Browse Topic: Surface enhancement

Items (226)
This Aerospace Standard covers components of rotary flap assemblies to be used with portable equipment for peening of metal parts.The flap assemblies consist of a flap attached to a mandrel and shall be of the following sizes.
AMS B Finishes Processes and Fluids Committee
Shot peened components present a challenge for the structural analyst when nicks, scratches and gouges are discovered. A common repair scheme calls for blending away of the defect with an appropriate grit abrasive. Though the blending operation removes the defect, it also takes away a portion the beneficial compressive layer as well as the cold-worked material. Large repair facilities may have touch-up shot peen capability but technicians in a field repair setting typically do not. If the shot peen cannot be restored, the structural analyst must have a method to quantify the effect on fatigue life of the repaired part. The purpose of this technical paper is to substantiate analytical techniques for evaluating the fatigue life of a shot peened part after a blend operation. In addition to practical methods to estimate the magnitude of the residual stresses, a numerical method is introduced using finite element modeling of shot peen impacts with non-linear finite element code and
Conklin, CraigFlores, RicBarrett, Arild
This specification covers the requirements for electrodeposited low-stressed nickel.
AMS B Finishes Processes and Fluids Committee
This SAE Recommended Practice defines requirements for equipment and supplies to be used in measuring shot peening arc height and other surface enhancement processes. Guidelines for use of these items can be found in SAE J443 and SAE J2597.
Surface Enhancement Committee
This specification covers the characteristics of glass beads used for peening, and provides for standard glass bead size numbers.
Surface Enhancement Committee
This SAE Recommended Practice Specification provides the procedures for using test strips per SAE J442 for peening processes.
Surface Enhancement Committee
ABSTRACT Accounting for effects of damage on the fatigue strength of metallic principal structural elements (PSE) is a requirement for fatigue tolerance evaluation of transport category rotorcraft. Parallel to the current structural test approach for showing regulatory compliance, an analysis method is sought. However, developing and executing an analytical compliance methodology has many challenges. One example is the stress state at the root of a flaw, and how that stress state interferes with the residual stress induced by specific processes such as shot peening. This paper presents an analysis method to determine the stress state at the root of a flaw with the presence of residual stresses. The method can quantify the effect of the residual stress on various flaw shapes and sizes, to avoid overly conservative assumptions in certification analysis.
Rajagopal, BalajiGreen, W.Reddy, ManjunathaLi, Xiaoming
ABSTRACT This paper presents the results of an experimental test program aimed at the investigation of the effect on fatigue life of blending surface damage on shot-peened parts. The test program was performed on shot-peened aluminum specimens where a surface damage was introduced on the specimen by machining a notch after the shot-peening operation. This notched area was then blended to a smooth surface before performing a four point bending fatigue test. The results showed little detrimental effect of the blending operation and, in some cases, improvement on the fatigue life of the specimen compared to a baseline shot-peened and undamaged specimen. These results were investigated with fractography, residual stress measurement using X-ray diffraction and a Discrete Element Model (DEM) - Finite Element Model (FEM) to simulate the blending and assess the redistribution of the residual stresses in the specimens.
Lapalme, MaximeOuellet, MarcBiron, Guillaume
This SAE Recommended Practice covers a high-strength corrosion-resisting steel wire, uniform in mechanical properties, intended for the manufacture of springs and wire forms. It also covers processing requirements of springs and forms fabricated from this wire.
Materials, Processes and Parts Council
This SAE Recommended Practice covers a high-quality corrosion-resisting steel wire, cold drawn, formed, and heat treated to produce uniform mechanical properties. It is magnetic in all conditions. It is intended for the manufacture of springs and wire forms that are to be heat treated after forming to enhance the spring properties. This document also covers processing requirements of the springs and forms fabricated from this wire.
Materials, Processes and Parts Council
STRESSONIC® Ultrasonic Shot Peening provides an economical shot peening solution to FAA Part 145 Repair Stations including Maintenance, Repair, and Overhaul facilities. This technology brings shot peening repairs to the shop floor, which eliminates the need to ship components to approved Conventional Shot Peening vendors, reducing shipping cost and turnaround time for a repair, as well as reducing the likelihood of damaged components due to shipping. Through a Small Business Innovative Research project with the U.S. Army, Avion and SONATS-Empowering Technologies qualified the use of the Ruggedized StressVoyager® on repairs for flight Critical Safety Items. Testing revealed that Ultrasonic Shot Peening induces a compressive residual stress comparable to Conventional Shot Peening methods used by Original Equipment Manufacturers, eliminating the concern of creating any stress concentration gradient when using this technology for repairs.
McClurg, KellyBuckner, RandyBrier, OlivierChateau, Frederic
This SAE Recommended Practice describes chemical composition and physical characteristic requirements for high-carbon cast-steel shot to be used for shot peening or blast cleaning operations.
Surface Enhancement Committee
This SAE recommended practice provides some procedure for determining shot peening coverage and relating coverage to part exposure to the media stream. Effectiveness of shot peening is directly dependent on coverage. Either incomplete or excessive coverage can be detrimental to fatigue strength and life.
Surface Enhancement Committee
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