HK1183511A1 - Tangential combustor with vaneless turbine for use on gas turbine engines - Google Patents

Tangential combustor with vaneless turbine for use on gas turbine engines

Info

Publication number
HK1183511A1
HK1183511A1 HK13110816.6A HK13110816A HK1183511A1 HK 1183511 A1 HK1183511 A1 HK 1183511A1 HK 13110816 A HK13110816 A HK 13110816A HK 1183511 A1 HK1183511 A1 HK 1183511A1
Authority
HK
Hong Kong
Prior art keywords
vaneless
turbine
gas turbine
combustor
tangential
Prior art date
Application number
HK13110816.6A
Other languages
English (en)
Chinese (zh)
Inventor
Majed Toqan
Brent Allan Gregory
Ryan Sadao Yamane
Jonathan David Regele
Original Assignee
Majed Toqan
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Majed Toqan filed Critical Majed Toqan
Publication of HK1183511A1 publication Critical patent/HK1183511A1/xx

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D9/00—Stators
    • F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • F01D9/023—Transition ducts between combustor cans and first stage of the turbine in gas-turbine engines; their cooling or sealings
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/002—Wall structures
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/007—Continuous combustion chambers using liquid or gaseous fuel constructed mainly of ceramic components
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/16—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration with devices inside the flame tube or the combustion chamber to influence the air or gas flow
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
    • F23R3/52—Toroidal combustion chambers
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/04—Air inlet arrangements
    • F23R3/06—Arrangement of apertures along the flame tube
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
HK13110816.6A 2010-05-25 2013-09-23 Tangential combustor with vaneless turbine for use on gas turbine engines HK1183511A1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US12/786,882 US8904799B2 (en) 2009-05-25 2010-05-25 Tangential combustor with vaneless turbine for use on gas turbine engines
PCT/US2011/037786 WO2011149973A1 (en) 2010-05-25 2011-05-24 Tangential combustor with vaneless turbine for use on gas turbine engines

Publications (1)

Publication Number Publication Date
HK1183511A1 true HK1183511A1 (en) 2013-12-27

Family

ID=44504537

Family Applications (1)

Application Number Title Priority Date Filing Date
HK13110816.6A HK1183511A1 (en) 2010-05-25 2013-09-23 Tangential combustor with vaneless turbine for use on gas turbine engines

Country Status (7)

Country Link
US (1) US8904799B2 (xx)
EP (1) EP2577169B1 (xx)
JP (1) JP5842311B2 (xx)
CN (1) CN102985758B (xx)
HK (1) HK1183511A1 (xx)
RU (1) RU2619963C2 (xx)
WO (1) WO2011149973A1 (xx)

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CN109654539B (zh) * 2018-12-07 2020-09-18 中国航发沈阳发动机研究所 一种干低排放燃气涡轮发动机燃烧室
KR102593508B1 (ko) * 2019-02-22 2023-10-24 한화에어로스페이스 주식회사 가스 터빈 엔진의 연료 노즐 구조체
EP3835657A1 (en) * 2019-12-10 2021-06-16 Siemens Aktiengesellschaft Combustion chamber with wall cooling
US11614233B2 (en) 2020-08-31 2023-03-28 General Electric Company Impingement panel support structure and method of manufacture
US11371702B2 (en) 2020-08-31 2022-06-28 General Electric Company Impingement panel for a turbomachine
US11460191B2 (en) 2020-08-31 2022-10-04 General Electric Company Cooling insert for a turbomachine
US11255545B1 (en) 2020-10-26 2022-02-22 General Electric Company Integrated combustion nozzle having a unified head end
US11549437B2 (en) * 2021-02-18 2023-01-10 Honeywell International Inc. Combustor for gas turbine engine and method of manufacture
EP4056903A1 (en) 2021-03-07 2022-09-14 CPS-Holding Limited Hydrogen-fueled combustor for gas turbines
CN114109711B (zh) * 2021-03-30 2023-08-18 李伟德 旋转发电装置及其制造和使用方法
CN113154451B (zh) * 2021-04-27 2022-09-06 西北工业大学 一种旋转爆震燃烧室的导向喷管
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Also Published As

Publication number Publication date
RU2012153796A (ru) 2014-06-27
EP2577169A1 (en) 2013-04-10
WO2011149973A1 (en) 2011-12-01
JP2013527421A (ja) 2013-06-27
EP2577169A4 (en) 2017-04-12
JP5842311B2 (ja) 2016-01-13
US8904799B2 (en) 2014-12-09
CN102985758B (zh) 2015-04-01
EP2577169B1 (en) 2018-09-19
RU2619963C2 (ru) 2017-05-22
WO2011149973A8 (en) 2013-02-28
US20110209482A1 (en) 2011-09-01
CN102985758A (zh) 2013-03-20

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