초록 ▼

A method of making combustion turbine transition duct bodies without longitudinal welds by hydroforming two duct bodies back to back with bellows thrusters secured to the duct body open ends. This enables the manufacturing of duct bodies with detailed features and high pressure without using compres

A method of making combustion turbine transition duct bodies without longitudinal welds by hydroforming two duct bodies back to back with bellows thrusters secured to the duct body open ends. This enables the manufacturing of duct bodies with detailed features and high pressure without using compression cylinders. Multi-layer transition duct bodies can also be assembled with layers of different materials, for example, having a heat-resistant layer inside and high strength layer outside. They can be assembled using cold shrinking and heat expanding. In addition, anti-fretting and anti-vibration coatings can be applied between the layers for improved performance.

대표청구항 ▼

The invention claimed is: 1. A method of making gas turbine transition duct bodies without longitudinal welds comprising the steps of providing at least one hemispherical bellows thruster having a bellows structure, structural welding a bellows thruster to each open end of a duct body such that the

The invention claimed is: 1. A method of making gas turbine transition duct bodies without longitudinal welds comprising the steps of providing at least one hemispherical bellows thruster having a bellows structure, structural welding a bellows thruster to each open end of a duct body such that the duct body is capable of containing internal pressure, removably securing a pressurizing means to at least one of said bellows thrusters capable of pressurizing the inside of a duct body, and hydroforming the transition duct body in a hydroforming press to a pressure less than the capacity of the hydroforming press. 2. The method of claim 1, wherein the bellows structure is uniform around the axis of the hemispherical bellows thruster. 3. A method of making gas turbine transition duct bodies without longitudinal welds comprising the steps of providing at least one hemispherical bellows thruster having a bellows structure, wherein the bellows structure is uniform around the axis of the hemispherical bellows thruster and comprises one ripple around the axis of the bellows thruster structural welding a bellows thruster to each open end of a duct body such that the duct body is capable of containing internal pressure, removably securing a pressurizing means to at least one of said bellows thrusters capable of pressurizing the inside of a duct body, and hydroforming the transition duct body in a hydroforming press to a pressure less than the capacity of the hydroforming press. 4. The method of claim 3, wherein the bellows structure is non-uniform around the axis of the hemispherical bellows thruster. 5. The method of claim 3, wherein the hemispherical bellows thruster bellows structure is adapted to supply more lateral force to the duct body during hydroforming than hemispherical bellows thrusters without bellows. 6. The method of claim 3, further comprising the step of providing a pair of hydroforming dies that when assembled form at least two hemispherical recesses sized to communicate with hemispherical bellows thrusters secured to the duct body during hydroforming. 7. The method of claim 3, adapted to form two transition duct bodies in a back-to-back arrangement, said hydroforming press comprising dies shaped to form two transition duct bodies in a back-to-back arrangement. 8. The method of claim 3, wherein the duct body is a multi-layer transition duct body. 9. The method of claim 8, wherein an anti-fretting material is disposed between an inner layer and an outer layer of the multi-layer transition duct body. 10. A method of making gas turbine transition duct bodies without longitudinal welds comprising the steps of providing at least one hemispherical bellows thruster having a bellows structure, wherein the bellows structure is non-uniform around the axis of the hemispherical bellows thruster and comprises at least two ripples on one side of the bellows thruster, and one ripple on the other aide of the bellows thruster, structural welding a bellows thruster to each open end of a duct body such that the duct body is capable of containing internal pressure, removably securing a pressurizing means to at least one of said bellows thrusters capable of pressurizing the inside of a duct body, and hydroforming the transition duct body in a hydroforming press to a pressure less than the capacity of the hydroforming press. 11. A method of making gas turbine transition duct bodies without longitudinal welds comprising the steps of providing at least one hemispherical bellows thruster having a bellows structure, wherein the bellows structure is non-uniform around the axis of the hemispherical bellows thruster and comprises one ripple around the axis of the bellows thruster, and wherein the hemispherical bellows thruster bellows structure is adapted to supply more lateral force to one side of the duct body during hydroforming than the other, structural welding a bellows thruster to each open end of a duct body such that the duct body is capable of containing internal pressure, removably securing a pressurizing means to at least one of said bellows thrusters capable of pressurizing the inside of a duct body, and hydroforming the transition duct body in a hydroforming press to a pressure less than the capacity of the hydroforming press.