APERIODIC MULTILAYER STRUCTURES

Abstract

An aperiodic multilayer structure (2, 2′) comprising a plurality of alternating layers of a first (4, 4′) and a second (6, 6′) material and a capping layer (10, 10′) covering these alternating layers, wherein the structure (2, 2′) is characterized in that the thickness of the alternating layers chaotically varies in at least a portion of said structure (2, 2′). The invention further comprises design method comprising the step of define a time interval and a first plurality of periodic multilayer structures (A), then calculate a first merit function (∫R(λ)10*I(λ)dλ) and define a first domain for each first structures. The method further includes the step of apply at least one random mutation to each first structures inside the associated first domain and calculate a second merit function (∫R(λ)10*I(λ)dλ for the at least one mutation. Then, the method proceeds with a comparison of each first merit functions with the second merit function of the associated at least one mutation and if said second merit function is enhanced with respect to the first merit function, the at least one mutation is substituted for the structure of the first plurality and a second domain is defined for the mutation, otherwise, the structure of the first plurality is maintained inside the corresponding first domain. The method further includes the step of calculate a mean value of the merit functions of the first plurality of structures or mutations present in each first or second domain and define a threshold value to said mean value; then, for each first plurality of structures or mutations present in each first or second domain whose merit function is enhanced of the threshold with respect to the mean value, substitute a third domain to the first or second domain until the corresponding merit function is enhanced of said predetermined threshold. Then, the preceding step are repeated until the time interval has lapsed and the merit functions of the first plurality of structures or mutations present in each first domain are compared and the structure or mutation whose merit function is the more enhanced is selected.

Description

The present invention refers to multilayer aperiodic structures covered by protective capping layers meant for use as reflective coatings for extreme ultraviolet radiation (EUV), particularly in photolithographic processes, as defined in the preamble of claim 1.

High normal incidence reflectivity of a source spectrum in the EUV and soft X-ray spectral range can be obtained only with multilayer structures designed so that the electric field components reflected at the various interfaces can add in phase; in fact, conventional single layer coatings provide negligible reflectance.

The multilayer structures used for EUV lithography (EUVL) in particular typically consist of alternating layers of different materials, for example Molybdenum and amorphous Silicon or Molybdenum and Beryllium (Paul B. Mirkarimi, Sasa Bajt et al. “Mo/Si and Mo/Be multilayer thin films on Zerodur substrates for extreme-ultraviolet lithography”, Applied Optics Vol. 39(10), pp. 1618-1625, 2000). High reflectivity is crucial for photolithographic applications, since the throughput of the system (i.e., number of patterned wafers per hour) depends critically on the intensity of the radiation beam used to project the image of a mask on the photo-resist-coated wafer. Since the optical system typically consists of 9-10 reflective elements, it is clear how even a very small change of the reflectivity of the coating can affect significantly its final performances.

A typical multilayer structure used in EUV photolithography is made of a periodic repetition of a pair of materials, for example Molybdenum and amorphous Silicon, for peak reflectivity near 13.5 nm. A typical periodic structure has a period of about 7 nm, and a Γ value of about 0.6, where Γ is the ratio between the thickness of the Silicon layer and the multilayer period.

The use of a thin interlayer of a different material, for example B₄C, is a well established technique that can be used to avoid interdiffusion and formation of oxide at the interfaces. Peak reflectivity of approximately 70% has been obtained using B₄C interlayers (Sasa Bajt, Jennifer B. Alameda et al. “Improved reflectance and stability of Mo/Si multilayers”, Optical Engineering 41(08), p. 1797-1804, Donald C. O'Shea; Ed., 2002), compared with 68-69% peak reflectance obtained in multilayers without any B₄C interlayers.

Another important key element of these structures is the capping layer. In a basic Molybdenum/Silicon multilayer, the highest peak reflectivity is obtained if the last layer is Molybdenum. However, this Molybdenum layer oxidizes in air and the formation of an oxide top surface degrades the peak reflectivity considerably (Underwood et al, Applied Optics 32, p. 6985, 1993). Therefore Silicon is preferred as capping layer, since, after forming an oxide film, it becomes stable over time. Different environmental effects can affect multilayer performance; in photolithographic apparatus, for example, the coating is exposed to high stress environmental conditions (presence of debris, contaminants, water vapour). For this reason, a protective layer of another material must be deposited on top of the structure. Unfortunately, the deposition of an additional protective capping layer structure on top of the multilayer, as those proved being stable and effective in harsh environments, can reduce the reflectivity as well. Even a small reduction of 1% absolute value of peak reflectivity means a final reduction of more than 18% of the total throughput for a ten elements (ten reflections) system.

When the EUV radiation interacts with a multilayer structure, the superposition of the incident and reflected electromagnetic wave generates a standing wave field distribution in the multilayer structure. In the case of periodic Silicon-Molybdenum multilayer with a last layer of Silicon, a standing wave node appears at the vacuum interface. If on top of the structure a typical capping layer is deposited, the maximum of the standing wave is placed inside the capping layer itself and the radiation is strongly weakened. Consequently less internal layers contribute to the building up of the reflected wave, affecting its intensity. Moreover, the fact that the capping layer absorbs an high amount of radiation increase the oxidation process of the capping layer itself.

