Abstract
State of Residual Stresses After the Process of Milling Selected Aluminium Alloys
Highlights
IntroductionSTATE OF KNOWLEDGEThe attempts to reduce aircraft mass and to maintain concurrently its operating characteristics (increased performance, range, load-carrying capacity, durability, and reliability; decreased fuel consumption) result largely from economic aspects and make the designers and manufacturers use new materials as well as new design solutions, which means the adoption of new production and assembling technologies
STATE OF KNOWLEDGEThe attempts to reduce aircraft mass and to maintain concurrently its operating characteristics result largely from economic aspects and make the designers and manufacturers use new materials as well as new design solutions, which means the adoption of new production and assembling technologies
The diversity of rolled plate material structures is a likely source of residual stresses
Summary
STATE OF KNOWLEDGEThe attempts to reduce aircraft mass and to maintain concurrently its operating characteristics (increased performance, range, load-carrying capacity, durability, and reliability; decreased fuel consumption) result largely from economic aspects and make the designers and manufacturers use new materials as well as new design solutions, which means the adoption of new production and assembling technologies. 1), the industry uses closed-plate structures where the connecting ribs and the outside coating are homogenous elements. Apart from plate or frame type structures Examples of such structures are the elements produced by means of Goodrich proprietary GRID-LOCK® technology Examples of such structures are the elements produced by means of Goodrich proprietary GRID-LOCK® technology (fig. 2)
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