Title:
POWER GENERATION SYSTEM AND AIRCRAFT
Document Type and Number:
WIPO Patent Application WO/2023/013398
Kind Code:
A1
Abstract:
[Problem] To provide: a power generation system capable of preventing the occurrence of failures of an engine caused by sharp reductions in the shaft torque of a power generator; and an aircraft provided with this power generation system. [Solution] A power generation system according to one embodiment of the present invention includes an engine, a power generator, a detection unit, and a control device. The engine includes a compressor including a rotary shaft. The power generator is connected to the rotary shaft, and generates power by the rotational force of the rotary shaft. The detection unit detects a shaft torque of the power generator. The control device controls an operating state of the engine or the power generator on the basis of the shaft torque.
Inventors:
KOBAYASHI HIROSHI (JP)
IIJIMA RYUJI (JP)
NOGUCHI SHUNSUKE (JP)
NISHIZAWA AKIRA (JP)
IIJIMA RYUJI (JP)
NOGUCHI SHUNSUKE (JP)
NISHIZAWA AKIRA (JP)
Application Number:
PCT/JP2022/028032
Publication Date:
February 09, 2023
Filing Date:
July 19, 2022
Export Citation:
Assignee:
JAPAN AEROSPACE EXPLORATION (JP)
International Classes:
H02P9/04; B64D27/10; B64D41/00; F01D15/10; F02C9/00; F02C9/28; F02C9/32
Foreign References:
| JP2013231366A | 2013-11-14 | |||
| JP5220242B1 | 2013-06-26 | |||
| JP2011230524A | 2011-11-17 | |||
| JP2005343458A | 2005-12-15 | |||
| JPH09193675A | 1997-07-29 |
Attorney, Agent or Firm:
MINAMI AOYAMA PATENT AND TRADEMARK ATTORNEYS (JP)
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