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Title:
MULTISTAGE TURBO SUPERCHARGER SYSTEM
Document Type and Number:
Japanese Patent JP2018184902
Kind Code:
A
Abstract:
PROBLEM TO BE SOLVED: To provide a multistage turbo supercharger system capable of avoiding generation of a high pressure stage side surge in the case of sudden speed reduction and/or sudden load decrease (cutoff) of an engine.SOLUTION: The present invention relates to a multistage turbo supercharger system in which a small-sized side high pressure stage turbo supercharger 50 and a large-sized side low pressure stage turbo supercharger 60 are connected in series from the side of an engine body 10. The multistage turbo supercharger system comprises: a low pressure stage exhaust bypass path 33 bypassing a low pressure stage turbine 61 of the low pressure stage turbo supercharger 60; a low pressure stage waste gate valve WG2 opening/closing the low pressure stage exhaust bypass path 33; and high pressure stage side surge avoiding means 90 by which, in a case where an actuation condition that a suction pressure P1 at an upstream side of a high pressure stage compressor 52 of the high pressure stage turbo supercharger 50 is higher than a suction pressure P2 at a downstream side of the high pressure stage compressor 52 is satisfied, the low pressure stage waste gate valve WG2 is opened.SELECTED DRAWING: Figure 2

Inventors:
YOSHIOKA TSUGIO
Application Number:
JP2017087451A
Publication Date:
November 22, 2018
Filing Date:
April 26, 2017
Export Citation:
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Assignee:
YANMAR CO LTD
International Classes:
F02B37/18; F02B37/00
Domestic Patent References:
JP2015108329A2015-06-11
JPH01160126U1989-11-07
JPS62162346U1987-10-15
JP2016125366A2016-07-11
JPH0197039U1989-06-28
JPS60164631U1985-11-01
JP2009270470A2009-11-19
JPS4964708A1974-06-22
Foreign References:
EP1927739A12008-06-04
WO2015083611A12015-06-11
US20160265468A12016-09-15
US20130211693A12013-08-15
Attorney, Agent or Firm:
Masahiro Miyaji