Invention Grant
- Patent Title: Thrust force generation device and aircraft
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Application No.: US15552699Application Date: 2016-02-24
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Publication No.: US10752369B2Publication Date: 2020-08-25
- Inventor: Hikaru Takami , Yuto Yokoi
- Applicant: MITSUBISHI HEAVY INDUSTRIES, LTD.
- Applicant Address: JP Tokyo
- Assignee: MITSUBISHI HEAVY INDUSTRIES, LTD.
- Current Assignee: MITSUBISHI HEAVY INDUSTRIES, LTD.
- Current Assignee Address: JP Tokyo
- Agent Manabu Kanesaka; Benjamin Hauptman; Kenneth Berner
- Priority: com.zzzhc.datahub.patent.etl.us.BibliographicData$PriorityClaim@2263aca7
- International Application: PCT/JP2016/055336 WO 20160224
- International Announcement: WO2016/136770 WO 20160901
- Main IPC: B64D27/02
- IPC: B64D27/02 ; B64D27/12 ; B64D27/24 ; B64D27/26 ; F02K5/00 ; B64D27/18 ; F02C6/00 ; F02C7/20 ; F02K3/06 ; F02C3/04

Abstract:
The thrust force generation device is provided with: a turbo fan engine unit that includes a generator for generating power using a rotation force of a drive shaft, and that drives a fan placed on the drive shaft using gas produced by combusting fuel; a motor driven fan unit that includes a motor driven by power supplied from the generator, that is placed in parallel with the turbo fan engine unit, and that drives a fan by using the motor; and a conducting unit that connects the generator to the motor, and supplies the power generated by the generator to the motor. The turbo fan engine unit and the motor driven fan unit are integrated with each other, and the conducting unit is placed between the turbo fan engine unit and the motor driven fan unit.
Public/Granted literature
- US20180044028A1 THRUST FORCE GENERATION DEVICE AND AIRCRAFT Public/Granted day:2018-02-15
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