JP2014139430A5 - - Google Patents

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Publication number
JP2014139430A5
JP2014139430A5 JP2013236361A JP2013236361A JP2014139430A5 JP 2014139430 A5 JP2014139430 A5 JP 2014139430A5 JP 2013236361 A JP2013236361 A JP 2013236361A JP 2013236361 A JP2013236361 A JP 2013236361A JP 2014139430 A5 JP2014139430 A5 JP 2014139430A5
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JP
Japan
Prior art keywords
exhaust duct
flow path
station
duct flow
casing angle
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
JP2013236361A
Other languages
English (en)
Japanese (ja)
Other versions
JP2014139430A (ja
Filing date
Publication date
Priority claimed from US13/681,630 external-priority patent/US9311445B2/en
Application filed filed Critical
Publication of JP2014139430A publication Critical patent/JP2014139430A/ja
Publication of JP2014139430A5 publication Critical patent/JP2014139430A5/ja
Pending legal-status Critical Current

Links

JP2013236361A 2012-11-20 2013-11-15 高効率ガスタービン排気ダクト流路用の方法、プロセス、及びシステム Pending JP2014139430A (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US13/681,630 US9311445B2 (en) 2012-11-20 2012-11-20 Method, process, and system for high efficiency gas turbine exhaust duct flow-path
US13/681,630 2012-11-20

Publications (2)

Publication Number Publication Date
JP2014139430A JP2014139430A (ja) 2014-07-31
JP2014139430A5 true JP2014139430A5 (enExample) 2016-12-28

Family

ID=49585321

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2013236361A Pending JP2014139430A (ja) 2012-11-20 2013-11-15 高効率ガスタービン排気ダクト流路用の方法、プロセス、及びシステム

Country Status (4)

Country Link
US (1) US9311445B2 (enExample)
EP (1) EP2733315A2 (enExample)
JP (1) JP2014139430A (enExample)
CN (1) CN203822433U (enExample)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP6546481B2 (ja) * 2015-08-31 2019-07-17 川崎重工業株式会社 排気ディフューザ
US20170130596A1 (en) * 2015-11-11 2017-05-11 General Electric Company System for integrating sections of a turbine
US10570926B2 (en) * 2015-12-03 2020-02-25 The Boeing Company Variable-geometry ducted fan
DE102016217320A1 (de) * 2016-09-12 2018-03-15 Siemens Aktiengesellschaft Gasturbine mit getrennter Kühlung für Turbine und Abgasgehäuse
US10808576B2 (en) 2017-02-06 2020-10-20 General Electric Company Methods of replacing seals in exhaust frames of turbine systems and related components
US11560797B2 (en) * 2018-03-30 2023-01-24 Siemens Energy Global GmbH & Co. KG Endwall contouring for a conical endwall
US11423198B2 (en) * 2020-01-02 2022-08-23 Viettel Group Aerodynamic designing method of the central section of small size gas turbine engines
CN116595790B (zh) * 2023-05-26 2024-06-14 中国航发沈阳发动机研究所 一种发动机整机低导流通能力需求精准确定方法
US12253004B1 (en) * 2024-02-28 2025-03-18 Ge Infrastructure Technology Llc Inlet duct system for a heat recovery steam generator

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE59204947D1 (de) 1992-08-03 1996-02-15 Asea Brown Boveri Mehrzoniger Diffusor für Turbomaschine
JP2961067B2 (ja) * 1995-04-19 1999-10-12 三菱重工業株式会社 船舶用ガスタービンの排気装置
JP2002364310A (ja) * 2001-06-06 2002-12-18 Mitsubishi Heavy Ind Ltd 排気ディフューザ
JP5812567B2 (ja) * 2010-02-16 2015-11-17 三菱日立パワーシステムズ株式会社 タービン
JP5618879B2 (ja) * 2011-03-24 2014-11-05 株式会社東芝 軸流排気タービン

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