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Title:
THERMO-MECHANICAL CONTROLLED CRYOGENIC DELAMINATION PROCESS FOR THE FULL RECOVERY OF RIGID MONO-, POLYCRYSTALLINE OR AMORPHOUS MATERIALS COATED WITH PLASTIC MATERIALS
Document Type and Number:
WIPO Patent Application WO/2014/141311
Kind Code:
A1
Abstract:
The purpose of the invention is to provide a process for the recovery of raw materials fro multilayer artifacts. The process involves cryogenic conditioning of the materials to be recovered and exploits the different thermal and elastic behaviour of different layers of different material.

Inventors:
DASSISTI MICHELE (IT)
Application Number:
PCT/IT2013/000135
Publication Date:
September 18, 2014
Filing Date:
May 08, 2013
Export Citation:
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Assignee:
POLITECNICO DI BARI (IT)
International Classes:
H01L31/048; B08B7/00; B09B3/00; B09B5/00; B29B17/02; B32B43/00
Foreign References:
JP2006346636A2006-12-28
US20110183442A12011-07-28
EP0893250A11999-01-27
US5842650A1998-12-01
US6063995A2000-05-16
US6129779A2000-10-10
US5997718A1999-12-07
DE102008058530A12010-05-27
Other References:
SUKMIN KANG ET AL: "Experimental investigations for recycling of silicon and glass from waste photovoltaic modules", RENEWABLE ENERGY, PERGAMON PRESS, OXFORD, GB, vol. 47, 18 April 2012 (2012-04-18), pages 152 - 159, XP028510222, ISSN: 0960-1481, [retrieved on 20120426], DOI: 10.1016/J.RENENE.2012.04.030
Attorney, Agent or Firm:
RUSSO, Dimitri (Via G. Bozzi 47A, Bari, IT)
Download PDF:
Claims:
CLAIMS

1. Thermo-mechanical controlled cryogenic delamination process for the full recovery of rigid mono-, polycrystalline or amorphous materials coated with plastic materials, comprising the use of at least one system for the controlled cryogenic cooling (1) of the elements or parts thereof, at least one selective temperature control system for high speed heating (2), a system for high frequency transmission of motion to produce vibrations at the first natural frequency of resonance (3), at least one insufflation system at controlled pressure (4) and at least one power transmission system, at least one mechanical actuator (5) for manipulating layers; the process being characterized by the following phases:

- Temperature homogenization of all the layers for a given time;

- Swift or super swift cooling at cryogenic temperatures of the layers adjacent to the layer of the material to be recovered, by means of the controlled cryogenic cooling system (1) controlling the flow rate and pressure of a cold carrier through a fluids compressor or other suitable system;

- When cryogenic temperature is stable, superimposition of thermal cycles at controlled frequency in the layer of the material to be recovered, to transmit a temperature differential between the external layers maintained at cryogenic temperature and the layer to be recovered, at significantly higher temperature differentials, to exploit the different mechanical properties of expansion at different temperatures and then produce different share stress between the layers (here defined as thermal delamination stress or τ T);

- Always in condition of stable cryogenic temperature, possible simultaneous superimposition of cycles of bending stresses controlled by vibrations of the entire element or of the combination of layers at frequencies at the first frequency of resonance; this action is to produce a secondary mechanical shear stress (here defined mechanical delamination stress or τ M ) between the layer of material to be recovered and the contiguous layers, whose frequency is in phase with the thermal cycles and produce a total delamination stress which is synergic than the individual effects.

- Insufflation of liquid mixtures at controlled pressure and flow rate for the final delamination of the layers or full immersion of layers into a liquid or gaseous mixture;

- Mechanical separation, also through the immersion in an appropriate liquid or gaseous mixture, of one or more external layers with respect to the layer of the material to be recovered by means of suitable mechanical action devices.

2. Process of claim 1 characterized in that the cryogenic cooling system (1) is suitable for cooling and for real time control of the cooling conditions, that is of the temperature and flow rate of the refrigeration carrier.

3. Process according to the previous claims characterized in that the cold carrier compressor continuously controls the pressure and the flow rate, and it is suitable to operate at temperatures lower than 0 degrees centigrade.