The design of a periodic multilayer structure such as those described above doesn't take into account the full effect of the complex phase of the electric field at each interface in the stack. It has been so proposed by Masaki Yamamoto and Takeshi Namioka the use of aperiodic multilayer structures (“Layer-by-layer design method for soft-X-rays multi layers”, Applied Optics, Vol. 31, No. 10, pp. 1622-1630, 1992). In this paper an analytical method effective for the design of soft-X-rays multilayers has been presented. The design is carried on by the aid of the graphic representation of the complex amplitude reflectance in a Gaussian plane.

In past works, aperiodic structures have been designed first to offer best performance in term of peak reflectivity and the incorporation of a capping layer was considered subsequently. By using this approach, solutions have not always offered significantly higher performance with respect to periodic structures: for example the performance of a periodic or an aperiodic multilayer structure with an a-SiO₂ capping layer are quite similar.

Only more recently has the need to protect the structure by a resistant capping layer lead to the optimization of the structure as a whole. Some commercial tools are available to optimize thin layer structures, as for example TFCalc (M. Singh, J. M. Braat, “Design of multilayer extreme-ultraviolet mirrors for enhanced reflectivity”, Applied Optics Vol. 39, No. 13, p. 2189, 2000 and EP 1065532 A2 and U.S. Pat. No. 6,724,462 B1). TFCalc can allow optimization of some parameters of the structures using a global optimization procedure, but only by assuming ideally smooth interfaces. Aperiodic Molybdenum/amorphous Silicon solutions, within possibly the insertion of a third needle layer, have been optimized under some proposed capping layers. In the proposed design typical thickness of the capping layers considered are of the order of 1.5-1.7 nm and last layer under the capping is amorphous Silicon. In the case of a two component Molybdenum/amorphous Silicon multilayer (without the needle layer) the optimization results in a gradual, smooth variation of the layer thickness of the two materials, while the period remains constant, around 7 nm.

Different possible materials can be in principle selected as capping layer for aperiodic structures if the choice is based on the refractive index properties (M. Singh and J. J. M. Braat, “Capping layers for extreme ultraviolet multilayer interference coatings,” Opt. Lett. 26, pp. 259-261, 2001 and U.S. Pat. No. 6,724,462 B1). However, in addition to optical properties requirements, capping layer materials need to meet additional criteria for acceptable performance, as stated above. In particular, they have not to inter-diffuse with the material underneath and they have to be oxidation resistant in a water-vapor environment.

Oxidation of multilayer structures in a photo-lithographic apparatus is mainly due to the presence of water vapor. The oxidation depends on the interaction between EUV photons and the multilayer material (Sasa Bajt, Zu Rong Dai et al. “Oxidation resistance of Ru-capped EUV multilayers” Proc. SPIE Vol. 5751, p. 118-127, Emerging Lithographic Technologies IX; R. Scott Mackay, 2005). The use of an oxidation-resistant protective capping layer is therefore necessary. Ruthenium, which form RuO₂ on top, is the material identified as having the best performance thus far in this regard. Unfortunately, Ruthenium deposited directly on Silicon has been discovered to be unstable, interdiffusing with Silicon and forming Ruthenium Silicide (Sasa Bajt, Henry N. Chapman et. al “Design and performance of capping layers for extreme-ultraviolet multilayer mirrors”, Applied Optics 42(28), pp. 5750-5758, 2003).

Innovative capping layers consisting of two layers have been proposed in U.S. Pat. No. 6,780,496 B2. A top layer protects the structures from the environment, while the second one acts as a diffusion barrier between the top of the multilayer structure beneath. Material combinations considered include Ru/B₄C and Ru/Mo. Structures with Ruthenium layers thicker than 2.3 nm have been demonstrated to be quite stable against environmental agents (Sasa Bajt, Jennifer B. Alameda, et al. “Improved reflectance and stability of Mo/Si multilayers”, Optical Engineering 41(08), p. 1797-1804, Donald C. O'Shea; Ed., 2002).

One object of the present invention is to propose innovative aperiodic multilayer structures which provide improved flux performance in photolithography or in another optical apparatus and which have a reduced sensibility of reflectivity performances to oxidation or contamination of capping layers so that experimental realized structures have life-time performances closer to theoretical. The proposed structures have furthermore improved reflectivity performances stability to layer thickness errors occurring during deposition and are less sensitive to the capping layer materials optical properties.

Another object is to provide an aperiodic multilayer structure design method for designing such structures which allows to obtain a best peak reflectivity (one or more reflections), a large spectral band (one or more reflections) and a match with spectral source distribution (one or more reflections).

These and other objects are achieved according to the invention with an aperiodic multilayer structure as defined in claim 1 and an aperiodic multilayer structure design method as defined in claim 13. Specific embodiments are defined in the dependent claims.

