KR102915025B1 - 회전식 내연 기관 엔진 - Google Patents

회전식 내연 기관 엔진

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Publication number
KR102915025B1
KR102915025B1 KR1020217030019A KR20217030019A KR102915025B1 KR 102915025 B1 KR102915025 B1 KR 102915025B1 KR 1020217030019 A KR1020217030019 A KR 1020217030019A KR 20217030019 A KR20217030019 A KR 20217030019A KR 102915025 B1 KR102915025 B1 KR 102915025B1
Authority
KR
South Korea
Prior art keywords
combustion
intake
exhaust
air
turbine
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Active
Application number
KR1020217030019A
Other languages
English (en)
Korean (ko)
Other versions
KR20210145740A (ko
Inventor
찰스 매티슨 그린
그랜트 오. 머스그로브
케빈 엘. 호그
데이비드 피. 브래니언
토마스 이. 레인하트
Original Assignee
그린 엔진, 엘엘씨
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Filing date
Publication date
Application filed by 그린 엔진, 엘엘씨 filed Critical 그린 엔진, 엘엘씨
Publication of KR20210145740A publication Critical patent/KR20210145740A/ko
Application granted granted Critical
Publication of KR102915025B1 publication Critical patent/KR102915025B1/ko
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C5/00Gas-turbine plants characterised by the working fluid being generated by intermittent combustion
    • F02C5/12Gas-turbine plants characterised by the working fluid being generated by intermittent combustion the combustion chambers having inlet or outlet valves, e.g. Holzwarth gas-turbine plants
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C3/00Gas-turbine plants characterised by the use of combustion products as the working fluid
    • F02C3/14Gas-turbine plants characterised by the use of combustion products as the working fluid characterised by the arrangement of the combustion chamber in the plant
    • F02C3/16Gas-turbine plants characterised by the use of combustion products as the working fluid characterised by the arrangement of the combustion chamber in the plant the combustion chambers being formed at least partly in the turbine rotor or in an other rotating part of the plant
    • F02C3/165Gas-turbine plants characterised by the use of combustion products as the working fluid characterised by the arrangement of the combustion chamber in the plant the combustion chambers being formed at least partly in the turbine rotor or in an other rotating part of the plant the combustion chamber contributes to the driving force by creating reactive thrust
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C5/00Gas-turbine plants characterised by the working fluid being generated by intermittent combustion
    • F02C5/02Gas-turbine plants characterised by the working fluid being generated by intermittent combustion characterised by the arrangement of the combustion chamber in the chamber in the plant
    • F02C5/04Gas-turbine plants characterised by the working fluid being generated by intermittent combustion characterised by the arrangement of the combustion chamber in the chamber in the plant the combustion chambers being formed at least partly in the turbine rotor
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C6/00Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use
    • F02C6/20Adaptations of gas-turbine plants for driving vehicles
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/42Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
    • F23R3/56Combustion chambers having rotary flame tubes

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Supercharger (AREA)
  • Engine Equipment That Uses Special Cycles (AREA)
KR1020217030019A 2019-02-20 2020-02-20 회전식 내연 기관 엔진 Active KR102915025B1 (ko)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US201962808174P 2019-02-20 2019-02-20
US62/808,174 2019-02-20
PCT/US2020/019026 WO2020172399A1 (en) 2019-02-20 2020-02-20 Rotating internal combustion engine

Publications (2)

Publication Number Publication Date
KR20210145740A KR20210145740A (ko) 2021-12-02
KR102915025B1 true KR102915025B1 (ko) 2026-01-21

Family

ID=72141579

Family Applications (1)

Application Number Title Priority Date Filing Date
KR1020217030019A Active KR102915025B1 (ko) 2019-02-20 2020-02-20 회전식 내연 기관 엔진

Country Status (7)

Country Link
US (2) US12398670B2 (https=)
EP (1) EP3927952A4 (https=)
JP (1) JP7587512B2 (https=)
KR (1) KR102915025B1 (https=)
CA (1) CA3130896A1 (https=)
MX (2) MX2021010045A (https=)
WO (1) WO2020172399A1 (https=)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20230193759A1 (en) * 2021-12-22 2023-06-22 Cnx Resources Corporation Expander systems for harnessing energy from pressurized fluid flow
CN116608487B (zh) * 2023-02-13 2025-11-25 北京航空航天大学 一种应用于变循环发动机的加力燃烧室
CN116378825B (zh) * 2023-05-18 2025-10-17 宝鸡市荣豪钛业有限公司 一种涡轮发动机

