Description:

Axial compressor design type, compressor engine section location, steel, ams 6415, rockwell c35-40 hardness, 3.210-3.221 in. Thk, 19.825-19.835 in. Od, 6.995-7.005 in. Id, 27 blade slots equally spacedaround od, sixteen 0.437-0.440 in. Holes equally spaced on 8.000 in.Centerline radius, thirty-two 0.101-0.113 in. Holes equally spaced on7.260 in. Centerline radius, thirty-two scallops equally spaced on 7.260in. Centerline radius .

Special Features:

Steel, ams 6415, rockwell c35-40 hardness, 3.210-3.221 in. Thk, 19.825-19.835 in. Od, 6.995-7.005 in. Id, 27 blade slots equally spacedaround od, sixteen 0.437-0.440 in. Holes equally spaced on 8.000 in.Centerline radius, thirty-two 0.101-0.113 in. Holes equally spaced on7.260 in. Centerline radius, thirty-two scallops equally spaced on 7.260in. Centerline radius

Properties:

An item having provisions on the outer periphery for attaching a designated number of blade, turbine rotor, aircraft gas turbine engine. It also has provisions for attachment to a hub, turbine, aircraft gas turbine engine.