Process according to the previous claims characterized in that the differential heating is achieved via a selective induction heating system (2), either by direct contact or non- direct contact, said system (2) being suitable to exclusively affect the high thermal conductivity layers (material to be recovered) of the multilayered component to be treated, without warming the adjacent layers.

Process according to claims 1 and 4 characterized in that in case of non-direct contact system the selective induction heating system can be of the magnetic induction type, of the photonic induction type or of the radiation induction type; whereas in case of direct- contact system, the selective induction heating system can be of the electrical conduction type or of the heat conduction type or similar.

Cryogenic process of claim 1, characterized in that the separation of the materials is exclusively obtained by imposition of thermal cycles at controlled frequency of the layer of the material to be recovered, or without the superimposition of vibrations at the first natural frequency of resonance.

Process according to the previous claims, characterized in that the insufflation of liquid and/or gaseous mixtures at controlled pressure and flow rate for the final delamination of the layers (C2, P, M, CI) is achieved through a compressor, or in a controlled atmosphere chamber wherein the element (A) to be treated is immersed.

8. Process according to the previous claims, characterized in that the detachment of the layers (C2, P, M, CI) of the element (A) is achieved by means of shear stresses distributed and transferred to said layers (C2, P, M, CI) via contact depression systems, or via mechanical cutting by means of a rigid clutch system affecting the thickness of the external layers (C2, P, CI).

9. Thermo-mechanical controlled delamination cryogenic process for the full recovery of rigid mono-, polycrystalline or amorphous materials coated with plastic materials wherein the detachment of the layers (C2, P, M, CI) is achieved through the insufflation of a low chemical aggressive liquid mixture, or through a complete immersion of the element (A) in a controlled atmosphere chamber in saturation condition of said liquid and/or gaseous mixture.

10. Process according to claim 9 characterized by suitable means or processes allowing induced degradation of the mechanical properties of the plastic parts (P) by accelerated aging.

AMENDED CLAIMS

received by the International Bureau on 24 February 2014 (24.02.2014)

1. Thermo-mechanical controlled cryogenic delamination process for the full recovery of rigid mono-, polycrystalline or amorphous materials coated with plastic materials, comprising the use of at least one system for the controlled cryogenic cooling (1) of the elements or parts thereof, at least one selective temperature control system for high speed heating (2), a system for high frequency transmission of motion to produce vibrations at the first natural frequency of resonance (3), at least one insufflation system at controlled pressure (4) and at least one power transmission system, at least one mechanical actuator (5) for manipulating layers; the process being characterized by the following phases:

- Temperature homogenization of all the layers, say laying along the X-Y plane in a generic Cartesian reference system, for a given time;

- Swift or super swift cooling at cryogenic temperatures of the layers adjacent to the X-Y layer of the material to be recovered, induced by means of the controlled cryogenic cooling system (1) controlling the spatial flow rate over the X-Y plane and pressure of a cold carrier through a fluids compressor or other suitable system over time;

- When cryogenic temperature is stable, superimposit on of thermal cycles at controlled frequency in the X-Y layer of the material to be recovered, to transmit a temperature differential between the external layers maintained at cryogenic temperature and the layer to be recovered, at significantly higher temperature differentials, to exploit the different mechanical properties of expansion, along the X direction, at different temperatures and then produce different share stress between the layers i.e. thermal delamination stress or ττ along X direction while the stress along Y direction is considered negligible,

- Always in condition of stable cryogenic temperature, possible simultaneous superimposition of cycles of bending stresses around Y axis controlled by induced vibrations of the entire element or of the combination of layers of the X-Z plane at frequencies at the first frequency of resonance; this action is to produce a secondary mechanical shear stress i.e. mechanical delamination stress or τ over the X-Y plane between the layer of material to be recovered and the contiguous layers, whose frequency is in phase with the thermal cycles to induce a total delamination stress in the X-Y plane which is synergic than the individual effects; namely τΤοι≥ττ+τΜ.

- Insufflation of liquid mixtures at controlled pressure and flow rate for the final delamination of the layers or full immersion of layers into a liquid or gaseous mixture; - Mechanical separation, also through the immersion in an appropriate liquid or gaseous mixture, of one or more external layers with respect to the layer of the material to be recovered by means of suitable mechanical action devices.