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JP2010138710A (ja) * 2008-12-09 2010-06-24 Hino Motors Ltd 二段過給システム
US20160194087A1 (en) * 2013-03-15 2016-07-07 Indiana University Research & Technology Corporation Hybrid Wave Rotor Propulsion System

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US1319752A (en) * 1919-10-28 Engine
US2395404A (en) * 1939-10-18 1946-02-26 Daniel And Florence Guggenheim Aerial propulsion apparatus
US2705867A (en) 1949-06-30 1955-04-12 Curtiss Wright Corp Engine having a rotor with a plurality of circumferentially-spaced combustion chambers
US3321911A (en) * 1965-02-12 1967-05-30 Myles Tommie Lynn Gas turbine engine with rotating combustion chamber
US3417564A (en) * 1967-04-19 1968-12-24 John G. Call Jet engine with relatively rotatable combustion means, intake manifold and exhaust manifold
US3811275A (en) * 1969-04-02 1974-05-21 A Mastrobuono Rotary turbine engine
US3639076A (en) * 1970-05-28 1972-02-01 Gen Electric Constant power control system for gas turbine
US3771311A (en) * 1971-02-01 1973-11-13 Exxon Research Engineering Co Power system
US4232515A (en) * 1978-03-06 1980-11-11 The Boeing Company Supersonic cruise airplane and engine
US4620414A (en) * 1983-07-27 1986-11-04 Dieter Christ Gas turbine engine
JPS63268938A (ja) * 1987-04-27 1988-11-07 Nec Corp ガスタ−ビンエンジン
DE4113680A1 (de) * 1991-03-12 1992-09-17 Asea Brown Boveri Gasturbogruppe
US5372005A (en) * 1992-09-14 1994-12-13 Lawler; Shawn P. Method and apparatus for power generation
US6460342B1 (en) * 1999-04-26 2002-10-08 Advanced Research & Technology Institute Wave rotor detonation engine
WO2004072451A1 (en) * 2003-02-12 2004-08-26 Ishikawajima-Harima Heavy Industries Co., Ltd. Pulse detonation engine system for driving turbine
US7150143B2 (en) * 2003-07-21 2006-12-19 General Electric Company Hybrid fuel cell-pulse detonation power system
US7278256B2 (en) * 2004-11-08 2007-10-09 United Technologies Corporation Pulsed combustion engine
WO2008070210A2 (en) * 2006-06-15 2008-06-12 Indiana University Research And Technology Corporation Pilot fuel injection for a wave rotor engine
US7841163B2 (en) * 2006-11-13 2010-11-30 Hamilton Sundstrand Corporation Turbofan emergency generator
JP2011102669A (ja) * 2009-11-10 2011-05-26 Mitsubishi Heavy Ind Ltd ガスタービン燃焼器及びガスタービン
US8733317B2 (en) 2009-12-14 2014-05-27 Gotek Energy, Inc. Rotary, internal combustion engine
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KR20150032911A (ko) * 2012-07-24 2015-03-30 브렌트 웨이-테 이 내부 폭발 엔진, 그것을 포함하는 하이브리드 엔진, 및 그것의 제조 및 사용 방법
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EP3056713B1 (en) * 2015-02-11 2017-10-25 Rolls-Royce North American Technologies, Inc. Exhaust mixer for wave rotor assembly
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JP2010138710A (ja) * 2008-12-09 2010-06-24 Hino Motors Ltd 二段過給システム
US20160194087A1 (en) * 2013-03-15 2016-07-07 Indiana University Research & Technology Corporation Hybrid Wave Rotor Propulsion System

Also Published As

Publication number Publication date
MX2025009130A (es) 2025-09-02
CA3130896A1 (en) 2020-08-27
US20200271047A1 (en) 2020-08-27
US20260104006A1 (en) 2026-04-16
WO2020172399A1 (en) 2020-08-27
JP2022520878A (ja) 2022-04-01
EP3927952A4 (en) 2023-05-31
KR20210145740A (ko) 2021-12-02
US12398670B2 (en) 2025-08-26
EP3927952A1 (en) 2021-12-29
MX2021010045A (es) 2021-11-17
JP7587512B2 (ja) 2024-11-20

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