Project Scope | Salvage repair of the discharge nozzle combustion liner assembly |
Capabilities Applied/Processes | Primary: Welding Blending Brazing Secondary: Abrasive Blasting |
Overall Part Dimensions | Length: 5.125" Width: 6.500" |
Tightest Tolerances | ± 0.0035" |
Material Used | Frame: C242 Nickel Alloy, Body: C263 Nickel Alloy
|
Material Finish | As Formed, No Coating |
In process testing/inspection performed | Fluorescent Penetrant Inspection |
Industry for Use | Aerospace |
Volume | 500 per Year |
Delivery/Turnaround Time | 2 – 3 Weeks |
Delivery Location | Customer Dock |
Standards Met | Customer Specifications, Rolls-Royce Standards |
Product Name | Discharge Nozzle Combustion Liner Assembly |