The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Aug. 13, 2019

Filed:

Mar. 12, 2015
Applicant:

Japan Aerospace Exploration Agency, Tokyo, JP;

Inventors:

Hiroshi Kobayashi, Tokyo, JP;

Akira Nishizawa, Tokyo, JP;

Tomoko Iijima, Tokyo, JP;

Takeshi Tagashira, Tokyo, JP;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64D 27/24 (2006.01);
U.S. Cl.
CPC ...
B64D 27/24 (2013.01); B64C 2201/021 (2013.01); Y02T 10/7258 (2013.01); Y02T 50/64 (2013.01);
Abstract

To provide an electrified aircraft, and a method of controlling a regenerative electric power of the electrified aircraft where a path angle and a descending rate can be controlled with a good response independently from a speed while controlling the drag force of the propulsion drive system and where it is possible to maximize safely a generated electric power in each flight status at the time of descent or ascent. The electrified aircraft includes a propeller or a fan for propulsion; an electric drive motor for rotary-driving the propeller or the fan and for generating an electric power by the rotation of the propeller or the fan; and an estimation unit for estimating a drag force of the propeller or the fan or an electric power generation amount of the electric drive motor based on propulsion system parameters of the electric drive motor.


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