Briefly, the invention consists of aperiodic multilayer structures which have an aperiodicity distributed chaotically in at least a part of the layer thicknesses. In this context the term chaotically is intended to mean that the values of the thicknesses can not be described by or do not follow any particular order or trend. Preferably, the aperiodicity is distributed in all the layer thicknesses, alternatively, the aperiodicity is limited to the layers of the last period underneath the capping layer.

The optimization of structure with only the layers underneath the capping layer varied is made only to achieve best peak reflectivity, while the ones in which the aperiodicity is distributed in all the layer thicknesses is made to maximize total photon flux according to different optical apparatus. In any case, aperiodic structures with chaotically distributed layer thicknesses through all the stack offer better performances, as shown later in the examples.

The structures are made of two or more materials (preferably Molybdenum and amorphous Silicon) and include protective capping layers for best performances in EUV lithography applications. Preferably, different interlayer materials, for example B₄C, are included to prevent interdiffusion.

The design optimization of the aperiodic multilayer structures is dependent on the presence of the capping layer. First the capping layer properties such as layer thickness and materials are defined for maximum performance, then the multilayer structure is optimized. In order to guarantee feasibility of the structure according to recent studies on capping layers, structures with most performing capping layers of Mo/Ru and B₄C/Ru have been considered specifically, but the invention is not limited to these specific capping layer prescriptions. Indeed, because the aperiodic design optimization results in greatly relaxed optical properties requirements for the capping layer, other materials and material combinations that eventually show even greater protection than Mo/Ru and B₄C/Ru can be utilized.

The new multilayer designs result in very interesting properties:

1) They provide improved flux performance in a photolithography or in another optical apparatus. This is due to two main facts:

• • the energy absorption in the top layers of the multilayer is reduced, therefore the EUV signal penetrates deeper into the structure and more layers can contribute to the final reflectivity;
  • in case of multilayers with aperiodicity distributed chaotically through the all stack, the optimization of layers thickness allows a further increasing of the amplitude of the reflected field. In fact interference among interfaces reflected components is further improved by optimizing multiple reflections contribution inside each layer.2) The absorption of the EUV in the top layers of the multilayer is reduced, therefore also the mechanism of oxidation formation is slowed down.3) The multilayer structure is less sensitive to the capping layer materials, i.e. its performance is nearly independent on the choice of capping layer optical properties. This means also that if there is a change of the optical constants of the top layer, for example due to contamination or oxidation, the performance remains unchanged.4) Since the absorption of top layers is reduced the energy can penetrate deeper in the multilayer structure and consequently it will be distributed in a larger volume with less density, accordingly reducing the induced thermal stress.5) Multilayers have an improved stability of performances with respect to possible layer thickness errors occurring during deposition.All aspects 2-4 increase the lifetime of the multilayer structure.

Further characteristics and advantages of the invention will be made clear by the following detailed description, provided purely by way of non-limiting example, with reference to the attached drawings, in which:

FIG. 1 is a schematic sectional view of last final layers of a first aperiodic multilayer structure according to the invention;

FIG. 2 is a schematic view of last final layers of a second aperiodic multilayer structure according to the invention;

FIG. 3 is a graphic of the experimental reflectance of the structure of FIG. 1 for two different capping layer materials;

FIG. 4 is a schematic sectional view of a multilayer structure;

FIG. 5 is a scheme of a spherical domain;

FIG. 6 is a schematic sectional view of a conical sub-domain with respect to the one of FIG. 5;

FIG. 7 is a graphic of the thicknesses of the layer of a possible structure according to the invention;

FIG. 8 is a graph of the experimental reflectance for two different structures;

FIG. 9 is a graph of the throughput a projection system;

FIG. 10 is a graphic of the intensity value of a node out of the capping layer;

FIG. 11 is a graphic of the peak reflectivity as a function of the oxidation of the capping layer; and

FIG. 12 are two graphs of the percentage of reflected spectrum for two different structures.

The superposition of the incident and reflected electromagnetic wave results in a standing wave field distribution in the multilayer structure, as previously stated. The structures according to the invention are characterized by the property that the capping layer is spatially shifted with respect to the position of the standing-wave anti-node at the top of the multilayer, while providing best reflectance performances, as described later. In particular, a deep analysis of the standing wave field distribution inside the multilayer itself shows that the solutions founded are the best compromise between the two following characteristics:

• • at working wavelength, the standing wave field strength is minimized in the capping layer (i.e. the absorbed energy is minimized);
  • the standing wave field is distributed to maximize reflectivity performances; this is equivalent to minimize the first node of the standing wave outside the multilayer.

Moreover, the properties remain valid not only at one wavelength but they extend over the full spectral range of the source in case of the structures having a chaotically distributed layer thicknesses made, for example, to match a source spectrum in a photolithographic apparatus or to have a large spectral band.

For example, in case of a photolithographic apparatus with a Sn plasma laser source and ten reflections, an improved flux more then two times with respect to standard coating is achievable, while resistance to the environmental attach is guaranteed by the use of most reliable capping layers.

