Method for manufacturing variable-throat exhaust turbocharger and constituent members of nozzle throat area varying mechanism
An exhaust turbocharger equipped with a nozzle throat area varying mechanism can be provided in which brazing welding is achieved with a small number of man-hour and at low cost, and which is stable in quality without danger of fracture of brazing-welded parts of constituent members. The variable-throat exhaust turbocharger equipped with a nozzle throat area varying mechanism for varying the blade angle of a plurality of nozzle vanes supported rotatably by members including turbine casing, is characterized in that members having at least one through-hole with at least one shaft member to be inserted into the through-hole(s) to be fixed therein among constituent members of the nozzle throat area varying mechanism are connected by means of brazing welding.
1. A method for manufacturing a variable-throat exhaust turbocharger having a nozzle throat area varying mechanism and a turbine casing within which a plurality of nozzle vanes are disposed and also having a plurality of members rotatably supporting the plurality of nozzle vanes, the plurality of members including a member having at least one through-hole and also including at least one shaft member, the method comprising:
forming a conically tapered portion at an entrance of the at least one through-hole;
putting a piece of solder on the tapered portion;
inserting the at least one shaft member into the through-hole with an interference provided between the at least one shaft member and the member having the at least one through-hole;
heating the integrated member formed of the at least one shaft member and the member having at least one through-hole in a vacuum furnace to a temperature of 1000-1100 degrees Celsius such that the piece of solder infiltrates into a small clearance between the member having at least one through-hole and the shaft member; and
cooling the integrated member slowly to thereby firmly fix the at least one shaft member to the member having at least one through-hole.
2. The method of claim 1 , wherein
the member having at least one through-hole is a drive ring with a plurality of through-holes and the at least one shaft member is a plurality of drive pins of the nozzle throat area varying mechanism.
3. A variable-throat exhaust turbocharger including:
a turbine casing; and
a nozzle throat area varying mechanism for varying a blade angle of a plurality of nozzle vanes that are rotatably supported in said turbine casing;
wherein said nozzle throat area varying mechanism comprises constituent members, including a drive ring for controlling the varying of the blade angle of said plurality of nozzle vanes, drive pins connected to said drive ring for engaging lever plates connected to nozzle shafts of said nozzle vanes, a lever engaging with said drive ring and a control sleeve fixed to said lever;
wherein said drive ring and said lever comprise through-holes, and said drive pins and said control sleeve form shaft members inserted and fixed into said through-holes of said drive ring and said lever, respectively, so as to form respective connecting parts; and
wherein at least one of said connecting parts is connected together by brazing welding.
4. A variable-throat exhaust turbocharger including:
a turbine casing; and
a nozzle throat area varying mechanism for varying a blade angle of a plurality of nozzle vanes that are rotatably supported in said turbine casing;
wherein said nozzle throat area varying mechanism comprises constituent members, including a member having at least one through-hole and at least one shaft member inserted and fixed into said at least one through-hole, respectively, which have a clearance created between the inside periphery of said through-hole and the outside periphery of said shaft member in a state in which said shaft member is inserted into said through-hole such that the solder infiltrates into said clearance and said at least one through-hole and said at least one shaft member are connected together by brazing welding to form a connecting part between said at least one through-hole and said at least one shaft member; and
wherein said connecting part between said at least one through-hole and said at least one shaft member is one or more of (a) a connecting part between a drive ring and drive pins and (b) a connecting part between a control sleeve and a lever.
5. A variable-throat exhaust turbocharger according to claim 4 , further comprising:
a clearance gap for allowing solder to infiltrate between said at least one through-hole and said shaft member, said clearance gap extending axially of and within said through-hole between said drive ring and said drive pin and having a depth of 0.05 mm to 0.5 mm.
6. A variable-throat exhaust turbocharger according to claim 5 , wherein
said clearance gap is a semicircular groove having a depth of 0.2 mm to 0.5 mm.
7. The variable-throat exhaust turbocharger of claim 4 , wherein:
said member having at least one through-hole comprises said drive ring having a plurality of through-holes; and
said at least one shaft member comprises said drive pins.
8. The variable-throat exhaust turbocharger of claim 4 , wherein:
said member having at least one through-hole comprises said control sleeve; and
said at least one shaft member comprises said lever.