IP Library Granted Patent US 7,364,401
Granted Patent B2
US 7,364,401 · App. 11/350,108 · Granted Apr 29, 2008

Method for manufacturing variable-throat exhaust turbocharger and constituent members of variable throat-area mechanism

Assignee: Mitsubishi Heavy Industries, Ltd.
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Quick Facts
Patent No.
US 7,364,401
App. No.
11/350,108
Granted
Apr 29, 2008
Kind
B2
Abstract

The present invention provides a variable-throat exhaust turbocharger equipped with a variable-throat mechanism of which connection of constituent members can be achieved with a small number of man-hour and at low cost and which is stable in quality with firm connection of constituent members maintained under severe operating conditions. Among constituent members of the variable throat-area mechanism of the variable-throat exhaust turbocharger for varying the blade angle of a plurality of nozzle vanes supported rotatably by a members in a turbine casing, shaft members to be inserted and fixed in through-holes in a member with through-holes are produced by a method in which wear-resistant material is welded to form cladding of a certain thickness on the upper surface of a steel plate, said material being harder than the steel plate, and then crude shafts for forming drive pins are cut out from the clad plate.

Claims (8)

1. A method for manufacturing constituent members of a variable throat-area mechanism of a variable-throat exhaust turbocharger for varying the blade angle of a plurality of nozzle vanes supported rotatably by a member in a turbine casing, wherein, for producing shaft members to be inserted and fixed in through-holes in a member with through-holes among constituent members of said variable throat-area mechanism, wear-resistant material is welded on the upper surface of a steel plate to form cladding of a certain thickness thereon, said material being harder than the steel plate, and then crude shaft members are cut out from the clad plate.

2. A variable-throat exhaust turbocharger equipped with a variable throat-area mechanism for varying the blade angle of a plurality of nozzle vanes supported rotatably by a member in a turbine casing, wherein firm connection of drive pins pressed into through-holes in a drive ring among constituent members of said variable throat-area mechanism is performed by caulking, whereby said drive pin is formed to be composed of two stratums of a wear-resistant shaft portion stratum of hard material and a connecting shaft portion stratum of material less in hardness than said wear-resistant material by forming said wear-resistant shaft portion by cladding welding on an end of said connecting shaft portion in the axial direction thereof, said connecting shaft portion is pressed into the through-hole and caulked at the end thereof for firm connection, and said wear-resistant shaft portion functions as a sliding part to be engaged with a mating member which is connected slidably to the drive pin.

3. A variable-throat exhaust turbocharger according to claim 2 , wherein said wear-resistant shaft portion is made of Co—Mo alloy and said connecting shaft portion is made of steel including stainless steel and carbon steel.

4. A method for manufacturing constituent members of a variable throat-area mechanism of a variable-throat exhaust turbocharger for varying the blade angle of a plurality of nozzle vanes supported rotatably by a members in a turbine casing, wherein, for producing a shaft member to be inserted and fixed in a through-hole in a member with through-holes among constituent members of said variable throat-area mechanism, an end side of a connecting shaft is pressed into the hollow of a hollow cylinder formed of sintered material to obtain a shaft member composed of two stratums of a wear-resistant stratum and a connecting shaft stratum, the connecting shaft being less in hardness than said cylinder of sintered material, then the connecting shaft part of said shaft member is pressed into the through-hole and caulked at the end thereof for firm connection.

5. A variable-throat exhaust turbocharger equipped with a variable throat-area mechanism for varying the blade angle of a plurality of nozzle vanes supported rotatably by a member in a turbine casing, wherein firm connection of drive pins pressed into through-holes in a drive ring among constituent members of said variable throat-area mechanism is performed by caulking, whereby said drive pin is formed to be composed of two stratums of a wear-resistant stratum of hard material and a connecting shaft stratum of material less in hardness than said wear-resistant material by pressing-in part of the connecting shaft into the hollow of a hollow cylinder formed of sintered material, said connecting shaft member is pressed into the through-hole of the drive ring and caulked at the end thereof for firm connection, and said wear-resistant stratum functions as a sliding part to be engaged with a mating member which is connected slidably to the drive pin.

6. A variable-throat exhaust turbocharger according to claim 5 , wherein said wear-resistant portion is made of sintered material and said connecting shaft member is made of any one of steel including stainless steel and carbon steel or sintered material.

7. A method for manufacturing constituent members of a variable throat-area mechanism of a variable-throat exhaust turbocharger for varying the blade angle of a plurality of nozzle vanes supported rotatably by a member in a turbine casing, wherein, for producing a shaft member to be inserted and fixed in a through-hole in a member with through-holes among constituent members of said variable throat-area mechanism, a wear-resistant shaft made of hard material and a connecting shaft are joined together at an end of each shaft by any one of friction welding or diffusion pressure welding to obtain a shaft member composed of two stratums of a wear-resistant shaft stratum and a connecting shaft stratum, then the connecting shaft part of said shaft member is pressed into the through-hole and caulked at the end thereof for firm connection.

8. A variable-throat exhaust turbocharger equipped with a variable throat-area mechanism for varying the blade angle of a plurality of nozzle vanes supported rotatably by a member in a turbine casing, wherein firm connection of drive pins pressed into through-holes in a drive ring among constituent members of said variable throat-area mechanism is performed by caulking, whereby said drive pin is formed to be composed of two stratums of a wear-resistant shaft stratum of hard material and a connecting shaft stratum of material less in hardness than said wear-resistant material by pressure-welding a wear-resistant shaft made of hard material to a connecting shaft at an end of each shaft, the connecting shaft part is pressed into the through-hole of the drive ring and caulked at the end thereof for firm connection, and said wear-resistant shaft part functions as a sliding part to be engaged with a mating member which is connected slidably to the drive pin.

Assignments (2)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Sep 13, 2018
From: MITSUBISHI HEAVY INDUSTRIES, LTD.
To: MITSUBISHI HEAVY INDUSTRIES ENGINE & TURBOCHARGER, LTD.
Reel/Frame 047063/0420 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Apr 28, 2006
From: NAKAGAWA, HIROSHI; JINNAI, YASUAKI; INAMURA, ISAMU
To: MITSUBISHI HEAVY INDUSTRIES, LTD.
Reel/Frame 017835/0407 →
Priority Claims (1)
JP 2005-035309 · Feb 10, 2005 · national
Continuity (1)
Related Publication 20060179838A1 · Aug 17, 2006