FIG. 1 shows a schematic section of a multilayer stack 2 made of two alternating layers of different material, a layer of a first material 4 and a layer of a second material 6. Interlayers 8 are included between the layer of the first 4 and the second 6 material to prevent inter-diffusion.

The first material 4 is for example amorphous Silicon, the second material 6 is Molybdenum and the interlayers 8 are of B₄C.

Further examples of first 4 and second 6 material may include Beryllium, Ruthenium, Rhodium, Strontium and similar materials or their compounds.

Further examples of interlayers 8 may include Carbon and Silicon Carbide and similar materials or compounds.

In an alternative embodiment, interlayers 8 are omitted so that the stack 2 is made only of the first 4 and second 6 material.

On the top of the stack 2 is deposited a capping layer 10, which comprises for example a first layer 10a of Ruthenium and a second layer 10b of B₄C. Alternatively, the capping layer 10 may be made of a single material.

Further examples of capping layer materials may include Ruthenium, Rhodium, Zirconium, Palladium, Platinum, Osmium, Iridium used alone or combined for example with a layer of Boron Carbide, Carbon, Silicon Carbide, Molybdenum and similar materials, used as pure elements or compounds.

The layers of the first 4 and the second 6 material present thicknesses which vary each other in a chaotic way through the whole stack 2, realizing an aperiodic structure.

The capping layer 10 is illuminated by radiation coming from a source S, for example a Sn laser produced plasma source or another optical element that redirects the source beam, placed in front of the capping layer 10.

The capping layer 10 is spatially shifted with respect to the position of the standing-wave anti-node at the top of the stack 2, as can be seen from FIG. 1 which shows a standing wave 12 which has a node 14 in the capping layer 10 and an anti-node 15 out of the capping layer so that the stack 2 offers superior efficiency performances and is substantially insensitive to the capping layer materials optical properties.

The standing wave field at working wavelengths is thus shifted in the capping layer with respect to the periodic multilayer structures of the prior art in order to minimize the absorbed energy in the first layers. The energy absorption in the top layers of the multilayer stack 2 is reduced, therefore the EUV signal penetrates deeper into the structure and therefore more layers can contribute to the final reflectivity. Due to this property, the thermal stress is also reduced, since the energy is distributed over more layers. Furthermore, the oxidation process of the capping layer 10 is slowed down due to the fact that capping layer 10 absorbs less EUV light which is responsible for the creation of secondary electrons that lead to oxidation. Moreover, the chaotic distribution of the layers of the first 4 and second 6 materials make them less sensitive to thickness errors during deposition, as demonstrated later.

FIG. 2 shows a schematic sectional view of a second embodiment of the multilayer structure according to the invention. A stack 2′ is made of two alternating layers of a first material 4′ and a second material 6′ with interlayers 8′ included between the layer of the first 4′ and the second 6′ material to prevent inter-diffusion.

The first material 4′ is for example amorphous Silicon, the second material 6′ is Molybdenum and the interlayers 8′ are of B₄C.

In an alternative embodiment, interlayers 8′ are omitted so that the stack 2′ is made only of the first 4′ and second 6′ material.

On the top of the stack is deposited a capping layer 10′ which comprises for example a first layer 10a′ of Ruthenium and a second layer 10b' of B₄C. Alternatively, the capping layer 10′ may be made of a single material.

The first layer of the first material under the capping layer 10′ is indicated 4a; the first layer of the second material under the capping layer 10′ is indicated 6a. Layers 4a and 6a are indicated together as pre-caplayer. These layers 4a and 6a have a thickness different from the thickness of respective layers of the first 4′ and second 6′ material, which realize a periodic structure through the whole stack 2′.

Useful materials are the same as listed with reference to the stack 2 of FIG. 1. Performances are generally lower than those of previous structure according to FIG. 1. Moreover, stability of solution with respect to layer thickness errors is lower. Therefore, advantageously, these solutions have a more simple design, requiring less optimization parameters.

In FIG. 3 are shown two experimental curves of the reflectance of the aperiodic stack 2 (without the interlayers 8) as function of the wavelength of the incident radiation. A first curve 16 is related to the stack 2 with a capping layer 10 made of a first layer 10a of Platinum and a second layer 10b of Molybdenum, a second curve 18 is related to the stack 2 with a capping layer 10 made of a first layer 10a of Ruthenium and a second layer 10b of Molybdenum. As can be noted, the reflectance properties are essentially equivalent, according to what previously stated. Additionally, even if the capping layer gets oxidized or contaminated, the reflectivity performances are essentially unchanged.

