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Book

SAE International Journals Complete Set
2010-04-30
This set includes: SAE International Journal of Aerospace March 2010 - Volume 2 Issue 1 SAE International Journal of Commercial Vehicles October 2009 - Volume 2, Issue 1 March 2010 - Volume 2, Issue 2 SAE International Journal of Engines October 2009 - Volume 2, Issue 1 March 2010 - Volume 2, Issue 2 SAE International Journal of Fuels and Lubricants October 2009 - Volume 2, Issue 1 March 2010 - Volume 2, Issue 2 SAE International Journal of Materials and Manufacturing October 2009 - Volume 2, Issue 1 March 2010 - Volume 2, Issue 2 SAE International Journal of Passenger Cars - Electronic and Electrical Systems October 2009 - Volume 2, Issue 1 SAE International Journal of Passenger Cars - Mechanical Systems October 2009 - Volume 2, Issue 1 March 2010 - Volume 2, Issue 2
Journal Article

Laser-Assisted Filler-Based Joining for Battery Assembly in Aviation
2020-10-19
Abstract A key problem of the construction of fully electric aircraft is the limited energy density of battery packs. It is generally accepted that this can only be overcome via new, denser battery chemistry together with a further increase in the efficiency of power utilization. One appealing approach for achieving the latter is using laser-assisted filler-based joining technologies, which offers unprecedented flexibility for achieving battery cell connections with the least possible electrical loss. This contribution presents our results on the effect of various experimental and process parameters on the electrical and mechanical properties of the laser-formed bond.
Journal Article

Carbon Fiber/Epoxy Mold with Embedded Carbon Fiber Resistor Heater - Case Study
2018-04-07
Abstract The paper presents a complete description of the design and manufacturing of a Carbon Fiber/epoxy mold with an embedded Carbon Fiber resistor heater, and the mold performances in terms of its surface temperature distribution and thermal deformations resulting from the heating. The mold was designed for manufacturing aileron skins from Vacuum Bag Only prepreg cured at 135°C. The glass transition temperature of the used resin-hardener system was about 175°C. To ensure homogenous temperature of the mold working surface in the course of curing, the Carbon Fiber heater was embedded in a layer of a highly heat-conductive cristobalite/epoxy composite, forming the core of the mold shell. Because the cristobalite/epoxy composite displayed much higher thermal expansion than CF/epoxy did, thermal stresses could arise due to this discrepancy in the course of heating.
Collection

Recent Developments in Aerospace Automated Fastening/Assembly & Tooling 2010
2010-09-20
This technical paper collection contains 14 papers focusing on automated robotic drill and fastening systems; automation and automated fastening technologies; large component assembly sub-assembly, major section and final assembly; enhanced fasteners; assembly methodologies and advanced assembly fixtures and tooling; and composite assembly and fastening.
Collection

Recent Developments in Aerospace Manufacturing, Materials, and Structures 2010
2010-09-20
The 18 papers in this technical paper collection focus on aircraft coatings technologies; advanced metal materials, fabrication, and joining processes; advanced low cost aircraft structures; advanced robotics and automation applications; information technologies; structural health monitoring; lean manufacturing integration; metrology automated systems; high output composites; RFID applications in aerospace; hybrid metal/composite drilling and assembly; and environmental compliance, green and sustainable applications.
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