Title:
推力発生装置及び航空機
Document Type and Number:
Japanese Patent JP6437347
Kind Code:
B2
Abstract:
This thrust force generation device (1) is provided with: a turbo fan engine unit (2) that is provided with a generator (7) for generating power using a rotation force of a drive shaft, and drives a fan (5) provided on the drive shaft using gas produced by burning fuel; a motor driving fan unit (3) that is provided with a motor (9) driven by power supplied from the generator (7), that is provided in parallel with the turbo fan engine unit (2), and that drives a fan (8) by using the motor (9); and a conducting unit (20) that connects the generator (7) to the motor (9), and supplies the power generated by the generator (7) to the motor (9). The turbo fan engine unit (2) and the motor driving fan unit (3) are integrated with each other, and the conducting unit (20) is disposed between the turbo fan engine unit (2) and the motor driving fan unit (3).
Inventors:
High Mimitsu
Hiroto Yokoi
Hiroto Yokoi
Application Number:
JP2015038282A
Publication Date:
December 12, 2018
Filing Date:
February 27, 2015
Export Citation:
Assignee:
MITSUBISHI HEAVY INDUSTRIES,LTD.
International Classes:
B64D27/24; B64C3/32; B64D27/26
Domestic Patent References:
| JP2013099158A | ||||
| JP2006205755A |
Foreign References:
| US20140367510 | ||||
| US20130094963 | ||||
| FR2994707A1 | ||||
| EP2998557A1 |
Attorney, Agent or Firm:
Noriharu Fujita
Kunio Ueda
Kunio Ueda