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SAE/TP - 2010-01-1765 - SOH RECOGNITION OF LI-ION AVIATION BATTERIES VIA PASSIVE DIAGNOSTIC DEVICE Organization: SAE/TP
Date: 2010-11-02
Description: Nickel-Cadmium (NiCd), Valve Regulated Lead-Acid (VRLA), or Lithium-Ion (Li-ion) batteries are used to start engines, provide emergency back-up power, and assure ground power capability for maintenance and pre-flight checkout.
SAE PAPER 2013-01-0213 - FIRE FIGHTING OF LI-ION TRACTION BATTERIES Organization: SAE
SAE PAPER 2010-01-1074 - AVAILABLE POWER AND ENERGY PREDICTION USING A SIMPLIFIED CIRCUIT MODEL OF HEV LI-ION BATTERY Organization: SAE
SAE PAPER 2013-01-0242 - LI-ION AIR-COOLED BATTERY SYSTEM INTERACTIONS WITH THE VEHICLE HVAC SYSTEM Organization: SAE
SAE/TP - 2008-01-2894 - PRISMATIC LI-ION CELL FOR UNMANNED AIRCRAFT Organization: SAE/TP
Date: 2008-11-11
Description: Saft is working on advanced 28V Li-ion batteries for use in NAVY unmanned aircraft applications. This battery employs seven (7) prismatic state-of-the art Li-ion cells connected in series.
SAE/TP - 2008-01-2921 - NEXT GENERATION LI-ION TECHNOLOGY FROM SAFT Organization: SAE/TP
Date: 2008-11-11
Description: This work is funded by US Army TACOM and is continuation of US Air Force AFRL sponsored effort aimed at meeting the needs of both aircraft power as well as emerging Directed Energy applications. Ultra High Power (UHP) Li-ion cells offer unparalleled continuous and pulse power.
IEEE 1725 - RECHARGEABLE BATTERIES FOR CELLULAR TELEPHONES Organization: IEEE
Date: 2011-05-16
Description: This standard establishes criteria for design analysis for qualification, quality, and reliability of rechargeable lithium-ion (Li-Ion) and lithium-ion polymer (Li-Ion polymer) batteries for cellular telephone applications.
SAE AIR5561 - LITHIUM BATTERY POWERED PORTABLE ELECTRONIC DEVICES Organization: SAE
Date: 2013-10-01
Description: Purpose This AIR is prepared to bring attention to what is considered a potential shortcoming of current standards related to the usage of lithium-ion (Li-Ion) battery powered portable devices onboard aircraft. While work has been completed by other groups to develop standards for permanently installed, rechargeable lithium batteries, there is currently no aerospace standard for lithium battery powered portable electronic devices that are intended to be used in conjunction with flight operations.
SAE/TP - 2008-01-2895 - ADVANCED FEF3 CATHODE ENABLED LITHIUM-ION BATTERY Organization: SAE/TP
Date: 2008-11-11
Description: At present Li-ion batteries are the premier rechargeable energy storage technology and they offer a promising future as a power source for high energy density battery applications.
IEEE 1625 - RECHARGEABLE BATTERIES FOR MULTI-CELL MOBILE COMPUTING DEVICES Organization: IEEE
Date: 2008-09-26
Description: This standard covers rechargeable battery systems for mobile computing. The battery technologies covered are limited to Li-ion and Li-ion polymer, but future versions of this standard may include technologies that are not in general use at present.
SAE/TP - 2010-01-1762 - SOH RECOGNITION OF AVIATION BATTERIES VIA PASSIVE DIAGNOSTIC DEVICE Organization: SAE/TP
Date: 2010-11-02
Description: Nickel-Cadmium (NiCd), Valve Regulated Lead-Acid (VRLA), or prospective Li-ion batteries are used to start engines, provide emergency back-up power, and assure ground power capability for maintenance and pre-flight checkout.
SAE/TP - 2008-01-2933 - STATE OF HEALTH RECOGNITION FOR AIRCRAFT BATTERIES DYNAMIC EQUIVALENT SCHEMATIC AND FIRST PRINCIPLES MODEL CONSIDERATIONS Organization: SAE/TP
Date: 2008-11-11
Description: NiCd, VRLA, or prospective Li-ion batteries are used to start engines, provide emergency back-up power, and assure ground power capability for maintenance and pre-flight checkout.
NASA-LLIS-2046 - LESSONS LEARNED – LIMITATIONS OF INTERNAL PROTECTIVE DEVICES IN HIGH-VOLTAGE/HIGH- CAPACITY BATTERIES USING LITHIUM-IO Organization: NASA
Date: 2009-05-11
Description: Abstract: Most commercial cylindrical 18650 Lithium-Ion (Li-Ion) cells have two internal protective devices: the Positive Temperature Coefficient (PTC) and the Current Interrupt Device (CID).
SAE/TP - 2006-01-3022 - CELL EQUALIZATION OF LITHIUM ION CELLS Organization: SAE/TP
Date: 2006-11-07
Description: With increased use of Lithium-Ion (Li-ion) batteries in military and space applications, it is important to understand individual cell performance.
SAE/TP - 2009-01-3191 - ELECTROCHEMICAL TESTING AT SAFT TO SUPPORT HEALTH PROGNOSTICATION MANAGEMENT FOR AVIATION Organization: SAE/TP
Date: 2009-11-10
Description: Lithium ion batteries offer more power and longer cycle life than traditional technologies for many different applications. However, Li-ion batteries are new in the aviation applications and due to the lack of experience they are preventively removed from service before any problems may occur with the battery.
SAE J2990 - HYBRID AND EV FIRST AND SECOND RESPONDER RECOMMENDED PRACTICE Organization: SAE
Date: 2012-11-01
Description: Nickel metal hydride (NiMH) and lithium ion (Li-ion) batteries used for vehicle propulsion power are the assumed battery systems of this RP.
SAE/TP - 2006-01-3024 - EVALUATION OF LIFE CYCLE PERFORMANCE OF LITHIUM ION CELLS FOR SPACE APPLICATIONS Organization: SAE/TP
Date: 2006-11-07
Description: This paper describes a program at Boeing Phantom Works designed to evaluate life cycle performance of Lithium -Ion (Li-Ion) cells. The objective was to gather data, which will give us the capability to assess the performance of these cells during typical space missions.
DNVGL-RP-0043 - SAFETY, OPERATION AND PERFORMANCE OF GRID-CONNECTED ENERGY STORAGE SYSTEMS Organization: DNVGL
Date: 2015-12-01
Description: These aspects will be assessed for electricity storage systems in general, but also with emphasis on certain battery technologies (lead-acid, Li-ion and redox flow) and Li-ion capacitors. Other storage technologies, like flywheels, pumped hydro storage, compressed air and supercapacitors, are included in more general terms.
SAE/TP - 2010-01-1756 - A MODULAR POWER SYSTEM ARCHITECTURE FOR MILITARY AND COMMERCIAL ELECTRIC VEHICLES Organization: SAE/TP
Date: 2010-11-02
Description: A prototype SPU design using a high energy density Li-ion cell has been developed and is presented here with proof-of-concept simulation results, comparisons to existing architectures, and a discussion of its advantages and disadvantages when compared with conventional systems.
SAE/TP - 2010-01-1766 - FAULT MITIGATION AND CELL BALANCING OF HIGH POWER LITHIUM ION BATTERY PACKS Organization: SAE/TP
Date: 2010-11-02
Description: In order to address this situation, the authors are developing an advanced battery management system for LI battery packs that ensures adequate, safe, and reliable operation.

1 - 20 of 22 results