JP2013249843A5 - - Google Patents

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Publication number
JP2013249843A5
JP2013249843A5 JP2013114789A JP2013114789A JP2013249843A5 JP 2013249843 A5 JP2013249843 A5 JP 2013249843A5 JP 2013114789 A JP2013114789 A JP 2013114789A JP 2013114789 A JP2013114789 A JP 2013114789A JP 2013249843 A5 JP2013249843 A5 JP 2013249843A5
Authority
JP
Japan
Prior art keywords
rotor
steam turbine
flow
nozzles
steam
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.)
Pending
Application number
JP2013114789A
Other languages
English (en)
Japanese (ja)
Other versions
JP2013249843A (ja
Filing date
Publication date
Priority claimed from US13/487,332 external-priority patent/US9057275B2/en
Application filed filed Critical
Publication of JP2013249843A publication Critical patent/JP2013249843A/ja
Publication of JP2013249843A5 publication Critical patent/JP2013249843A5/ja
Pending legal-status Critical Current

Links

JP2013114789A 2012-06-04 2013-05-31 ノズルダイアフラムインデューサ Pending JP2013249843A (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US13/487,332 US9057275B2 (en) 2012-06-04 2012-06-04 Nozzle diaphragm inducer
US13/487,332 2012-06-04

Publications (2)

Publication Number Publication Date
JP2013249843A JP2013249843A (ja) 2013-12-12
JP2013249843A5 true JP2013249843A5 (enExample) 2016-07-14

Family

ID=48537832

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2013114789A Pending JP2013249843A (ja) 2012-06-04 2013-05-31 ノズルダイアフラムインデューサ

Country Status (5)

Country Link
US (1) US9057275B2 (enExample)
EP (1) EP2672062A3 (enExample)
JP (1) JP2013249843A (enExample)
CN (1) CN103452599B (enExample)
RU (1) RU2013125531A (enExample)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10113486B2 (en) * 2015-10-06 2018-10-30 General Electric Company Method and system for modulated turbine cooling
RU2621559C1 (ru) * 2016-07-05 2017-06-06 Публичное акционерное общество "Силовые машины-ЗТЛ, ЛМЗ, Электросила, Энергомашэкспорт" ( ПАО " Силовые машины"). Двухпоточный цилиндр паротурбинной установки с охлаждением ротора
RU2630817C1 (ru) * 2016-11-21 2017-09-13 федеральное государственное бюджетное образовательное учреждение высшего образования "Национальный исследовательский университет "МЭИ" (ФГБОУ ВО "НИУ "МЭИ") Двухъярусная ступень двухъярусного цилиндра низкого давления
CN108180076B (zh) * 2018-01-12 2024-04-12 南京航空航天大学 一种用于冷气预旋的双排喷嘴结构
US20230265862A1 (en) 2022-02-21 2023-08-24 General Electric Company Turbofan engine having angled inlet pre-swirl vanes
US11725526B1 (en) 2022-03-08 2023-08-15 General Electric Company Turbofan engine having nacelle with non-annular inlet
US12209557B1 (en) 2023-11-30 2025-01-28 General Electric Company Gas turbine engine with forward swept outlet guide vanes
US12385430B2 (en) 2023-11-30 2025-08-12 General Electric Company Gas turbine engine with forward swept outlet guide vanes
US12228037B1 (en) 2023-12-04 2025-02-18 General Electric Company Guide vane assembly with fixed and variable pitch inlet guide vanes
US12313021B1 (en) 2024-03-14 2025-05-27 General Electric Company Outer nacelle with inlet guide vanes and acoustic treatment

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KR20000071653A (ko) * 1999-04-15 2000-11-25 제이 엘. 차스킨, 버나드 스나이더, 아더엠. 킹 육상용 가스 터빈 및 가스 터빈의 하나의 단을 냉각시키는방법
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US8408868B2 (en) 2008-12-30 2013-04-02 General Electric Company Methods, systems and/or apparatus relating to inducers for turbine engines
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US8434766B2 (en) 2010-08-18 2013-05-07 General Electric Company Turbine engine seals

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