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Title:
VERTICAL TAKE-OFF AND LANDING AIRCRAFT AND METHOD FOR CONTROLLING VERTICAL TAKE-OFF AND LANDING AIRCRAFT
Document Type and Number:
WIPO Patent Application WO/2016/047343
Kind Code:
A1
Abstract:
This vertical take-off and landing aircraft (1) is provided with: a fuselage (2); a plurality of engines (3) that are installed on the fuselage and generate jet streams to produce thrust; an abnormality signal-acquiring unit for acquiring an abnormality signal that indicates the presence of a malfunctioning engine among the plurality of engines; and an engine control unit for outputting, on the basis of the abnormality signal, a stop signal for stopping a specific engine among the plurality of engines in operation.

Inventors:
KOBAYAKAWA, Toyonori (16-5, Konan 2-chome, Minato-k, Tokyo 15, 〒1088215, JP)
SAKAMOTO, Noboru (1 Furo-cho, Chikusa-ku, Nagoya-sh, Aichi 01, 〒4648601, JP)
HABAGUCHI, Yuta (1 Furo-cho, Chikusa-ku, Nagoya-sh, Aichi 01, 〒4648601, JP)
Application Number:
JP2015/073738
Publication Date:
March 31, 2016
Filing Date:
August 24, 2015
Export Citation:
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Assignee:
MITSUBISHI HEAVY INDUSTRIES, LTD. (16-5, Konan 2-chome Minato-k, Tokyo 15, 〒1088215, JP)
NATIONAL UNIVERSITY CORPORATION NAGOYA UNIVERSITY (1 Furo-cho, Chikusa-ku Nagoya-sh, Aichi 01, 〒4648601, JP)
International Classes:
B64C29/04; F02K9/90
Foreign References:
JP2004082999A2004-03-18
JP2002347698A2002-12-04
CN102114914A2011-07-06
US20110168835A12011-07-14
JP2009507700A2009-02-26
US3136499A1964-06-09
Attorney, Agent or Firm:
SAKAI, Hiroaki (Sakai International Patent Office, Toranomon Mitsui Building 8-1, Kasumigaseki 3-chome, Chiyoda-k, Tokyo 13, 〒1000013, JP)
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