Title:
航空機用レシプロエンジンの過給システム、航空機用レシプロエンジン及び航空機
Document Type and Number:
Japanese Patent JP6655640
Kind Code:
B2
Abstract:
There is provided a supercharging system for an aircraft reciprocating engine, comprising: a plurality of compressors for supplying compressed air to the aircraft reciprocating engine; at least one turbine for obtaining rotational power for at least one of the plurality of compressors, and a plurality of motors for respectively providing rotational power to the plurality of compressors. An object of the present invention is to reduce turbo lag in a reciprocating engine for an aircraft in which multiple-stage supercharging is performed by the turbocharger.
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Inventors:
Kazuaki Otani
Noriyuki Nakazato
Iwao Murata
Noriyuki Nakazato
Iwao Murata
Application Number:
JP2018036410A
Publication Date:
February 26, 2020
Filing Date:
March 01, 2018
Export Citation:
Assignee:
Subaru corporation
International Classes:
F02B37/04; B64D27/04; B64D27/24; F02D23/00
Domestic Patent References:
| JP2014159810A | ||||
| JP2033413A | ||||
| JP11315725A | ||||
| JP2012062823A | ||||
| JP2007162654A | ||||
| JP2007016721A | ||||
| JP2012503732A | ||||
| JP2015511199A |
Attorney, Agent or Firm:
Takehiko Yamada