Browse Topic: Solid state batteries

Items (21)
This SAE Recommended Practice provides a set of test methods and practices for the characterization of lithium ion battery cathode active material. It is beyond the scope of this document to establish criteria for the test results, as these are usually established between the vendor and customer. It should be noted that materials properties can vary substantially between classes of materials (e.g., LNO and LFP) and caution should be exercised when attempting to directly compare their chemical and physical properties. While these distinctions are important for the manufacturer, this document focuses on the techniques to measure the materials properties and not their absolute or relative values. Future materials such as solid-state batteries and sulfides are beyond the scope of this document. It is beyond the scope of this document to examine the rheological properties of the cathode material dispersed in a coating slurry since such properties are influenced by the conductive additive, binder, and solvent, which are determined by the coating process. It is beyond the scope of this document to examine the electrochemical properties of cathode materials since these are influenced by electrode and ultimately cell design. Due to the difference in electrical and electrochemical properties of the cathode material, it is unrealistic to establish an electrode and cell design that would justly compare different cathode active materials.
Battery Materials Testing Committee
Energetic, Environmental and Range Estimation of Hybrid and All-Electric Transformation of an Existing Light Utility Commuter Aircraft2018-01-193310/30/2018
Today it is necessary to face the energetic, environmental, and safety-related issues of a significant industrial sector such as aeronautic one. It is a marginal contributor to today global GHG emissions (less than 3%), In any case, the associated impacts grows with the increase of air traffic with annual rate 5%. Consequently, aviation will need to face four fundamental problems for the future: 1 the overall impact of aviation is expected to grow up to 10÷15% of global GHG emissions by 2050; 2 the emissions of pollutants by commercial aviation affects the fragile atmospheric layers in the low stratosphere; 3 the increasing age of the flying fleet deals with increasing maintenance and safety issues; 4 the dependence on fossil fuels relates to problems of geopolitical instability and consequence volatility of prices. Substantial innovations are expected for both reducing energy consumption and environmental impacts of aviation and reducing the age of the fleets. They mostly relate to the decrease of weights and the introduction of environmental friendly propulsion systems, such as hybrid and all-electric propulsion. This paper will produce an assessment of different propulsive systems according to the first law of thermodynamics and environmental impacts. It assumes a well-tested light transport/commuter aircraft as reference architecture and produces a comparative analysis of different green propulsion systems including all electric and hybrid against actual aircrafts. The analysis assumes that the electric or hybrid configurations may not increase the overall mass of the aircraft. Energy model has been reformulated for the different configurations and considers both an analytical model based on basic flight mechanics and a new formulation of the Breguet range equation, which has been specifically formulated for both hybrid and all-electric airplanes.
Trancossi, MichelePascoa, Jose
Multifunctional Fiber Batteries for Next Generation Space Suits2008-01-19966/29/2008
As next generation space suit concepts enable extravehicular activity (EVA) mission capability to extend beyond anything currently available today, revolutionary advances in life support technologies are required to achieve anticipated NASA mission profiles than may measure years in duration and require hundreds of sorties. Since most life support systems require power, increased mass and volume efficiency of the energy storage materials can have a dramatic impact on reducing the overall weight of next generation space suits. ITN Energy Systems, in collaboration with Hamilton Sundstrand and the NASA Johnson Space Center's EVA System's Team, is developing multifunctional fiber batteries to address these challenges. By depositing the battery on existing space suit materials, e.g. scrim fibers in the thermal micrometeoroid garment (TMG) layers, parasitic mass (inactive materials) is eliminated leading to effective energy densities ∼400 Wh/kg. The solid-state nature of the fiber battery also provides: Outstanding cycle life: >10,000 cycles, High rate: Near full capacity charge in ∼10 min., and Improved safety and packaging efficiency by eliminating liquid electrolytes. This paper highlights recent development of the multifunctional energy storage for EVA Systems. Advances in the performance of solid-state batteries on fiber/ribbon substrates are presented as well as design considerations for the integration of this technology into advanced EVA systems. Preliminary results are provided for an initial demonstration of the benefits of this technology by powering space suit health monitoring sensors with multifunctional energy storage devices. As wireless sensors are becoming of increased importance to NASA missions in general, this technology is expected to have wide spread application beyond the advanced EVA systems.
Berland, BrianLanning, BruceHodgson, EdwardQuinn, GregoryBue, GrantTrevino, Luis
Multifunctional Fiber Batteries for Next Generation Space Suits2007-01-31737/9/2007
As next generation space suit concepts enable extravehicular activity (EVA) mission capability to extend beyond anything currently available today, revolutionary advances in life support technologies are required to achieve anticipated NASA mission profiles that may measure years in duration and require hundreds of sorties. Since most life support systems require power, increased mass and volume efficiency of the energy storage materials can have a dramatic impact on reducing the overall weight of next generation space suits. This paper details the development of a multifunctional fiber battery to address these needs. The fiber battery is based on a solid-state lithium technology that is fully rechargeable and provides: (1) greater than 10,000 cycles at 100% depth of discharge at 95% of initial capacity; (2) high rates (full capacity charge or discharge in ∼10 minutes); (3) improved safety and packaging efficiency by eliminating liquid electrolytes; and (4) flexible integration schemes that allow the battery to be fabricated on/in space suit materials or components. By depositing the battery on existing space suit fibers (e.g., scrim fibers in the thermal micro-meteoroid garment (TMG) layer) parasitic mass (inactive material) is eliminated, leading to dramatically higher energy densities (∼400 Wh/kg). The high surface area to volume packing efficiency of fiber batteries compared to planar configurations further enhances the energy storage efficiency.
Berland, BrianLanning, BruceHodgson, EdwardQuinn, GregoryBue, GrantTrevino, Luis
Advanced Lithium Solid State Battery Developments2000-01-15884/2/2000
This paper presents a summary of a recent conference entitled Advanced Lithium Solid State Batteries Workshop that was held on July 13–15, 1999. The conference was sponsored by the Department of Energy's Office of Advanced Automotive Technologies, and the Office of Basic Energy Sciences' (BES) Division of Chemical Sciences. This paper presents a summary of the results and recommendations from the conference, including: A review of current research on solid state electrolytes and their interfaces with an emphasis on both applied and basic studies. The research includes theoretical studies of solid polymer electrolytes (SPEs), lithium ion transport in SPEs, and simulations of the electrolyte–cathode interface. Experimental results are presented on ion transport phenomena in SPEs (NMR and X–ray) and mechanical stresses on electrodes, among other topics. The issues addressed center on improved stability of and transport at interfaces, improved conductivity in the SPE, and higher transference numbers. A synopsis of problem areas and barriers to future progress in this field, the solution to which would benefit from both new theoretical treatment and the application of recent advances in experimental techniques. A summary of the recommendations and suggestions of the workshop participants are presented, organized into programmatic and technical recommendations and suggestions.
Deppe, JohnHeitner, KennethDuong, TienMaupin, Paul H.Landgrebe, Albert
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