Variable-capacity exhaust turbocharger equipped with variable-nozzle mechanism
A variable-capacity exhaust turbocharger is provided which is equipped with a variable-nozzle mechanism having a lever plate and a peripheral structure capable of ensuring regular operability of a nozzle vane and of preventing an occurrence of local excessive stress by increasing rigidity of the lever plate without increasing a thickness of the lever plate. In a variable-capacity exhaust turbocharger equipped with a variable-nozzle mechanism including: a plurality of nozzle vanes; an annular drive ring; and a lever plate provided as many as the number of the nozzle vanes so that one end is connected to an engagement pin portion engaging with a groove portion formed in the drive ring and the other end is fixed to each nozzle vane, the drive ring is disposed between the lever plate and a nozzle mount in an axial direction, and the lever plate is curved in an axial direction from a surface of the lever plate connected to the fixed portion on the side of the nozzle vane so as to be connected to the groove portion of the drive ring.
1. A variable-capacity exhaust turbocharger equipped with a variable-nozzle mechanism comprising:
a plurality of nozzle vanes rotatably supported to a nozzle mount fixed to a bearing housing or a casing including a turbine casing;
an annular drive ring interlocked with an actuator; and
a lever plate provided in a circumferential direction as many as the number of the nozzle vanes so that one end is connected to an engagement pin portion engaging with a groove portion formed in the drive ring and another end is fixed to each nozzle vane,
wherein each lever plate is swung by a rotation of the drive ring, and each blade angle of the plurality of nozzle vanes is changed by the swing of the lever plate,
wherein the drive ring is disposed between the lever plate and the nozzle mount in an axial direction, and
wherein the lever plate is curved in an axial direction from a surface of the lever plate connected to the fixed portion on the side of the nozzle vane so as to be connected to the groove portion of the drive ring.
2. The variable-capacity exhaust turbocharger equipped with the variable-nozzle mechanism according to claim 1 , wherein the engagement pin portion of the lever plate is formed into an engagement protrusion integrally formed with the lever plate and engaging with the groove portion.
3. The variable-capacity exhaust turbocharger equipped with the variable-nozzle mechanism according to claim 2 wherein the engagement pin portion of the lever plate is formed in an oval shape in which a section of a fitting-sliding surface of the engagement pin portion is formed in a circular-arc shape and a non-sliding portion of the engagement pin portion is formed in a linear shape, and
wherein a long axis of the oval shape is disposed in a circumferential direction of the drive ring.
4. A variable-capacity exhaust turbocharger equipped with a variable-nozzle mechanism comprising:
a plurality of nozzle vanes of which both ends are supported so that one end is rotatably supported to a nozzle mount fixed to a bearing housing or a casing including a turbine casing and the other end is supported to a nozzle plate;
an annular drive ring interlocked with an actuator; and
a lever plate provided in a circumferential direction as many as the number of the nozzle vanes so that one end is connected to an engagement pin portion engaging with a groove portion formed in the drive ring and the other end is fixed to each nozzle vane,
wherein each lever plate is swung by a rotation of the drive ring, and each blade angle of the plurality of nozzle vanes is changed by the swing of the lever plate,
wherein the drive ring is disposed between the lever plate and the nozzle mount in an axial direction, and
wherein the lever plate has a configuration according to claim 2 .
5. The variable-capacity exhaust turbocharger equipped with the variable-nozzle mechanism according to claim 1 , wherein the engagement pin portion of the lever plate is formed in such a manner that an engagement pin is fitted in a direction perpendicular to a surface of the lever plate and the engagement pin engages with the groove portion.
6. The variable-capacity exhaust turbocharger equipped with the variable-nozzle mechanism according to claim 5 wherein the engagement pin portion of the lever plate is formed in an oval shape in which a section of a fitting-sliding surface of the engagement pin portion is formed in a circular-arc shape and a non-sliding portion of the engagement pin portion is formed in a linear shape, and
wherein a long axis of the oval shape is disposed in a circumferential direction of the drive ring.
