| Literature DB >> 29861993 |
Pascal G Yot1, Louis Vanduyfhuys2, Elsa Alvarez3,4, Julien Rodriguez5, Jean-Paul Itié6, Paul Fabry3, Nathalie Guillou3, Thomas Devic3, Isabelle Beurroies6, Philip L Llewellyn6, Veronique Van Speybroeck2, Christian Serre3, Guillaume Maurin1.
Abstract
The aluminum fumarate MOF A520 or MIL-53-FA is revealed to be a promising material for mechanical energy-related applications with performances in terms of work and heat energies which surpass those of any porous solids reported so far. Complementary experimental and computational tools are deployed to finely characterize and understand the pressure-induced structural transition at the origin of these unprecedented levels of performance.Entities:
Year: 2015 PMID: 29861993 PMCID: PMC5952545 DOI: 10.1039/c5sc02794b
Source DB: PubMed Journal: Chem Sci ISSN: 2041-6520 Impact factor: 9.825
Fig. 1Schematic representation of the pressure-induced contraction of MIL-53(Al)–FA between an open and a contracted form.
Fig. 2Cumulative volume of intruded mercury in two intrusion–extrusion cycles as a function of the applied pressure obtained for the dehydrated MIL-53(Al)–FA solid (Vinitial and Vfinal are the volumes of mercury intruded before and after the contraction of the solid respectively).
Fig. 3X-ray powder diffraction patterns of MIL-53(Al)–FA as a function of the applied pressure (λ = 0.37380 Å). Patterns in black correspond to the pure open form, blue corresponds to a mixture of open and contracted pore forms (* indicates the diffraction peaks assigned to the contracted form) and red corresponds to the contracted form although the presence of a small concentration of the open form is likely to occur.
Comparison of the work energy performance of MIL-53(Al)–FA with that of other porous solids
| Work (J g–1) |
| Reference | |
| MIL-53(Al)–FA | 60 | 110 | This work |
| MIL-53(Al)–BDC | 7 | 18 |
|
| MIL-53(Cr)–BDC | 16 | 55 |
|
| MIL-47(V)–BDC | 33 | 125 |
|
| ZIF-8 | 13.3 | — |
|
| Silicalite | 11 | — |
|
| SBA-15 mesoporous silica | 4.3–6.1 | — |
|
Fig. 4Volume variation of MIL-53(Al)–FA as a function of the applied oil pressure during three compression–decompression cycles.
Experimental energetic data of compression/decompression cycles on the MIL-53(Al)–FA
| Work (J g–1) | Heat (J g–1) | Internal energy (J g–1) | |
| Cycle 1: compression | 41.7 | –25.1 | 16.6 |
| Cycle 1: decompression | –10.8 | 6.4 | –4.4 |
| Cycle 2: compression | 22.9 | –18.7 | 4.2 |
| Cycle 2: decompression | –8.0 | 6.3 | –1.7 |
| Cycle 3: compression | 22.2 | –18.2 | 4.0 |
| Cycle 3: decompression | –8.8 | 6.5 | –2.3 |
Fig. 5Heat energy obtained for MIL-53(Al)–FA as a function of the pressure during the first cycle release. Red upwards-pointing triangles correspond to compression and blue downwards-pointing triangles correspond to decompression.