Structure of scroll of variable-throat exhaust turbocharger and method for manufacturing the turbocharger
AssigneeMitsubishi Heavy Industries, Ltd.
InventorsYasuaki Jinnai, Hiroshi Nakagawa, Takashi Mikogami
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AssigneeMitsubishi Heavy Industries, Ltd.
InventorsYasuaki Jinnai, Hiroshi Nakagawa, Takashi Mikogami
Estimating the term…
According to the present invention, the A/R, the ratio of cross sectional area A of scroll passage to scroll radius R can be increased without increasing the size of the turbine casing and with very simple construction and exhaust turbine capacity can be increased, so a variable-throat exhaust turbocharger with which engine output can be increased is provided. The turbocharger is equipped with a nozzle throat area varying mechanism of which the nozzle assembly unit is composed such that a plurality of nozzle vanes are supported rotatably by an annular nozzle mount and an annular nozzle plate is connected to the nozzle mount by means of a plurality of nozzle supports to sandwich the nozzle vanes, the nozzle plate is located in the scroll chamber by attaching the nozzle assembly unit to the turbine casing to allow the nozzle plate to form part of the inside sidewall face of the scroll chamber and a wall face of the annular flow passage.
A scroll structure of a variable-throat exhaust turbocharger equipped with a nozzle throat area varying mechanism for varying the blade angle of a plurality of nozzle vanes arranged in an annular flow passage formed in the inner side of a scroll chamber of a turbine casing whereby engine exhaust gas is introduced to the scroll chamber to pass through the annular flow passage to flow into a radial flow type turbine,
A method of manufacturing a variable-throat exhaust turbocharger equipped with a nozzle throat area varying mechanism for varying the blade angle of a plurality of nozzle vanes arranged in an annular flow passage formed in the inner side of a scroll chamber of a turbine casing whereby engine exhaust gas is introduced to the scroll chamber to pass through the annular flow passage to flow into a radial flow type turbine, comprising:
Dependencies are inferred from the claim text.