Abstract: A method for joining a cast metal material blade ring and a metal material hub structure into a turbine rotor. One of the blade ring and the hub structure is mounted in a holder and the other is mounted in a rotation holder for being rotated. At least one of these mountings is heated, and then they are pressed together with a selected force while rotating to weld the ring interior wall and the disk side to form the assembled structure.

Abstract: A method for joining a cast metal material blade ring and a metal material hub structure into a turbine rotor. One of the blade ring and the hub structure is mounted in a holder and the other is mounted in a rotation holder for being rotated. At least one of these mountings is heated, and then they are pressed together with a selected force while rotating to weld the ring interior wall and the disk side to form the assembled structure.

Abstract: A containment case for a turbine engine having a plurality of blades rotating therein has a first plurality of metallic layers each of the first plurality of layers being resistant to penetration of fragments therethrough and a second plurality of metallic layers, each of the second plurality of layers absorbing kinetic energy of fragments striking said second plurality of layers.

Abstract: A method for joining a cast metal material blade ring and a metal material hub structure into a turbine rotor. One of the blade ring and the hub structure is mounted in a holder and the other is mounted in a rotation holder for being rotated. At least one of these mountings is heated, and then they are pressed together with a selected force while rotating to weld the ring interior wall and the disk side to form the assembled structure.

Abstract: A method for joining a cast metal material blade ring having therein an initial interior ring passageway formed by a ring interior wall thereabout and a metal material hub structure, having therein a disk part thereof with a disk side configured such that at least a portion of a disk side is positionable against a portion of the ring interior wall so as to be assembleable into an assembled structure for a turbine rotor through mounting one of the blade ring and the hub structure in a holder and also mounting the remaining one of the blade ring and the hub structure in a rotation holder for being rotated by a rotatable portion of that rotation holder.

Abstract: High inertia and large bearing loads encountered in monorotors for gas turbine engines are reduced in a monorotor having a compressor wheel section (10) made of a relatively low density material while the turbine wheel section (12) maintains resistance to heat by being made of a relatively higher density, heat resistant material. The two are joined into a monorotor through the use of two bodies (24,38) which are inertia welded to the respective wheels (10,12) and then welded together by any one of a variety of welding processes.

Abstract: The disclosure relates to a turbine disk and a method of making the turbine disk comprising the steps of rotating a mold, adding a first powdered metal to the rotating mold at a first rate, reducing the rate of addition of the first metal to a second rate, and adding a second powdered metal to the mold at a third rate substantially equal to the difference between the first and second rates.

Abstract: The disclosure relates to a turbine disk and a method of making the turbine disk comprising the steps of rotating a mold, adding a first powdered metal to the rotating mold at a first rate, reducing the rate of addition of the first metal to a second rate, and adding a second powdered metal to the mold at a third rate substantially equal to the difference between the first and second rates.

Abstract: The disclosure relates to a process for the fabrication of low cost dual property turbine rotors having blades that are mechanically retained and a blade ring that is permanently bonded to a central hub.