JP2021014824A5 - - Google Patents

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Publication number
JP2021014824A5
JP2021014824A5 JP2019130169A JP2019130169A JP2021014824A5 JP 2021014824 A5 JP2021014824 A5 JP 2021014824A5 JP 2019130169 A JP2019130169 A JP 2019130169A JP 2019130169 A JP2019130169 A JP 2019130169A JP 2021014824 A5 JP2021014824 A5 JP 2021014824A5
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JP
Japan
Prior art keywords
turbine
combustion gas
outer shell
gas
external air
Prior art date
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Granted
Application number
JP2019130169A
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English (en)
Japanese (ja)
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JP7297574B2 (ja
JP2021014824A (ja
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Publication date
Application filed filed Critical
Priority to JP2019130169A priority Critical patent/JP7297574B2/ja
Priority claimed from JP2019130169A external-priority patent/JP7297574B2/ja
Priority to US17/624,965 priority patent/US11885232B2/en
Priority to PCT/JP2020/005608 priority patent/WO2021009953A1/ja
Priority to DE112020003364.3T priority patent/DE112020003364T5/de
Publication of JP2021014824A publication Critical patent/JP2021014824A/ja
Publication of JP2021014824A5 publication Critical patent/JP2021014824A5/ja
Application granted granted Critical
Publication of JP7297574B2 publication Critical patent/JP7297574B2/ja
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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JP2019130169A 2019-07-12 2019-07-12 ガスタービンシステムおよびそれを備えた移動体 Active JP7297574B2 (ja)

Priority Applications (4)

Application Number Priority Date Filing Date Title
JP2019130169A JP7297574B2 (ja) 2019-07-12 2019-07-12 ガスタービンシステムおよびそれを備えた移動体
US17/624,965 US11885232B2 (en) 2019-07-12 2020-02-13 Gas turbine system and movable body including the same
PCT/JP2020/005608 WO2021009953A1 (ja) 2019-07-12 2020-02-13 ガスタービンシステムおよびそれを備えた移動体
DE112020003364.3T DE112020003364T5 (de) 2019-07-12 2020-02-13 Gasturbinensystem und Bewegungskörper, der dasselbe enthält

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP2019130169A JP7297574B2 (ja) 2019-07-12 2019-07-12 ガスタービンシステムおよびそれを備えた移動体

Publications (3)

Publication Number Publication Date
JP2021014824A JP2021014824A (ja) 2021-02-12
JP2021014824A5 true JP2021014824A5 (enExample) 2022-07-13
JP7297574B2 JP7297574B2 (ja) 2023-06-26

Family

ID=74210520

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2019130169A Active JP7297574B2 (ja) 2019-07-12 2019-07-12 ガスタービンシステムおよびそれを備えた移動体

Country Status (4)

Country Link
US (1) US11885232B2 (enExample)
JP (1) JP7297574B2 (enExample)
DE (1) DE112020003364T5 (enExample)
WO (1) WO2021009953A1 (enExample)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US12085043B1 (en) 2023-06-16 2024-09-10 Pratt & Whitney Canada Corp. Aircraft propulsion system with turbine engine and exhaust condenser

Family Cites Families (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2944624A (en) 1957-08-07 1960-07-12 Rolls Royce Jet noise suppressor nozzle
US4099375A (en) 1977-02-03 1978-07-11 The United States Of America As Represented By The Secretary Of The Navy Exhaust plume reduction and cooling system
US4215536A (en) 1978-12-26 1980-08-05 The Boeing Company Gas turbine mixer apparatus
US4958489A (en) 1985-03-04 1990-09-25 General Electric Company Means for controlling augmentor liner coolant flow pressure in a mixed flow, variable cycle gas turbine engine
US5203164A (en) 1990-06-06 1993-04-20 Paulson Allen E Method and apparatus for quieting a turbojet engine
US5706651A (en) * 1995-08-29 1998-01-13 Burbank Aeronautical Corporation Ii Turbofan engine with reduced noise
US5947412A (en) * 1997-01-10 1999-09-07 Titan Corporation Jet engine noise suppressor assembly
US6612106B2 (en) 2000-05-05 2003-09-02 The Boeing Company Segmented mixing device having chevrons for exhaust noise reduction in jet engines
US7047725B2 (en) 2003-05-28 2006-05-23 Rohr, Inc. Assembly and method for aircraft engine noise reduction
JP4092728B2 (ja) 2005-01-25 2008-05-28 独立行政法人 宇宙航空研究開発機構 航空機用推進システム
FR2892152B1 (fr) 2005-10-19 2007-11-23 Airbus France Sas Turbomoteur a bruit de jet attenue
US7870722B2 (en) 2006-12-06 2011-01-18 The Boeing Company Systems and methods for passively directing aircraft engine nozzle flows
JP5447920B2 (ja) 2009-03-25 2014-03-19 独立行政法人 宇宙航空研究開発機構 航空機用排気ノズル
US8984890B2 (en) * 2011-10-31 2015-03-24 General Electric Company Turbofan engine mixer assembly
FR3039517B1 (fr) 2015-07-31 2019-05-17 Safran Nacelles Structure d’attenuation acoustique a multiples degres d’attenuation pour ensemble propulsif d’aeronef
US10392120B2 (en) * 2016-04-19 2019-08-27 General Electric Company Propulsion engine for an aircraft
US10308366B2 (en) 2016-08-22 2019-06-04 General Electric Company Embedded electric machine

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