Senior Design : Shape Conformable Battery Pack

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Presentation transcript:

Senior Design : Shape Conformable Battery Pack Sponsor: Dr.Zheng Advisor: Dr.Shih Team Members: Jenna Pine Niraj Thakker Jianchen Yu David Goss Roberto Moutran Brian Rainbeau 11/12/2018

Battery CRASH COURSE Jenna Pine

What’s the project about? Project Description What’s the project about? Objective Constraints Build a battery that can be integrated into the wing of a UAV system Develop uniquely shaped battery or formable battery The battery must satisfy the power need of the RC plane Battery is to be detachable for charging Limited project Budget Limited research or experience available Battery must not explode or catch fire Enough power must be supplied for at least a 5 minute flight without switching batteries or recharging Jenna Pine

House of Quality Roberto Moutran

What is a lithium pouch cell battery? Introduction What is a lithium pouch cell battery? Cathode sheets consist of Lithium Iron Phosphate ( LiFePO 4 ) spread over an Aluminum Sheet Anode Sheets consist of graphite spread over a copper sheet Roberto Moutran

Design Concept for battery Concept 1: Thin C-Shaped Pouches Create many thin layered batteries and seal them independently Pros Easy to seal Making the batteries thin increases their bendability Cons Bending pouches may result in loss of electrolyte conductivity Sharp bending angle may impair electrolyte flow David Goss

Design Concept for battery Concept 2: Single Pouch Require different size anode and cathode sheets Pros True conformability Cons High risk of shorting the battery Vacuum sealing will be difficult due to the shape of the pack. David Goss

Design Concept for battery Concept 3: Individual Cell Pouches Make individual batteries and connect them in series/parallel Pros Easiest to manufacture No loss of electrolyte conductivity from bending Cons Longer manufacturing time Not the most creative design David Goss

Design Concept for Plane Wing over Body Wings to the side Pros More Support for the heavy wings Having a single wing makes the attachment and detachment process easier Conformable battery placement is more flexible Cons Support rods add additional weight, which increase the power requirement Rods will also increase the induced drag Less induced drag Weigh’s less, since there are no additional support components Attachable/detachable wing will be unstable Less flexibility for placing the conformable battery Jianchen Yu 11/12/2018

Analysis of the airfoil How are we going to analyze Lift on the airfoil? Assumptions Thin Air Foil (To use Kutta-Condition for coefficient of Lift) Laminar Flow Experimental Analysis Placing the airfoil in the wind tunnel Computing lift at different angles of attack Theoretical Analysis Use 2-D Finite Element Model for a flow over an airfoil Use natural boundary condition to set up the model Jianchen Yu

Selection of battery Material What kind of Lithium Battery are we going to choose? Two choices : Lithium Ion and Lithium Solid Polymer. Light-weight, Rechargeable and High capacity Lithium Ion Lithium Polymer Pros Commercially available materials Access to battery lab Cons Lower specific energy Less shape conformable High specific energy Shape conformable Materials are harder to find No production facility available Since Lithium Ions materials are readily available, Lithium Ion will be selected Brian Rainbeau

Selection of battery Material Types of Lithium Ion Batteries Three Prevalent types of Lithium Ion Battery cathode. Lithium-cobalt dioxide (LiCoO2) Lithium-manganese oxide (LiMn2O4) Lithium iron phosphate (LiFePO4) Of these three LiCoO2 and LiFePO4 offer higher specific energy, but LiFePO4 is roughly half the cost of LiCoO2 (Iron is more common than cobalt) Choices for ready made Anode and Electrolyte materials were limited to Graphite and Lithium Salt (Lithium hexafluorophosphate) Brian Rainbeau

Analysis of battery material How much material is needed to produce the required power? The plane is equipped with a 11.1V, 3200mAh battery which weights 309 g Electrode Volts Capacity (mAh/cm2) material to achieve 3200mAh (cm2) material to achieve 3200mAh, 11.1V (cm2) anode + substrate weight per cm2 (g) cathode + substrate weight per cm2 (g) weight needed total(g) Electrolyte needed total(g) 3200mAh 11.1V cell weight no package (g) LiFePO4 3.45 2.42 1322.31 4254.40 0.03 0.02 205.63 102.81 308.44 We need 4254cm2 of each electrode and 102.81g of electrolyte Brian Rainbeau

What designs did we choose? Summary What designs did we choose? Based on house of quality we choose For battery housing Concept 1: Thin-C shaped Pouches Concept 3: Individual Cell Pouches For plane Concept 1: Wing over the body For battery material(Cathode) LiFePo4 Niraj Thakker

Future Works What’s next? Analyzing the power output of each of the battery shape concepts Analyzing the placement of the battery in the wing Designing various concepts to attach and detach the wing from the plane Analyzing different combinations of series and parallel connection to obtain the required output Niraj Thakker

References Niraj Thakker 1Amin, D. (2013, August). EML4551C-Senior Design Project 1 . Retrieved September 22, 2013, from Blackboard: https://campus.fsu.edu/webapps/portal/frameset.jsp?url=%2Fwebapps%2Fblackboard%2Fexecut e%2Flauncher%3Ftype%3DCourse%26id%3D_6389491_1%26url%3D 2Ismail, M. H. (2003). Designing lithium ion batteries for high power applications. PECon 2003 National Proceedings, (pp. 289 – 291). 3Kam, K. C. (2012). Electrode Materials for Lithium Ion Batteries. Material Matters. 4Linden, D. (2002). Handbook of Batteries. New York: McGraw-Hill. 5Server Experts. (2011). LiPo Batteries and Charging for your Model RC Airplane. Retrieved September 21, 2013, from L.I. Foam Flyers: http://www.longislandelectricrcairplanes.com/learnbatteries.php 6Unknown. (2010, October). Learn about Batteries. Retrieved September 21, 2013, from Battery University: http://batteryuniversity.com/learn/article/is_lithium_ion_the_ideal_battery 7Unknown. (2012). BYD Company Limited. Retrieved 10 19, 2013, from http://bydit.com/doce/products/Li- EnergyProducts/ 8Unknown. (2013, 10 20). Apprentice S 15e RTF. Retrieved from HobbyZone: http://secure.hobbyzone.com/EFL3100.html 9Zheng, H., Liu, G., Crawford, S., & Battaglia, V. S. (2010). Fabrication Procedure for Lithium-ion Rechargeable Coin Cells. Berkeley: Lawrence Berkeley National Laboratory. Niraj Thakker

Questions?? Niraj Thakker