Structure and method for joining nozzle vane and lever, and variable geometry turbocharger
An object is to provide a structure and a method of joining a nozzle vane and a lever, and a variable geometry turbocharger, capable of reducing breakage of a welded part between a shaft portion of the nozzle vane and the lever during usage of the same by reducing generation of a hot crack in weld metal at the welded part. A joint structure includes: a nozzle vane 2 disposed in an exhaust passage for guiding exhaust gas to a turbine wheel 34 of a variable geometry turbocharger 500 , and including a shaft portion 2 a ; and a lever 1 including a fitting surface 42 a fitted with a peripheral surface 72 on one end side of the shaft portion, for transmitting torque to the shaft portion to adjust a vane angle of the nozzle vane. Weld metal 50 at a welded part 40 between the lever and the nozzle vane is formed so that a center position 64 of the weld metal is disposed inside a position 17 of the fitting surface with respect to a radial direction of the shaft portion.
1. A joint structure of a nozzle vane and a lever, comprising:
a nozzle vane to be disposed in an exhaust passage for guiding exhaust gas to a turbine wheel of a variable geometry turbocharger, the nozzle vane including a shaft portion; and
a lever including a fitting surface to be fitted with a peripheral surface on one end side of the shaft portion, for transmitting torque to the shaft portion to adjust a vane angle of the nozzle vane,
wherein the lever and the one end side of the shaft portion are joined to each other by welding, and
wherein weld metal at a welded part between the lever and the one end side of the shaft portion is formed so that a center position of the weld metal is disposed inside a position of the fitting surface with respect to a radial direction of the shaft portion, and
wherein the lever includes
a first contact surface formed to extend inward in the radial direction of the shaft portion from a first end of the fitting surface with respect to the axial direction of the shaft portion, and to contact the shaft portion from the axial direction of the shaft portion, and
a second contact surface formed to extend outward in the radial direction of the shaft portion from a second end of the fitting surface with respect to the axial direction of the shaft portion, and to contact the shaft portion from the axial direction of the shaft portion.
2. The joint structure of a nozzle vane and a lever, according to claim 1 ,
wherein an outer position of the weld metal is formed inside the fitting surface with respect to the radial direction of the shaft portion.
3. The joint structure of a nozzle vane and a lever, according to claim 1 ,
wherein the variable geometry turbocharger is for a gasoline engine, and
wherein the nozzle vane is composed of nickel-based alloy, and the lever is composed of stainless steel.
4. A variable geometry turbocharger, comprising:
the joint structure of a nozzle vane and a lever according to claim 1 ;
the turbine wheel; and
a compressor driven by the turbine wheel.
5. A joint structure of a nozzle vane and a lever, comprising:
a nozzle vane to be disposed in an exhaust passage for guiding exhaust gas to a turbine wheel of a variable geometry turbocharger, the nozzle vane including a shaft portion; and
a lever including a fitting surface to be fitted with a peripheral surface on one end side of the shaft portion, for transmitting torque to the shaft portion to adjust a vane angle of the nozzle vane,
wherein the nozzle vane is composed of nickel-based alloy,
wherein the lever is composed of stainless steel, and
wherein the lever and the one end side of the shaft portion are welded to each other, and a radiation-center position radiated by heat for welding is disposed outside a position of the fitting surface with respect to a radial direction of the shaft portion, and
wherein an expression of D/S≥0.25 is satisfied, where D is a distance between the radiation-center position and the position of the fitting surface with respect to the radial direction of the shaft portion and S is a width of weld metal with respect to the radial direction of the shaft portion.
6. A variable geometry turbocharger, comprising:
the joint structure of a nozzle vane and a lever according to claim 5 ;
the turbine wheel; and
a compressor driven by the turbine wheel.
7. A method of joining a nozzle vane and a lever by welding, comprising:
providing
a nozzle vane to be disposed in an exhaust passage for guiding exhaust gas to a turbine wheel of a variable geometry turbocharger, the nozzle vane including a shaft portion and being composed of nickel-based alloy, and
a lever including a fitting surface to be fitted with a peripheral surface on one end side of the shaft portion, for transmitting torque to the shaft portion to adjust a vane angle of the nozzle vane, the lever being composed of stainless steel; and
welding the lever and the one end side of the shaft portion by radiating heat to the lever and the one end side of the shaft portion so that a radiation-center position is disposed outside a position of the fitting surface with respect to a radial direction of the shaft portion, and
wherein heat is radiated so that an expression of D/S≥0.25 is satisfied, where D is a distance between the radiation-center position and the position of the fitting surface with respect to the radial direction of the shaft portion and S is a width of weld metal with respect to the radial direction of the shaft portion.