For the design of the aperiodic structures with chaotically distributed layer thicknesses above described, a new design method has been developed. The realization of the structures is made by defining a merit function accordingly, as for example ∫R(λ)^N*I(λ)dλ, where I(λ) is the source spectrum, R(λ) is the reflectivity of the structure and N is number of mirrors in the apparatus (particularly 9 or 10). Other merit functions can also be used. The design method looks for the best solution defined in the space of the different multilayer structures. Considering that multilayer reflection r(f) depends very critically from its structural parameters, i.e. its performances are very sensitive to small variations of the multilayer structure, an “evolutive strategy” has been used. The “evolutive” approach differs from a local optimization algorithm, that would be improper since it would explore only a limited domain region, and from typical global optimizations, like a genetic algorithm, which would be too weak for focus towards a domain region with overconfidence. For this reason, the design method developed is able to acquire domain knowledge based on the merit function values during the optimization process. During the optimization, typical roughness values at the interfaces are also taken into account; this makes possible to find solutions having superior performances with respect to those solutions in which roughness is not taken into account. This type of optimization explores a wide interval in the space of solutions, taking into account all experimental aspects related to practical feasibility of the structure.

The method provide computation of the multilayer reflectance as well as of the whole merit function. Computation takes into account roughness at interfaces, inter-diffusion between layers, roughness at the substrate, and can include any other parameter related to a real deposited multilayer structure, differently from other used software, as TFCALC. The optical constants used for the calculation are those provide by the Center for X-Ray Optics database.

The design algorithm must focus toward a structure that maximize the merit function. A generic multilayer composed by N layers is defined as x=(L₁^x, L₂^x, L₃^x, L₄^x, . . . , L_N^x) where the L_i^x are the distance of the i-th interface from a top interface of the multilayer x in angstrom, as shown in FIG. 4. N is typically 110.

FIG. 4 shows a multilayer structure 100 formed by alternating layers 102, 104 of different material, for example Silicon and Molybdenum, deposited on a substrate 106; the top interface of the multilayer x is indicated 108. L₁ is the distance of a first interface 110 from the top interface 108, L₂ is the distance of a second interface 112 from the top interface 108, L₃ is the distance of a third interface 114 from the top interface 108 and L₄ is the distance of a fourth interface 116 from the top interface 108.

The norm of x is:

$\stackrel{\_}{x}=\sqrt{\sum _{i=1}^N{\left(L_i^{\stackrel{\_}{x}}\right)}^2}$

and the distance between two different structures x₁ and x₂ is:

$d\left({\stackrel{\_}{x}}_1,{\stackrel{\_}{x}}_2\right)={\stackrel{\_}{x}}_1-{\stackrel{\_}{x}}_2=\sqrt{\sum _{i=1}^N{\left(L_i^{{\stackrel{\_}{x}}_1}-L_i^{{\stackrel{\_}{x}}_2}\right)}^2}$

The first step of the method according to the invention is the definition of a predetermined time interval into which execute said design method; preferably, said time interval is of eight hours for a home computer with a 3 GHz processor. Then, a set of periodic multilayer structures is considered, particularly a family of 4 multilayer structures

$\left\{{\stackrel{\_}{x}}_1^{\mathrm{step}=0},{\stackrel{\_}{x}}_2^{\mathrm{step}=0},{\stackrel{\_}{x}}_3^{\mathrm{step}=0},x_4^{\mathrm{step}=0}\right\}$

which have an optimized period value and a randomly defined Γ ratio. For each multilayer structure x_i of said set a spherical domain B( x_i, ρ) centred in x_iεB( x i, ρ) is defined, where ρ is the radius of the sphere, in angstrom. FIG. 5 shows a structure x_i^step=j 118 and a spherical domain 120 having a radius 122; to visualize the concept, a tri-dimensional domain is represented.

In any successive j-th calculation step (j=1, 2, 3, . . . ) a mutation ζ_i^j is applied to the structures x_i^step=j. Mutations ζ_i^j( x_i^step=j) are randomly chosen inside the proper domain

$B\left({\stackrel{\_}{x}}_{i=1,2,3,4}^{\mathrm{step}=j},\rho \right)$

associated to each multilayer structure x_i. If an enhancement of the merit function is obtained, the mutation solution ζ_i^j( x_i^step=j) swap the solution x_i^step=j in the population at the j+1-th step ( x_i^step=j+1=ζ_i^j( x_i^step=j)) and a new spherical domain centred in the mutation solution B x_i^j+1, ρ) is substituted for the spherical domain B( x_i, ρ). In the case that the merit function associated to one of the structures x^step=j+1 has a value that exceeds a mean value of the merit functions of the family at the j+1-th step over a predetermined threshold, the spherical domain region where applying a mutation becomes a cone C( x^step=j+1, ρ, versor, α) where:

• • x_i^step=j+1 is the central point,
  • versor is the central axes determined by the formula:

$\mathrm{versor}=\frac{\left({\zeta }_i^j\left({\stackrel{\_}{x}}_i^j\right)-{\stackrel{\_}{x}}_i^j\right)}{d\left({\zeta }_i^j\left({\stackrel{\_}{x}}_i^j\right),{\stackrel{\_}{x}}_i^j\right)}·\frac{\mathrm{MF}\left({\zeta }_i^j\left({\stackrel{\_}{x}}_i^j\right)\right)-\mathrm{MF}\left({\stackrel{\_}{x}}_i^j\right)}{\mathrm{MF}\left({\zeta }_i^j\left({\stackrel{\_}{x}}_i^j\right)\right)-\mathrm{MF}\left({\stackrel{\_}{x}}_i^j\right)}$

where MF( x^step=j) is the merit function value of the multilayer x^step=j;

