Title:
航空機用発電装置
Document Type and Number:
Japanese Patent JP4700113
Kind Code:
B2
Abstract:
This invention provides an aircraft electric generation system (1), which can achieve significantly increased capacity of electric generation, while adequately suppressing unwanted increase of a front face area of an aircraft engine as well as successfully dealing with considerably large changes of an engine spool speed. This electric generation system (1) is driven by the engine (E) and includes: a continuously variable transmission (CVT) (22) connected with a rotation shaft of the engine (9,21); an electric generator (23) located above the CVT (22) and driven by an output of the CVT; and a lubricating oil pump unit (24) located below the CVT (22) and also driven by the output of the CVT (22).
Inventors:
Tatsuhiko Goi
Kenichiro Tanaka
Masahide Nakamura
Koji Watanabe
Kenichiro Tanaka
Masahide Nakamura
Koji Watanabe
Application Number:
JP2009026220A
Publication Date:
June 15, 2011
Filing Date:
February 06, 2009
Export Citation:
Assignee:
Kawasaki Heavy Industries, Ltd.
International Classes:
B64D41/00; H02K7/116; H02K7/14; H02K7/18
Domestic Patent References:
| JP2008082208A | ||||
| JP2008239063A | ||||
| JP3440287B2 |
Attorney, Agent or Firm:
Shuji Sugimoto