Title:
ELECTRIFIED AIRCRAFT AND REGENERATED ELECTRIC POWER CONTROL METHOD FOR ELECTRIFIED AIRCRAFT
Document Type and Number:
WIPO Patent Application WO/2015/146608
Kind Code:
A1
Abstract:
[Problem] To provide electrified aircraft such that the path angle and rate of descent can be controlled independently of speed and with high response by operating the drag of a propulsion drive system whereby electric power generated during descent or in an updraft can be maximized safely in various flying states, and to provide a regenerated electric power control method for the electrified aircraft.
[Solution] This electrified aircraft is provided with: a propeller for propulsion; an electric drive motor for rotatably driving the propeller and generating electricity by the rotation of the propeller; and an estimation unit that estimates the drag of the propeller or a fan on the basis of a propulsion system parameter of the electric drive motor.
Inventors:
KOBAYASHI HIROSHI (JP)
NISHIZAWA AKIRA (JP)
IIJIMA TOMOKO (JP)
TAGASHIRA TAKESHI (JP)
NISHIZAWA AKIRA (JP)
IIJIMA TOMOKO (JP)
TAGASHIRA TAKESHI (JP)
Application Number:
PCT/JP2015/057317
Publication Date:
October 01, 2015
Filing Date:
March 12, 2015
Export Citation:
Assignee:
JAPAN AEROSPACE EXPLORATION (JP)
International Classes:
B64D27/24; B64D31/14
Domestic Patent References:
WO2014020596A1 | 2014-02-06 | |||
WO2014053057A1 | 2014-04-10 | |||
WO2014089509A1 | 2014-06-12 |
Foreign References:
JP2013169972A | 2013-09-02 | |||
JP5046104B2 | 2012-10-10 | |||
JP3942570B2 | 2007-07-11 | |||
JP2011031879A | 2011-02-17 | |||
JP2014172435A | 2014-09-22 |
Attorney, Agent or Firm:
OMORI, JUNICHI (JP)
Omori Junichi (JP)
Omori Junichi (JP)
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