• • α is the angle in the vertex determined by:

$\alpha =\frac{\mathrm{MF}\left({\zeta }_i^j\left({\stackrel{\_}{x}}_i^{\mathrm{step}=j}\right)\right)-\mathrm{MF}\left({\stackrel{\_}{x}}_i^{\mathrm{step}=j}\right)}{\mathrm{MF}\left({\stackrel{\_}{x}}_i^{\mathrm{step}=j+1}\right)-\frac{\sum _{i=1}^4\mathrm{MF}\left({\stackrel{\_}{x}}_i^{\mathrm{step}=j+1}\right)}{4}}$

In FIG. 6 is represented a schematic cone inside the spherical domain 120 of FIG. 8 in which a versor 124 and an angle 126 are depicted.

When the time interval into which the above disclosed calculation steps are performed is finished, a comparison is made between the merit functions of the structures thus obtained and the structure whose merit function is the more enhanced is selected as the best one.

In this way, differently form a pure genetic algorithm, it is possible to deeply explore some specific domain areas. The method allows also the optimization of interlayers, when these are introduced between the two main materials; they are seen as added layers with different optical constants. More generally, the method may optimize whatever structure.

EXAMPLES

In the following examples are presented. In all examples, the structures are optimized for a 10° incidence angle between the normal to the front surface of the first layer 10a, 10a′ and the direction of the light from the source. In all the examples, a 5 Å of multilayers interface roughness has been taken into account.

Example 1

Aperiodic multilayer stacks 2 of type shown in FIG. 1 (without the interlayers 8) made of alternating layers of Molybdenum and amorphous Silicon with a Mo/RuO₂ capping layer have been compared with a standard periodic multilayer structure made of the same materials.

In table 1 are reported the thicknesses of the layers.

TABLE 1
Structure according to embodiment of FIG. 1 (without interlayers)
Capping layer	RuO2/Mo	23 Å/20 Å
	amorphous Silicon layer minimum	24.1 Å
	amorphous Silicon layer maximum	42.9 Å
	Molybdenum layer minimum	26.8 Å
	Molybdenum layer maximum	35.5 Å

FIG. 7 shown the curves of the thicknesses of the layers as function of the layer index, which indicates the layers (capping layers omitted) with an increasing number from the most external to the internal one: a first curve 20 is related to the layer of the first material 4, Silicon, a second curve 22 is related to the layer of the second material 6, Molybdenum. As shown, thicknesses and periods are chaotically distributed, being very far from solution in a round of the periodic multilayer.

The multilayer structure is optimized to provide maximum reflectance in a photolithographic system comprising N=10 mirrors. The optimization is made in order to match the spectrum of one of the possible sources of an EUV lithographic system, i.e. the Sn laser produced plasma, according to the ∫R(λ)^N*I(λ)dλ, merit function previously introduced.

The reflectivity of the structure of table 1 has been compared with that of a standard periodic structure of the type reported in table 2.

TABLE 2
Periodic structure (period of 69.8 Å, Γ of 0.6)
	Capping layer	RuO2/Mo	23 Å/20 Å
		amorphous Silicon layer	41.9 Å
		Molybdenum layer	27.9 Å

Assuming, for instance, a projection system with ten subsequent reflections, an improvement of the efficiency up to 79%, corresponding to a multiplication factor of 1.79 with respect to the system of table 2, has been computed.

FIG. 8 shows experimental results obtained by the measure of two structures realized according to embodiment of FIG. 1 and table 2. A first curve 150 is related to a periodic structure as the one of table 2, a second curve 152 is related to a chaotically aperiodic structure as the one of table 1.

FIG. 9 shows a comparison between structures of table 1 and 2 for a projection system with ten subsequent reflections. A first curve 154 is related to the periodic structure of table 2, a second curve 156 is related to the chaotically aperiodic structure of table 1. It is clearly visible the improvement of the efficiency up to 79% above disclosed.

Example 2

The same comparison of example 1 with the standard periodic structure of table 2 has been made using stacks of the type shown in FIG. 2 (without the interlayers 8′), made of alternating layers of Molybdenum and amorphous Silicon with a Mo/RuO₂ capping layer in which only last layers underneath the capping layer are varied, according to parameters presented in table 3.

TABLE 3
Structure according to embodiment of FIG. 2
(without interlayers, period of 70.2 Å)
Capping layer	RuO2/Mo	23 Å/20 Å
Pre-caplayer	amorphous Silicon/Molybdenum	23.3 Å/27 Å
	amorphous Silicon layer	41.1 Å
	Molybdenum layer	29.1 Å

In a projection system with ten subsequent reflections, an improvement of the efficiency up to 77%, corresponding to a multiplication factor 1.77 with respect to the system of table 2, has been computed.

