that many modifications are possible (e.g., variations in sizes, dimensions, structures, shapes and proportions of the various elements, values of parameters, mounting arrangements, use of materials, colors, orientations, etc.) without materially departing from the novel teachings and advantages of the subject matter described herein. Other substitutions, modifications, changes and omissions may also be made in the design, operating conditions and arrangement of the various exemplary embodiments without departing from the scope of the present invention.
(103) While this specification contains many specific implementation details, these should not be construed as limitations on the scope of any inventions or of what may be claimed, but rather as descriptions of features specific to particular implementations of particular inventions. Certain features described in this specification in the context of separate implementations can also be implemented in combination in a single implementation. Conversely, various features described in the context of a single implementation can also be implemented in multiple implementations separately or in any suitable subcombination. Moreover, although features may be described above as acting in certain combinations and even initially claimed as such, one or more features from a claimed combination can in some cases be excised from the combination, and the claimed combination may be directed to a subcombination or variation of a subcombination.