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Preparation of Thick NI/AL Reactive Multilayer Films and Prospective Use for Self-Powered Brazing of TI-6AL-4V

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dc.contributor.author Bar-Cohen, Yoseph
dc.contributor.author Bridges, Denzel
dc.contributor.author Ma, Ying
dc.contributor.author Smith, Cary
dc.contributor.author Zhang, Zhi-Li
dc.contributor.author Hu, Anming
dc.contributor.author Rouleau, Christopher
dc.contributor.author Gosser, Zachary
dc.contributor.author Hong, Kunlun
dc.contributor.author Cheng, Jinquan
dc.date.accessioned 2020-04-28T15:30:03Z
dc.date.available 2020-04-28T15:30:03Z
dc.date.issued 2018-06-18
dc.identifier.citation 46th North American Manufacturing Research Conference, College Station, Texas, June 18 - 22, 2018 en_US
dc.identifier.clearanceno 18-1568
dc.identifier.uri http://hdl.handle.net/2014/48103
dc.description.abstract In this study we demonstrate a new method for depositing thick reactive multilayer films (RMFs) (thickness > 14 µm) by using Ti interlayer integration and substrate preheating during fabrication. These two adjustments are designed to alleviate internal planar stresses that cause delamination between deposited layers and peeling off the substrate. Decreasing the distance between Ti interlayers helps to eliminate delamination between deposited layers. Through high speed camera measurements, the reaction propagation speed of an RMF sample with preheating is 42% slower than the same RMF that was not preheated, indicating a slower heat release rate. The preliminary experiments on brazing Ti-6Al-4V coated with BAlSi-4 brazing material revealed dendritic structure branching out from the RMF surface into the brazing material. The dendrite structures most likely form because of rapid melting and solidification of the brazing material. However, this rapid melting and solidification cycle does not appear to occur uniformly across the BAlSi-4RMF interface which is linked to its low bonding strength. When the Ti-6Al-4V substrate is heated to 150 °C prior to ignition, the strength increases to 0.47 MPa when the total RMF thickness is 84 µm and 15 MPa of pressure is applied. en_US
dc.description.sponsorship NASA/JPL en_US
dc.language.iso en_US en_US
dc.publisher Pasadena, CA: Jet Propulsion Laboratory, National Aeronautics and Space Administration, 2018 en_US
dc.title Preparation of Thick NI/AL Reactive Multilayer Films and Prospective Use for Self-Powered Brazing of TI-6AL-4V en_US
dc.type Preprint en_US


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