Example 3

Different comparisons have been made with reference to the structures disclosed in tables 1, 2 and 3. For each of the structure, each intensity value of a node 24, 24′ (see FIGS. 1 and 2) out of the capping layer has been calculated for a wide spectral wavelength corresponding to about the Full Width Half Maximum of the multilayer reflectance. Results are reported in FIG. 10: a first curve 26 is related to the structure of table 2, a second curve 28 is related to the structure of table 3 and a third curve 30 is related to the structure of table 1. It is evident that value related to the aperiodic stack of table 1 is always lower then the one of the periodic standard multilayer, demonstrating that this is the optimum solution. The value of the aperiodic stack with pre-caplayer is lower almost everywhere, and in any case the integral of the curve is again lower that the one corresponding to the periodic standard structure.

Example 4

Some tests have been performed to compare the performances sensitivity to layer thickness errors during deposition of aperiodic structures with respect to standard periodic ones. Structures presented in tables 1, 2 and 3 have been considered for comparison. In order to do so, a mean percentage of reflected spectrum (calculated as 100*∫R(λ)¹⁰*I(λ)dλ/∫I(λ)dλ) has been evaluated for 3000 structures, obtained by a variation of the three structures: each layer thickness has been randomly varied inside a maximum interval of ±0.01 nm (which is a typical error during a deposition process), with a uniform probability distribution. In table 4 statistical data for the three types of structures are reported.

	TABLE 4
	Mean percentage of	Standard
	reflected spectrum	deviation
Structure according to table 1	0.4108	0.00106
Structure according to table 3	0.4063	0.00120
Structure according to table 2 (periodic)	0.2319	0.00211

Statistical analysis confirms that structures according to table 1 are more stable to random layer thickness variation then both standard periodic and aperiodic with pre-caplayer, and that the aperiodic with pre-caplayer are more stable then standard periodic ones.

Example 5

A stack according to embodiment of FIG. 1 has been optimized to provide maximum reflectance in a photolithographic system (see table 5).

In table 5 are reported the thicknesses of the layers.

TABLE 5
Structure according to embodiment of FIG. 1
Capping layer	RuO2/B4C	23 Å/20 Å
	amorphous Silicon layer minimum	19 Å
	amorphous Silicon layer maximum	40 Å
	B4C interlayer	2.5 Å
	Molybdenum layer minimum	25 Å
	Molybdenum layer maximum	30 Å
	B4C interlayer	4 Å

Standing wave field at wavelength 13.4 nm has been considered (actually is the one reported in FIG. 1). Comparison with a standard periodic Mo/B₄C/a-Si multilayer with a capping layer of RuO₂/B₄C has been made.

In table 6 are reported the thicknesses of the layers of the standard periodic Mo/B₄C/a-Si multilayer with a capping layer of RuO₂/B₄C.

TABLE 6
Periodic structure (period of 69.8 Å, Γ of 0.6)
	Capping layer	RuO2/B4C	23 Å/20 Å
		amorphous Silicon layer	38.6 Å
		B4C interlayer	2.5 Å
		Molybdenum layer	24.7 Å
		B4C interlayer	4.0 Å

Assuming, for instance, a projection system with ten subsequent reflections and a Sn laser plasma source, an improvement of the efficiency up to 115%, corresponding to a multiplication factor 2.15 with respect to the system of table 6, has been computed.

A comparison between the standing wave corresponding to the multilayer with RuO₂/Mo capping layer of example 1 (see table 1) and the one of this example (see table 5) shows that in the first case the position of the node in the capping layer is inside the Mo layer, while in the second one is in the RuO₂ layer (as in FIG. 1). This is due to the fact that at 13.4 nm absorption coefficient of B₄C is lower then the Mo one, which is closer to the one of RuO₂.

Example 6

A comparison similar to that of example 5 has been made using stacks of the type shows in FIG. 2.

In table 6 are reported the thicknesses of the layers.

TABLE 6
Structure according to embodiment of FIG. 2 (period of 70.3 Å)
Capping layer	RuO2/B4C	23 Å/20 Å
Pre capping layer	a-Si/B4C/Mo/B4C	19 Å/2.5 Å/24.75 Å/4 Å
	amorphous Silicon layer	35.3 Å
	B4C interlayer	2.5 Å
	Molybdenum layer	28.5 Å
	B4C layer	4.0 Å

Assuming, for instance, a projection system with ten subsequent reflections, an improvement of 110% with respect to the system of table 6 is obtained.

Example 7

In order to prove the less sensitivity of the performances to capping layer oxidation, the following calculation has been performed for structure of table 1 and 3 to be compared with the standard periodic structure of table 2: the last layer of the capping layer (i.e. the RuO₂ in the tables) has been initially considered not oxidized, and then partially oxidized up to be totally oxidized. Peak reflectivity has been calculated at 13.4 nm in all cases. Results obtained are reported in FIG. 11: a first curve 32 refers to the structure of table 1, a second curve 34 refers to the structure of table 3 and a third curve 36 refers to the standard periodic structure of table 2. It is clear that the reflectivity of aperiodic structures is less affected by the growing of the oxide.

