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Patent Searching and Data


Title:
The jet engine and gas turbine engine which compress strongly by compression rotation feather's carrying out reverse rotation, respectively, and combustion discharge rotation feather carrying out reverse rotation, respectively, and strengthen combustion,
Document Type and Number:
Japanese Patent JP6166201
Kind Code:
B2
Inventors:
Shinji Takeda
Application Number:
JP2014050915A
Publication Date:
July 19, 2017
Filing Date:
March 13, 2014
Export Citation:
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Assignee:
Shinji Takeda
International Classes:
F02C3/067; F02K3/072
Domestic Patent References:
JP7189603A
JP2011012675A
JP2008115859A
JP2012031861A
JP64012005A
JP2000104503A
JP11257012A
JP11114662A
Foreign References:
US20140027102
US4159624
US20130000322