2. Process of claim 1 characterized in that the cryogenic cooling system (1) is suitable for cooling and for real time control of the cooling conditions, that is of the temperature and flow rate of the refrigeration carrier.

3. Process according to the previous claims characterized in that the cold carrier compressor continuously controls the pressure and the flow rate, and it is suitable to operate at temperatures lower than 0 degrees centigrade.

4. Process according to the previous claims characterized in that the differential heating is achieved via a selective induction heating system (2), either by direct contact or non- direct contact, said system (2) being suitable to exclusively affect the high thermal conductivity layers, i.e. material to be recovered of the multilayered component to be treated, without warming the adjacent layers.

5. Process according to claims 1 and 4 characterized in that in case of non-direct contact system the selective induction heating system can be of the magnetic induction type, of the photonic induction type or of the radiation induction type; whereas in case of direct- contact system, the selective induction heating system can endeavor the electrical resistivity properties of the same material processed by superimposition of an electrical current or of the heat conduction type or similar.

6. Cryogenic process of claim 1, characterized in that the separation of the materials is exclusively obtained by imposition of thermal cycles at controlled frequency of the layer of the material to be recovered, or without the superimposition of vibrations at the first natural frequency of resonance.

7. Process according to the previous claims, characterized in that the insufflation of liquid and/or gaseous mixtures at controlled pressure and flow rate for the final delamination of the layers (C2, P, M, CI) is achieved through a compressor, or in a controlled atmosphere chamber wherein the element (A) to be treated is immersed.

8. Process according to the previous claims, characterized in that the detachment of the layers (C2, P, M, Cl) of the element (A) is achieved by means of shear stresses distributed and transferred to said layers (C2, P, , Cl) via contact depression systems, or via mechanical cutting by means of a rigid clutch system affecting the thickness of the external layers (C2, P, Cl).

Description:
THERMO-MECHANICAL CONTROLLED CRYOGENIC DELAMINATION PROCESS FOR THE FULL RECOVERY OF RIGID MONO-, POLYCRYSTALLINE OR AMORPHOUS MATERIALS COATED WITH PLASTIC MATERIALS

DESCRIPTION

The object of the present invention is in the field of processes employed for end of life recovery of the raw materials employed in the manufacture of multilayer artifacts. More particularly, the object of the present invention is a cryogenic conditioning process for artifacts composed of multiple rigid material layers interspersed with materials having different thermal and elasticity characteristics and different stiffness.

As known, a good part of electronics and electrical waste, such as the artifacts described above, goes to landfill or alternatively undergoes incineration and recovery process without any preliminary treatment and therefore results in the subsequent dispersion into environment of highly polluting substances.

In contrast, many end of life electronic products could be reused, restored or recycled thus obtaining a clear benefit in protecting and safeguarding the environment and reducing pollution. Another advantage could derive from the recovery of materials that in many cases have a high economic value.

An example of an electronic system made with materials consisting of rigid layers alternated with plastic layers, i.e. the type to which it is possible to apply the process according to the present invention, and upon which much attention has recently been focused regarding its end of life disposal, is represented by photovoltaic modules.

At a structural level, photovoltaic modules are made from a sandwich of several layers joined together by means of a hot lamination process.

The main component of each module is represented by photovoltaic cells which are contained within a polymeric layer made of Ethylene Vinyl Acetate (EVA).

Said sandwich is constituted by a plurality of layers, adjacent to each other, namely: one rear polymeric waterproof coating layer, made according to requirement in either Ethylene Vinyl Acetate (EVA), polyethylene terephthalate (PET) or polyvinyl fluoride (Tedlar); a pair of layers approximately 0.6 mm thick realized in Ethylene Vinyl Acetate (EVA) that are protect the photovoltaic cells (said rigid layer); and a rigid front layer of tempered glass approximately 3 mm thick that serves as a protective surface that is also receptive to light. At the end of their operational life of around twenty to thirty years, each PV module can be subjected to a special treatment that allows for the safe disposal of toxic materials (usually metal) and that also allows for the recovery of some elements comprising the module, some of which are characterized by a high economic value (silicon and precious metals).

