Auto‐Oxygenated Porphyrin‐Derived Redox Mediators for High‐Performance Lithium Air‐Breathing Batteries

2022 ◽  
pp. 2103527
Author(s):  
Hyun‐Soo Kim ◽  
Boran Kim ◽  
Hyunyoung Park ◽  
Jongsoon Kim ◽  
Won‐Hee Ryu
2016 ◽  
Vol 41 (21) ◽  
pp. 9191-9196 ◽  
Author(s):  
Zi'ang Xiong ◽  
Shijun Liao ◽  
Sanying Hou ◽  
Haobin Zou ◽  
Dai Dang ◽  
...  

2002 ◽  
Vol 68 (9) ◽  
pp. 4341-4349 ◽  
Author(s):  
Andreas Keck ◽  
Jörg Rau ◽  
Thorsten Reemtsma ◽  
Ralf Mattes ◽  
Andreas Stolz ◽  
...  

ABSTRACT During aerobic degradation of naphthalene-2-sulfonate (2NS), Sphingomonas xenophaga strain BN6 produces redox mediators which significantly increase the ability of the strain to reduce azo dyes under anaerobic conditions. It was previously suggested that 1,2-dihydroxynaphthalene (1,2-DHN), which is an intermediate in the degradative pathway of 2NS, is the precursor of these redox mediators. In order to analyze the importance of the formation of 1,2-DHN, the dihydroxynaphthalene dioxygenase gene (nsaC) was disrupted by gene replacement. The resulting strain, strain AKE1, did not degrade 2NS to salicylate. After aerobic preincubation with 2NS, strain AKE1 exhibited much higher reduction capacities for azo dyes under anaerobic conditions than the wild-type strain exhibited. Several compounds were present in the culture supernatants which enhanced the ability of S. xenophaga BN6 to reduce azo dyes under anaerobic conditions. Two major redox mediators were purified from the culture supernatants, and they were identified by high-performance liquid chromatography-mass spectrometry and comparison with chemically synthesized standards as 4-amino-1,2-naphthoquinone and 4-ethanolamino-1,2-naphthoquinone.


2016 ◽  
Vol 332 ◽  
pp. 413-419 ◽  
Author(s):  
Huanhuan Zhang ◽  
Jinyu Li ◽  
Cheng Gu ◽  
Mingming Yao ◽  
Bing Yang ◽  
...  

Small ◽  
2021 ◽  
pp. 2102072
Author(s):  
Ahmad Jaradat ◽  
Chengji Zhang ◽  
Sachin Kumar Singh ◽  
Junaid Ahmed ◽  
Alireza Ahmadiparidari ◽  
...  

Author(s):  
J. V. Taylor ◽  
F. Flanagan ◽  
A. Dunlop ◽  
S. D. Grimshaw ◽  
R. J. Miller

Abstract Air breathing rocket engines require turbomachinery and ducting that is substantially lighter than that used in ground based or aerospace gas turbines. In order to reduce the weight of the axial compressor, the design of the inter-spool swan neck duct is targeted. In this paper a circumferential splitter blade is used to reduce loading and diffusion on the duct endwalls. The splitter and duct geometry are coupled and optimised together using 2D CFD. A design is selected that is 30% shorter than ducts that are currently used in aerospace gas turbines and the 3D flow features are investigated in further detail using an experimental rig and 3D CFD. This paper shows that the “splittered” duct has 3 benefits over a conventional duct design: First, separation of the endwalls is prevented even at short duct lengths, this will reduce distortion into the downstream compressor. Second, losses generated by corner separations on structural struts can be reduced by 20%, enabling short ducts to achieve high performance. Third, splittered ducts are shown to be twice as robust to uncertain inlet flow conditions as conventional ducts. This allows a designer to target high performance short designs with reduced risk.


Author(s):  
Steven F. Perry ◽  
Markus Lambertz ◽  
Anke Schmitz

This chapter introduces the ‘who has what’ in terms of air-breathing respiratory faculties for craniotes. Air breathing has arisen independently dozens of times among ray-finned fishes, but none has become completely terrestrial. The lobe-finned fishes eventually gave rise to amphibians and amniotes, and we see an increased importance of primarily lung-based air breathing. A muscular mechanism for lung ventilation (a buccal pump in amphibians and primarily a negative pressure aspiration mechanism in amniotes), pulmonary veins that return oxygenated blood to the heart, and some mechanism for partial or complete separation of oxygenated and deoxygenated blood masses at the heart are seen. Each major tetrapod group, in fact, has its own specific breathing mechanism. The chapter examines in some detail low-performance and high-performance faculties, the latter being particularly realized in the diaphragm-powered, ventilated pool system of the mammalian bronchoalveolar lung, and in the cross-current system of the avian lung–air sac system.


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