SAE ARP5935
Current
The latest, up-to-date edition.
Use of HVOF Thermal Spray Coatings for Hard Chrome Replacement in Landing Gear Applications
Hardcopy , PDF
English
25-10-2013
1. SCOPE
2. REFERENCES
3. RECOMMENDATIONS
Electrolytically deposited chrome plate is the current standard surface treatment for landing gear component interface surfaces that require good wear resistance and corrosion protection.
DocumentType |
Standard
|
Pages |
7
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PublisherName |
SAE International
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Status |
Current
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Supersedes |
Electrolytically deposited chrome plate is the current standard surface treatment for landing gear component interface surfaces that require good wear resistance and corrosion protection. Chrome plated components are typically plagued by a slight debit in fatigue performance, detrimental mud cracking surface pattern, susceptibility to scoring, wear, and seal leakage. In addition, recent changes in environmental compliance standards place further restrictions on the use of electrolytically deposited chromium. Some commercial applications have already eliminated the use of chrome plate on current and future products. As a result, a substitute for electrolytically deposited chrome plate has been sought for several years.High Velocity Oxygenated Fuel (HVOF) thermal spray coatings have been developed to the point where they are being implemented as an alternative to hard chrome plate on high strength low alloy steels for external surfaces on landing gear applications. Some of the characteristics of HVOF coatings, such as fatigue and wear resistance are superior to hard chrome plate. Yet, performance characteristics, such as adhesion under very high strains, are clearly different. This document is intended to outline and describe the design and usage guidelines for HVOF tungsten carbide coatings to assure adequate quality and performance of the landing gear equipment. This document is not intended to act as a detailed process specification for applying HVOF coatings. Also, the recommendations in this document do not necessarily apply to certain proprietary spraying systems (i.e., D-Gun™).The information in this document pertains to HVOF tungsten carbide based coatings applied to high strength steel alloys only, and is not necessarily applicable to other substrates.
SAE AS4941B | Aerospace - General Requirements for Commercial Aircraft Hydraulic Components |
SAE AIR1594C | Plain Bearing Selection for Landing Gear Applications |
SAE ARP1311C | Landing Gear Structures and Mechanisms |
SAE AS4716C | Gland Design, O-ring and Other Seals |
SAE ARP1311D | Landing Gear Structures and Mechanisms |
SAE AMS 2447 : 2012 | COATING, THERMAL SPRAY, HIGH VELOCITY OXYGEN/FUEL PROCESS |
SAE AMSQQC320 | Chromium Plating (Electrodeposited) |
SAE AMS7881A | Tungsten Carbide-Cobalt Powder Agglomerated and Sintered |
SAE AMS 2449 : 2004 | GRINDING OF HVOF SPRAYED TUNGSTEN CARBIDE COATINGS APPLIED TO HIGH STRENGTH STEELS |
SAE ARP 4462 : 1991 | BARKHAUSEN NOISE INSPECTION FOR DETECTING GRINDING BURNS IN HIGH STRENGTH STEEL PARTS |
SAE AMS7882B | Tungsten Carbide-Cobalt Chrome Powder Agglomerated and Sintered |
SAE AMS 2649 : 2013 | ETCH INSPECTION OF HIGH STRENGTH STEEL PARTS |
SAE AMS2448B | Application of Tungsten Carbide Coatings on Ultra High Strength Steels High Velocity Oxygen / Fuel Process |
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