Irreversible temperature-responsive formation of high-strength hydrogel from an enantiomeric mixture of starburst triblock copolymers consisting of 8-arm PEG and PLLA or PDLA

2008 ◽  
Vol 46 (18) ◽  
pp. 6317-6332 ◽  
Author(s):  
Koji Nagahama ◽  
Kanae Fujiura ◽  
Shunsuke Enami ◽  
Tatsuro Ouchi ◽  
Yuichi Ohya
Langmuir ◽  
2016 ◽  
Vol 32 (21) ◽  
pp. 5314-5323 ◽  
Author(s):  
Sergey K. Filippov ◽  
Anna Bogomolova ◽  
Leonid Kaberov ◽  
Nadiia Velychkivska ◽  
Larisa Starovoytova ◽  
...  

Author(s):  
Asiya Mustafina ◽  
Julia Elistratova ◽  
Lucia Zakharova ◽  
Yuliana Kudryashova ◽  
Olga Bochkova ◽  
...  

2013 ◽  
Vol 46 (3) ◽  
pp. 1054-1065 ◽  
Author(s):  
Bernhard V. K. J. Schmidt ◽  
Martin Hetzer ◽  
Helmut Ritter ◽  
Christopher Barner-Kowollik

2017 ◽  
Vol 121 (18) ◽  
pp. 4885-4899 ◽  
Author(s):  
Josefine Eilsø Nielsen ◽  
Kaizheng Zhu ◽  
Sverre Arne Sande ◽  
Lubomír Kováčik ◽  
Dušan Cmarko ◽  
...  

2007 ◽  
Vol 80 (3) ◽  
pp. 533-544 ◽  
Author(s):  
G. R. Hamed

Abstract Principles of rubber reinforcement are discussed and new nomenclature is proposed to classify reinforced rubbers. The engineering tensile strength σb of amorphous, gum, non-crystallizable rubbers is only about σb≈3 MPa. These have no commercial use. However, if such rubbers contain enough stiff (hard or rigid) “entities” of density ρ and specific surface area S, such that 600/ρ m2/mL>S>60/ρ m2/mL, then σb>20 20 MPa. These rubbers are considered highly reinforced. The value of S for a stiff “entity” is largely dependent on its characteristic smallest dimension, d. For spheres or rods, d is diameter, and for plates, d is thickness. For all three shapes, the range of d corresponding to the limits of S given previously is approximately 100 nm>d>1 nm. Sometimes, the prefix nano- has been used to designate materials that contain stiff “entities” in this range of d. Other times, the prefix nano- has denoted a smaller range of d, 10 nm>d>1 nm. Thus, the term nano- is ambiguous in the literature. It is proposed to divide the size range, 1 nm<d<100 nm, of stiff “entities” into two ranges with different designations. When 10 nm>d>1 nm, the prefix proposed is nano-, and when 100 nm>d>10 nm, meso- is proposed as the prefix. This division may seem superfluous and arbitrary, but there is scientific merit for it. The way that the stiff “entities” come about provides criteria for further categorization. If the “entities” are (insoluble) particles that have similar d before and after incorporation (i.e., d is largely pre-determined) into an elastomer, then “composite” is the suffix proposed. But, if the stiff “entities” evolve and d depends on the kinetics and thermodynamics of phase separation, then the suffix is “structured.” Nomenclature for four types of rubber are then proposed: meso-composite, meso-structured, nano-structured and nano-composite. Commercial examples of the first three are known: black-filled SBR vulcanizates (meso-composite, σb≈20–30 MPa), SBS triblock copolymers (mesostructured, σb≈20–30 MPa), and elastomeric ionomers (nano-structured, σb≈50–60 MPa). Both meso-rubbers need about 20–25% (by volume) stiff “entity” to attain high reinforcement, whereas, only 2% stiff “entity” (ionic domains) imparts high reinforcement to nano-structured ionomers. Highly reinforced meso-rubber contains a higher concentration of stiff “entity” than that present in highly reinforced nano-rubber. However, in both meso- and nano-rubbers, the average distance between stiff “entities” is about 5 nm. This distance is similar to the spacing of crosslinks in vulcanizates that are optimally crosslinked. To the author's knowledge, no nano-composite rubber that is highly reinforced has been made. Nonetheless, the existence of high strength nano-structured ionomers suggests that highly reinforced nano-composites may be possible.


Author(s):  
Y. L. Chen ◽  
S. Fujlshiro

Metastable beta titanium alloys have been known to have numerous advantages such as cold formability, high strength, good fracture resistance, deep hardenability, and cost effectiveness. Very high strength is obtainable by precipitation of the hexagonal alpha phase in a bcc beta matrix in these alloys. Precipitation hardening in the metastable beta alloys may also result from the formation of transition phases such as omega phase. Ti-15-3 (Ti-15V- 3Cr-3Al-3Sn) has been developed recently by TIMET and USAF for low cost sheet metal applications. The purpose of the present study was to examine the aging characteristics in this alloy.The composition of the as-received material is: 14.7 V, 3.14 Cr, 3.05 Al, 2.26 Sn, and 0.145 Fe. The beta transus temperature as determined by optical metallographic method was about 770°C. Specimen coupons were prepared from a mill-annealed 1.2 mm thick sheet, and solution treated at 827°C for 2 hr in argon, then water quenched. Aging was also done in argon at temperatures ranging from 316 to 616°C for various times.


Author(s):  
L.J. Chen ◽  
H.C. Cheng ◽  
J.R. Gong ◽  
J.G. Yang

For fuel savings as well as energy and resource requirement, high strength low alloy steels (HSLA) are of particular interest to automobile industry because of the potential weight reduction which can be achieved by using thinner section of these steels to carry the same load and thus to improve the fuel mileage. Dual phase treatment has been utilized to obtain superior strength and ductility combinations compared to the HSLA of identical composition. Recently, cooling rate following heat treatment was found to be important to the tensile properties of the dual phase steels. In this paper, we report the results of the investigation of cooling rate on the microstructures and mechanical properties of several vanadium HSLA steels.The steels with composition (in weight percent) listed below were supplied by China Steel Corporation: 1. low V steel (0.11C, 0.65Si, 1.63Mn, 0.015P, 0.008S, 0.084Aℓ, 0.004V), 2. 0.059V steel (0.13C, 0.62S1, 1.59Mn, 0.012P, 0.008S, 0.065Aℓ, 0.059V), 3. 0.10V steel (0.11C, 0.58Si, 1.58Mn, 0.017P, 0.008S, 0.068Aℓ, 0.10V).


Author(s):  
L. S. Lin ◽  
C. C. Law

Inconel 718, a precipitation hardenable nickel-base alloy, is a versatile high strength, weldable wrought alloy that is used in the gas turbine industry for components operated at temperatures up to about 1300°F. The nominal chemical composition is 0.6A1-0.9Ti-19.OCr-18.0Fe-3Mo-5.2(Cb + Ta)- 0.1C with the balance Ni (in weight percentage). The physical metallurgy of IN 718 has been the subject of a number of investigations and it is now established that hardening is due, primarily, to the formation of metastable, disc-shaped γ" an ordered body-centered tetragonal structure (DO2 2 type superlattice).


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