Example 8

The design method used for the search of the aperiodic chaotic solution considers the amount of roughness at interfaces. This fact thus leads to solutions that take into account advanced manufacturing aspects and physical properties of practical multilayer structures. To show how this is relevant, a test has been performed.

It has been used the merit function ∫R(λ)¹⁰*I(λ)dλ, and it has been searched for the aperiodic best structure following the steps above described. In FIG. 12 there are shown two graphs which compare the percentage of reflected spectrum of a first structure 200 found by the method assuming an interface roughness equal to zero, and of a second structure 202 found assuming an interface roughness of 5 Å. The percentage of reflected spectrum has been calculated as 100*∫R(λ)¹⁰*I(λ)dλ/∫I(λ)dλ. In a first graph 204, the percentage of reflected spectrum of structure 200 is compared with the one of the second structure 202, but calculated without roughness; in a second graph 206 the percentage of reflected spectrum of the first structure 200 is calculated adding a roughness of 5 Å (as would be more realistic in case of a real deposit) and compared with the one of structure 202. As shown in 206, in this more realistic case in which both structures have a 5 Å roughness at interfaces, structure 202 shows better performances. If the search did not carry on by adding this roughness at interfaces, ideal best solution would have found to be structure 200, as demonstrated in 204; but, a real deposited multilayer according to design 200 would not preserve its supremacy over 202. The second structure 202 is therefore a better solution as the real physical properties of the interfaces are taken into account during mathematical search.

Clearly, the principle of the invention remaining the same, the embodiments and the details of construction can be varied widely from what has been described and illustrated purely by way of non-limiting example, without departing from the scope of protection of the present invention as defined in the attached claims.

Claims

1. An aperiodic multilayer structure (2, 2′) comprising a plurality of alternating layers of a first (4, 4′) and a second (6, 6′) material and a capping layer (10, 10′) covering said layers, said structure (2, 2′) being characterized in that the thickness of said alternating layers chaotically varies in at least a portion of said structure (2, 2′).

2. The aperiodic stack (2, 2′) according to claim 1, in which the thickness of said alternating layers chaotically varies in the whole structure (2, 2′).

3. The aperiodic structure (2, 2′) according to claim 1, comprising at least one interlayer (8, 8′) of a third material interposed between said first (4, 4′) and second (6, 6′) material.

4. The aperiodic structure (2, 2′) according to claim 1, in which said first (4, 4′) and second (6, 6′) material are selected from the group consisting of amorphous Silicon, Molybdenum, Beryllium, Ruthenium, Rhodium, Strontium and their compounds.

5. The aperiodic stack (2, 2′) according to claim 3, in which said third material is selected from the group consisting of Boron Carbide, Carbon, Silicon Carbide and their compounds.

6. The aperiodic structure (2, 2′) according to claim 1, in which said capping layer (10, 10′) is made of a material selected from the group consisting of Ruthenium, Rhodium, Zirconium, Palladium, Platinum, Iridium, Osmium, Molybdenum, Boron Carbide, Silicon Carbide and their compounds.

7. The aperiodic structure (2, 2′) according to claim 1, in which said capping layer (10, 10′) comprise at least a first layer (10a) and a second layer (10b) made of different materials.

8. The aperiodic structure (2, 2′) according to claim 7, in which said first layer (10a) is made of a material selected from the group consisting of Ruthenium, Rhodium, Zirconium, Palladium, Platinum, Iridium, Osmium and their compounds.

9. The aperiodic structure (2, 2′) according to claim 7, in which said second layer (10b) is made of a material selected from the group consisting of Boron Carbide, Carbon, Silicon Carbide, Molybdenum and their compounds

10. The aperiodic structure (2, 2′) according to claim 1, in which said capping layer (10, 10′) is spatially shifted with respect to the position of a standing-wave anti-node (15) at the top of the structure (2, 2′).

11. A reflective coating comprising an aperiodic structure (2, 2′) as defined in claim 1.

12. A photolithographic apparatus comprising an aperiodic structure (2, 2′) as defined in claim 1.

13. An aperiodic multilayer structure design method comprising the step of: a) define a predetermined time interval;b) define a first plurality of periodic multilayer structures

14. The aperiodic multilayer structure design method according to claim 13, wherein said first predetermined domain is spherical.

15. The aperiodic multilayer structure design method according to claim 13, wherein said second predetermined domain is spherical.

16. The aperiodic multilayer structure design method according to any of the claim 13 wherein said third predetermined domain is conical.

17. The aperiodic multilayer structure design method according to claim 13, wherein said predetermined time interval is of eight hour.

18. The aperiodic multilayer structure design method according to claim 13, wherein said first merit function takes into account roughness and interdiffusion.

19. The aperiodic multilayer structure design method according to claim 13, wherein said second merit function takes into account roughness and interdiffusion.