The prior art relating to end of life recycling processes and the treatment of photovoltaic panel parts that cannot be removed, as already mentioned, consists in recovering the rigid layers of material (electronic grade silicon) and plastic elements (copolymers) to be found in adjacent layers bound together by melting processes. This consists in a series of different processes, both from the technological and industrial points of view and from the point of view of the process outputs.

One of these processes for the recycling of photovoltaic modules, as described in Patent No. US6063995, involves the separation of the components that constitute the photovoltaic module by means of a baking process which raises its temperature, such as to melt only the polymeric component of the module, leaving unaltered the tempered glass and the photovoltaic cells themselves.

In particular said process provides the photovoltaic module, deprived of the outer frame and terminal blocks, to be initially heated to a temperature close to 100°C, thereby allowing for easy manual separation of the rear layer polymeric coating. It is then subsequently placed in an electric furnace where it undergoes a baking process at temperatures between 480°C and 540°C.

During the photovoltaic module baking process, in order to achieve an inert atmosphere, an inert gas, preferably nitrogen, is introduced into the oven through a feeder conduit.

The photovoltaic module baking process occurs at temperatures between 480°C and 540°C and for a period of time necessary for the degradation of the EVA polymeric layers.

When the two EVA polymeric layers reach melting temperature, physical separation of the photovoltaic cells occurs at which point, together with the tempered glass, they detach and rest on supports contained in the oven.

The gaseous decomposition products from the polymeric layers are subsequently burned within an afterburner producing as waste products carbon dioxide and water vapor.

Said process allows for the full recovery of the tempered glass and photovoltaic cells. The latter can then be subjected to further processing, such as cementing or acid attack so as to recover the silver or other metals present within the cells.

A further and different known process, which allows for the recycling of photovoltaic modules, is described in patent No. US6129779. It is based on a process that provides for the recycling and recovery of the metallic constituents of a photovoltaic module by crushing the photovoltaic module itself and subsequently dissolving out the metals in an acid solution bath. The solution thus obtained is then separated from the solid fragments and treated with a precipitating agent that then allows for the recovery of the metals obtained from the photovoltaic module.

More particularly, said process comprises a first step in which the photovoltaic module is crushed in order to obtain a plurality of fragments having a size sufficiently small to be chemically treated. The fragments of the module thus obtained are transferred to a container containing an acid, for example sulphuric acid, nitric acid or hydrochloric acid, which is capable of dissolving the metal material to be recovered thus separating it from the rest of the fragments. Upon the chemical reaction between the photovoltaic cell metals and the acid, the dissolution of the metal material occurs with the subsequent formation of a liquid phase consisting of metals combined with mordant acid and a solid phase formed by the non-metallic PV module fragments.

The solid phase present in the solution is then separated from the liquid phase by means of a filtration process, and on the contrary the non-metallic material contained in the solid phase is separated from the liquid phase by means of a vibrating screen.

Finally, in the last phase of the process, the recovery of the metals from the solution occurs. A method for separating the components within the solution consists in precipitating the metals in solution through the addition of a suitable chemical precipitating agent.

Another known photovoltaic module recycling process is described in patent No.

US5997718, relating to a procedure to recover the semiconductor metals from end of life photovoltaic modules by means of a "hydrometallurgical" process.

Upon the mechanical fragmentation of the photovoltaic module, the photovoltaic cells or any other photovoltaic waste is subjected to a leaching process that by means of an acid solution provides for the removal of all metals from the remaining photovoltaic module materials.

Before chemical treatment, the glass substrate is removed and can be thereafter further reused in the manufacture of photovoltaic modules or recycled or disposed of in landfill as non- hazardous waste.

The leaching solution is subsequently neutralized by mixing it with a basic compound containing a certain amount of calcium that leads to the formation of a solid precipitate of cadmium and tellurium.

Finally, the solid precipitate is subjected to a combustion process and subsequently cooled and washed in order to recover the cadmium oxide (CdO) and tellurium oxide (TeO). Finally, a further known process is described in patent No. DE102008058530A1, regarding a method for the recycling of photovoltaic modules and waste of photovoltaic origin, and in particular thin-film Cadmium Telluride and CIS solar cells. Specifically, this German patent provides information relating to a method for disassembling modules into their constituent elements so as to easily use them in the manufacture of new modules.

