JP2014501380A5 - - Google Patents

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Publication number
JP2014501380A5
JP2014501380A5 JP2013547610A JP2013547610A JP2014501380A5 JP 2014501380 A5 JP2014501380 A5 JP 2014501380A5 JP 2013547610 A JP2013547610 A JP 2013547610A JP 2013547610 A JP2013547610 A JP 2013547610A JP 2014501380 A5 JP2014501380 A5 JP 2014501380A5
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JP
Japan
Prior art keywords
combustion
engine
channel
flow
individual
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JP2013547610A
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English (en)
Japanese (ja)
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JP2014501380A (ja
JP6170438B2 (ja
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Priority claimed from PCT/US2011/067373 external-priority patent/WO2012092264A1/en
Publication of JP2014501380A publication Critical patent/JP2014501380A/ja
Publication of JP2014501380A5 publication Critical patent/JP2014501380A5/ja
Application granted granted Critical
Publication of JP6170438B2 publication Critical patent/JP6170438B2/ja
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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JP2013547610A 2010-12-28 2011-12-27 エンジンおよび燃焼システム Expired - Fee Related JP6170438B2 (ja)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US201061427584P 2010-12-28 2010-12-28
US61/427,584 2010-12-28
PCT/US2011/067373 WO2012092264A1 (en) 2010-12-28 2011-12-27 Engine and combustion system

Publications (3)

Publication Number Publication Date
JP2014501380A JP2014501380A (ja) 2014-01-20
JP2014501380A5 true JP2014501380A5 (https=) 2015-02-19
JP6170438B2 JP6170438B2 (ja) 2017-07-26

Family

ID=46383498

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2013547610A Expired - Fee Related JP6170438B2 (ja) 2010-12-28 2011-12-27 エンジンおよび燃焼システム

Country Status (4)

Country Link
US (1) US9027324B2 (https=)
EP (1) EP2659187B1 (https=)
JP (1) JP6170438B2 (https=)
WO (1) WO2012092264A1 (https=)

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US9719678B2 (en) * 2010-09-22 2017-08-01 The United States Of America, As Represented By The Secretary Of The Navy Apparatus methods and systems of unidirectional propagation of gaseous detonations
EP2971514B1 (en) 2013-03-15 2020-07-22 Rolls-Royce North American Technologies, Inc. Continuous detonation combustion engine and system
WO2015200346A1 (en) 2014-06-23 2015-12-30 Air Products And Chemicals, Inc. Solid fuel burner and method of operating
EP3062023A1 (en) 2015-02-20 2016-08-31 Rolls-Royce North American Technologies, Inc. Wave rotor with piston assembly
US10393383B2 (en) 2015-03-13 2019-08-27 Rolls-Royce North American Technologies Inc. Variable port assemblies for wave rotors
CN106438014B (zh) * 2016-08-26 2019-06-18 南京航空航天大学 一种内燃波转子强化燃烧装置
US10520195B2 (en) * 2017-06-09 2019-12-31 General Electric Company Effervescent atomizing structure and method of operation for rotating detonation propulsion system
US10969107B2 (en) 2017-09-15 2021-04-06 General Electric Company Turbine engine assembly including a rotating detonation combustor
US11149954B2 (en) 2017-10-27 2021-10-19 General Electric Company Multi-can annular rotating detonation combustor
US11473780B2 (en) 2018-02-26 2022-10-18 General Electric Company Engine with rotating detonation combustion system
US11320147B2 (en) 2018-02-26 2022-05-03 General Electric Company Engine with rotating detonation combustion system
US11619172B1 (en) * 2022-03-01 2023-04-04 General Electric Company Detonation combustion systems
US12037962B1 (en) 2023-03-07 2024-07-16 General Electric Company Airbreathing propulsion engines including rotating detonation and bluff body systems
US12510249B2 (en) 2023-06-20 2025-12-30 Pratt & Whitney Canada Corp. Auxiliary power unit with pulse detonation combustion
CN119178170B (zh) * 2024-10-09 2025-09-12 南京航空航天大学 超燃冲压-斜爆震组合发动机燃烧室中的可分离支板结构

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JPH06280679A (ja) * 1993-03-26 1994-10-04 Ishikawajima Harima Heavy Ind Co Ltd 燃焼器とその保炎方法
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US5494438A (en) 1994-02-08 1996-02-27 National Science Council Sudden expansion combustion chamber with slotted inlet port
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