7. A variable-capacity exhaust turbocharger equipped with a variable-nozzle mechanism comprising:
a plurality of nozzle vanes of which both ends are supported so that one end is rotatably supported to a nozzle mount fixed to a bearing housing or a casing including a turbine casing and the other end is supported to a nozzle plate;
an annular drive ring interlocked with an actuator; and
a lever plate provided in a circumferential direction as many as the number of the nozzle vanes so that one end is connected to an engagement pin portion engaging with a groove portion formed in the drive ring and the other end is fixed to each nozzle vane,
wherein each lever plate is swung by a rotation of the drive ring, and each blade angle of the plurality of nozzle vanes is changed by the swing of the lever plate,
wherein the drive ring is disposed between the lever plate and the nozzle mount in an axial direction, and
wherein the lever plate has a configuration according to claim 5 .
8. The variable-capacity exhaust turbocharger equipped with the variable-nozzle mechanism according to claim 1 , wherein the engagement pin portion of the lever plate is formed in an oval shape in which a section of a fitting-sliding surface of the engagement pin portion is formed in a circular-arc shape and a non-sliding portion of the engagement pin portion is formed in a linear shape, and
wherein a long axis of the oval shape is disposed in a circumferential direction of the drive ring.
9. A variable-capacity exhaust turbocharger equipped with a variable-nozzle mechanism comprising:
a plurality of nozzle vanes of which both ends are supported so that one end is rotatably supported to a nozzle mount fixed to a bearing housing or a casing including a turbine casing and the other end is supported to a nozzle plate;
an annular drive ring interlocked with an actuator; and
a lever plate provided in a circumferential direction as many as the number of the nozzle vanes so that one end is connected to an engagement pin portion engaging with a groove portion formed in the drive ring and the other end is fixed to each nozzle vane,
wherein each lever plate is swung by a rotation of the drive ring, and each blade angle of the plurality of nozzle vanes is changed by the swing of the lever plate,
wherein the drive ring is disposed between the lever plate and the nozzle mount in an axial direction, and
wherein the lever plate has a configuration according to claim 1 .
10. A variable-capacity exhaust turbocharger equipped with a variable-nozzle mechanism comprising:
a plurality of nozzle vanes rotatably supported to a nozzle mount fixed to a bearing housing or a casing including a turbine casing;
an annular drive ring interlocked with an actuator; and
a lever plate provided in a circumferential direction as many as the number of the nozzle vanes so that one end is connected to an engagement pin portion engaging with a groove portion formed in the drive ring and the other end is fixed to each nozzle vane,
wherein each lever plate is swung by a rotation of the drive ring, and each blade angle of the plurality of nozzle vanes is changed by the swing of the lever plate,
wherein the drive ring is disposed between the lever plate and the nozzle mount in an axial direction, and
wherein a curved portion curved in an axial direction from a surface of the lever plate connected to the fixed portion on the side of the nozzle vane and an engagement protrusion connected to the curved portion and engaging with the groove portion are formed by bending one sheet of plate.
11. The variable-capacity exhaust turbocharger equipped with the variable-nozzle mechanism according to claim 10 wherein the engagement pin portion of the lever plate is formed in an oval shape in which a section of a fitting-sliding surface of the engagement pin portion is formed in a circular-arc shape and a non-sliding portion of the engagement pin portion is formed in a linear shape, and
wherein a long axis of the oval shape is disposed in a circumferential direction of the drive ring.
12. A variable-capacity exhaust turbocharger equipped with a variable-nozzle mechanism comprising:
a plurality of nozzle vanes of which both ends are supported so that one end is rotatably supported to a nozzle mount fixed to a bearing housing or a casing including a turbine casing and the other end is supported to a nozzle plate;
an annular drive ring interlocked with an actuator; and
a lever plate provided in a circumferential direction as many as the number of the nozzle vanes so that one end is connected to an engagement pin portion engaging with a groove portion formed in the drive ring and the other end is fixed to each nozzle vane,
wherein each lever plate is swung by a rotation of the drive ring, and each blade angle of the plurality of nozzle vanes is changed by the swing of the lever plate,
wherein the drive ring is disposed between the lever plate and the nozzle mount in an axial direction, and
wherein the lever plate has a configuration according to claim 10 .