The method involves firstly that the photovoltaic modules, or parts thereof, in which the polymeric layer has not been structurally damaged, are subjected to a continuous or discontinuous mechanical crushing process by means of a vibrating disc mill.

The fragments thus obtained are then subjected to a chemical bath treatment at room temperature in a 15% hydrochloric acid solution wherein the complete dissolution of the metals contained within the fragments occurs. This phase is influenced by the amount of hydrogen peroxide (35% in weight) contained within the solution and is facilitated by the use of a suitable magnetic stirrer.

Finally, at the end of the metals dissolution process, the solution is filtered thus obtaining the recovery of the glass and polymers. These are subsequently subjected to a further process of washing thereby definitively recovering the glass and EVA.

The processes described in the prior art have a number of drawbacks, such as in the case of the hot photovoltaic module recovery processes that, despite making it possible to fully recover the photovoltaic cells and covering glass, involve high energy consumption.

With respect to recycling processes comprising module crushing and subsequent chemical bath, as such these processes do not allow for the recovery of higher added value photovoltaic module components and give rise, at the end of the process, to a series of fragments whose reintegration into the production cycle requires additional processing which is costly both from an economic and an environmental standpoint.

The purpose of this patent is to solve the drawbacks of the prior art by providing a process which allows for the recovery of rigid materials contained within artifacts composed of multiple rigid material layers interspersed with materials having different thermal and elasticity characteristics and different stiffness, with as such high added value or, as originally present in industrial type artifacts, minimizing the mechanical or chemical deterioration and therefore the need to proceed to subsequent treatments.

A further objective is to reduce the costs for the treatment of end of life fir multi-layer materials with different thermal and elastic features and for their reuse into the recovery processes currently in use. Another objective is to provide a process which allows for almost immediate reuse of the components and materials recovered by following the same process, thus lengthening the useful life of the components themselves and not requiring further treatment.

The process, object of the present invention, relates to a more sustainable methodology with therefore lower economic and environmental impact compared to the processes currently known in the field of recycling and/or the recovery of systems of the type in question such as, for example, the recovery of silicon cells contained in photovoltaic modules.

The operating principle of this treatment process does not preclude its application within different fields of application, as far as in the presence of separate layers consisting of rigid materials (e.g. metals) connected by interposing materials with different levels of stiffness and thermal conductivity (e.g. plastic or amorphous) minimizing chemical and/or destructive treatment without altering the geometrical structure or mechanical properties and exploiting the physical properties of materials that exhibit different expansion.

The thermo-mechanical controlled cryogenic delamination process for the full recovery of rigid mono-, polycrystalline or amorphous materials coated with plastic materials according to the present invention, is hereinafter described with the aid of accompanying drawings which respectively illustrate the following figures:

Fig. 1 is a block diagram of the process steps;

Fig. 2 is a cutaway view of a generic multilayer component;

Fig. 3 is an axonometric exploded view of a photovoltaic module;

Fig. 4 is an axonometric view of a photovoltaic module when subjected to the cryogenic cooling phase;

Fig. 5 is an axonometric view of a photovoltaic module when the layer of material to be recovered is subjected to the thermal and mechanical oscillation phase while at the same time maintaining the adjacent layers at cryogenic temperature;

Fig. 6 is an axonometric exploded view of a photovoltaic module when subjected to insufflation of liquid mixtures and the consequent final delamination of the layers;

Fig. 7 is a diagram illustrating the variations in temperature as a function of time during the course of the whole cryogenic process;

Fig. 8 are diagrams relating to changes in stress and mechanical deformation, temperature, deformations induced by vibrations brought about by the first natural frequency of resonance and relative forces applied as a function of time.

The thermo-mechanical controlled cryogenic delamination process according to the present invention, is based on a methodology that relies on the exploitation of the different thermal expansion characteristics of the plastic materials adjacent to rigid components (mono-, polycrystalline or amorphous in the case of photovoltaic panels) and the different ductility/brittleness curves that produce, possibly together with a simultaneous mechanical vibration, the same controlled thermo-mechanical delamination effect.

