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Reinforcing Additives for Ice Adhesion Reduction CoatingsAdhesion of contaminants has been identified as a ubiquitous issue for aeronautic exterior surfaces. In-flight icing is particularly hazardous for all aircraft and can be experienced throughout the year under the appropriate environmental conditions. On larger vehicles, the accretion of ice could result in loss of lift, engine failure, and potentially loss of vehicle and life were it not for active deicing or anti-icing equipment. Smaller vehicles though cannot support the mass and mechanical complexity of active ice mitigating systems and thus must rely upon passive approaches or avoid icing conditions altogether. One approach that may be applicable to all aircraft is the use of coatings. Durability remains an issue and has prevented realization of coatings for leading edge contamination mitigation. In this work, epoxy coatings were generated as a passive approach for ice adhesion mitigation and methods to improve durability were evaluated. Highly cross-linked epoxy systems can be extremely rigid, which could have deleterious consequences regarding application as a leading edge coating. Incorporation of flexible species, such as poly(ethylene glycol) may improve coating toughness.8 Additionally, core-shell rubber (CSR) particles have been utilized to improve fracture toughness of epoxies.9 Both of these more established additives are investigated in this work. An emerging additive that is also evaluated here is holey graphene. This nanomaterial possesses many of the advantageous properties of graphene (excellent mechanical properties, thermal and electrical conductivity, large surface area, etc.) while also exhibiting behaviors associated with flexible, porous materials (i.e., compressibility, increased permeation, etc.). Holey graphene, HG, was synthesized by the oxidation of defect-rich sites on graphene sheets through controlled thermal expo-sure.10 It is envisioned that the porous nature of HG would allow resin penetration through the graphitic plane, resulting in better interfacial interaction and therefore better translation of the nanomaterial’s properties to the surrounding matrix.



Document ID
20200002447
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Wohl, Christopher J
(NASA Langley Research Center Hampton, VA, United States)
Balderson, Lilly L.
(NASA Langley Research Center Hampton, VA, United States)
Beck, Devon M.
(NASA Langley Research Center Hampton, VA, United States)
Sosa, Francisco A. Mendez
(NASA Langley Research Center Hampton, VA, United States)
Lin, Yi
(National Inst. of Aerospace Hampton, VA, United States)
Smith, Joseph G., Jr.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
April 14, 2020
Publication Date
February 17, 2019
Subject Category
Composite Materials
Report/Patent Number
NF1676L-31070
Meeting Information
Meeting: 2019 Annual Meeting of the Adhesion Society
Location: Hilton Head, SC
Country: United States
Start Date: February 17, 2019
End Date: February 20, 2019
Sponsors: Adhesion Society, Inc.
Funding Number(s)
WBS: 081876.02.07.50.08.03
Distribution Limits
Public
Copyright
Public Use Permitted.
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