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Title:
HYBRID ROTOR DRIVE SYSTEM AND HYBRID ROTORCRAFT
Document Type and Number:
WIPO Patent Application WO/2024/090524
Kind Code:
A1
Abstract:
This hybrid rotor drive system comprises: a gas turbine engine which includes a compressor, a combustor, a turbine, and a first output shaft mechanically connecting the compressor to the turbine; an electric motor including a second output shaft; and a gear box which includes a first input interface, a second input interface, a speed reducer that reduces the speed of a rotational force input from the first input interface and the second input interface, and an output interface that outputs the rotational force with the speed reduced by the speed reducer to the rotor. The first output shaft of the gas turbine engine is mechanically connected to the first input interface. The second output shaft of the electric motor is mechanically connected to the second input interface.

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Inventors:
KATO TOSHIHIRO
MAEDA ATSUSHI
IMAI TAKUYA
OKUWA TATSUYA
TAKAHASHI MASANORI
HASHIMOTO DAI
Application Number:
PCT/JP2023/038723
Publication Date:
May 02, 2024
Filing Date:
October 26, 2023
Export Citation:
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Assignee:
KAWASAKI HEAVY IND LTD (JP)
International Classes:
B64D37/30; B64D27/10; B64D27/24; B64D31/06; B64U50/12; B64U50/19; B64U50/32; F01D15/10; F01K23/02; F02C6/12; F02C6/18; F02C7/36; F02C9/56; H01M8/04; H01M8/04858; H01M10/48
Foreign References:
US20150191250A12015-07-09
US8141360B12012-03-27
JP2012522173A2012-09-20
Attorney, Agent or Firm:
ARCO PATENT & TRADEMARK ATTORNEYS (JP)
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