And in fact, the appropriate management of temperature transitions combined with mechanical actions induced by vibration at the first natural frequency of resonance is the mechanism that allows the separation of materials of different nature and characteristics, thus recovering at the end of the process the constituents of a multilayer element in such a state, that they can be used again without any special treatment, thus essentially obtaining an extension to the useful life of the component or its parts.

An example of an application of the process according to the present invention, is one that provides for the recovery of the electronic-grade silicon present within a photovoltaic module.

Thus, as illustrated in Figures 2 and 3 each photovoltaic module A consists of the following layers:

- a layer of silicon or different conductor or semiconductor material M;

- a pair of polymeric layer of Ethylene- vinyl-acetate P;

- a rear polymeric waterproof coating layer d;

- a front tempered glass layer C 2 .

As illustrated in Figure 1, the process involves the following steps:

- temperature stabilization and homogenization for a given time of all the component layers to be treated so that all the layers reach the same cryogenic temperature by placing said component in a conditioned environment: for example, a climatic chamber; in the case described, the multi-layer component is a photovoltaic module A.

- When the temperature is stable, there follows a period of swift or super swift cooling of the photovoltaic module A and in particular of the layers adjacent to the semiconductor material layer M, by means of a cryogenic cooling system 1 that provides for the continuous control of the flow rate and pressure of a cold carrier by means of a fluid compressor or other suitable system offering the possibility of temperature conditioning, as illustrated in Figures 4 and 7.

- The high cooling cryogenic system is equipped with a system that allows for the real-time control of the cooling conditions, namely, both the temperature and the flow rate of the refrigeration carrier. - As illustrated in Figures 5, 7 and 8, the second phase is followed by a phase during which thermal cycles at a controlled frequency is imposed upon the semiconductor material layer M (metallic, silicon). This produces a thermal differential between the layers at cryogenic temperature P and the semiconductor materials layer M at higher temperatures. In this way advantage is taken from the different mechanical expansion characteristics at different temperatures thereby producing a differential tangential stress between the various layers of the multilayer component A; this stress is defined as "thermal delamination stress or j".

- Said phase is realized by a selective system 2, providing heat to the high conductivity layer M only without warming the adjacent layers P which are of low thermal conductivity. The system 2 can be a contact system based on the Joule heating effect brought about by exploiting the cascade property of diodes, in the case of photovoltaic panels by superimposing a current which is greater than its resistance within the internal circuit or else by photonic excitation by contactless direct irradiation or any other equivalent system. Furthermore, always in the cooling condition of the module A and the simultaneous heating of the semiconductor layer M, it may be opportune, depending on the components, to apply cycles of bending stresses at controlled frequency of the entire element A or of the combination of layers to produce a secondary mechanical shear stress (here defined mechanical delamination stress or τ M ) between the semiconductor layer M and the contiguous layers P whose frequency is in phase with the thermal cycles and produce a total delamination stress which is synergic than the individual effects. The bending action resulting in the vibration of the element A is performed by suitable shaking systems 3.

- The following phase provides controlled delamination induced by the total effect of the thermal and mechanical delamination stress produced between the external layers P and the semiconductor layer M, producing a relative sliding action governed by the different planes of expansion τχοτ of the material being subject to the shearing force ττοτ = ττ+τΜ·

- In the last phase, the purpose of which is to obtain a final delamination of the layer P from the tempered glass C 2 , by means of suitable systems 4 a mixture of liquids at a controlled pressure and flow rate is introduced as shown in Figure 6 so as to allow for the final separation of the plastic parts from the rigid ones. This is due to the variation in the structural properties and bonding of said plastic materials (artificially induced aging mechanism).

At the end of the insufflation phase, the process continues with a mechanical separation phase of one or more external layers with respect to the semiconductor material layer M, by means of suitable mechanical systems suitable for producing stress that is both tangential and normal to the layer planes and induced into the them uy cumati systems lur example by contact depression systems 5, i.e. by mechanical cutting by means of a rigid stop system affecting the thickness of the external layers.