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 (JP)
SAKAMOTO NOBORU (JP)
HABAGUCHI YUTA (JP)
SAKAMOTO NOBORU (JP)
HABAGUCHI YUTA (JP)
Application Number:
PCT/JP2015/073738
Publication Date:
March 31, 2016
Filing Date:
August 24, 2015
Export Citation:
Assignee:
MITSUBISHI HEAVY IND LTD (JP)
UNIV NAGOYA NAT UNIV CORP (JP)
UNIV NAGOYA NAT UNIV CORP (JP)
International Classes:
B64C29/04; F02K9/90
Foreign References:
| JP2004082999A | 2004-03-18 | |||
| JP2002347698A | 2002-12-04 | |||
| CN102114914A | 2011-07-06 | |||
| US20110168835A1 | 2011-07-14 | |||
| JP2009507700A | 2009-02-26 | |||
| US3136499A | 1964-06-09 |
Attorney, Agent or Firm:
SAKAI, HIROAKI (JP)
Hiroaki Sakai (JP)
Hiroaki Sakai (JP)
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