JP2013199927A5 - - Google Patents

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Publication number
JP2013199927A5
JP2013199927A5 JP2013050195A JP2013050195A JP2013199927A5 JP 2013199927 A5 JP2013199927 A5 JP 2013199927A5 JP 2013050195 A JP2013050195 A JP 2013050195A JP 2013050195 A JP2013050195 A JP 2013050195A JP 2013199927 A5 JP2013199927 A5 JP 2013199927A5
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JP
Japan
Prior art keywords
airfoil
adjacent
bowl
bulge
platform
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.)
Granted
Application number
JP2013050195A
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English (en)
Japanese (ja)
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JP6183991B2 (ja
JP2013199927A (ja
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Publication date
Priority claimed from US13/429,312 external-priority patent/US9085985B2/en
Application filed filed Critical
Publication of JP2013199927A publication Critical patent/JP2013199927A/ja
Publication of JP2013199927A5 publication Critical patent/JP2013199927A5/ja
Application granted granted Critical
Publication of JP6183991B2 publication Critical patent/JP6183991B2/ja
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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JP2013050195A 2012-03-23 2013-03-13 スカラップ形状の表面のタービンステージ Expired - Fee Related JP6183991B2 (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US13/429,312 US9085985B2 (en) 2012-03-23 2012-03-23 Scalloped surface turbine stage
US13/429,312 2012-03-23

Publications (3)

Publication Number Publication Date
JP2013199927A JP2013199927A (ja) 2013-10-03
JP2013199927A5 true JP2013199927A5 (enExample) 2016-04-28
JP6183991B2 JP6183991B2 (ja) 2017-08-23

Family

ID=47913122

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2013050195A Expired - Fee Related JP6183991B2 (ja) 2012-03-23 2013-03-13 スカラップ形状の表面のタービンステージ

Country Status (6)

Country Link
US (1) US9085985B2 (enExample)
EP (1) EP2642075B1 (enExample)
JP (1) JP6183991B2 (enExample)
CN (1) CN103321686B (enExample)
BR (1) BR102013006076A2 (enExample)
CA (1) CA2808804A1 (enExample)

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US9598967B2 (en) * 2012-12-18 2017-03-21 United Technologies Corporation Airfoil member and composite platform having contoured endwall
FR3011888B1 (fr) * 2013-10-11 2018-04-20 Snecma Piece de turbomachine a surface non-axisymetrique
US10294805B2 (en) * 2013-12-20 2019-05-21 United Technologies Corporation Gas turbine engine integrally bladed rotor with asymmetrical trench fillets
JP2017528632A (ja) * 2014-06-18 2017-09-28 シーメンス エナジー インコーポレイテッド ガスタービンエンジン用のエンドウォール構成
US10060263B2 (en) * 2014-09-15 2018-08-28 United Technologies Corporation Incidence-tolerant, high-turning fan exit stator
US10287901B2 (en) 2014-12-08 2019-05-14 United Technologies Corporation Vane assembly of a gas turbine engine
US20160237914A1 (en) * 2015-02-18 2016-08-18 United Technologies Corporation Geared Turbofan With High Gear Ratio And High Temperature Capability
DE102015208572A1 (de) * 2015-05-08 2016-12-15 MTU Aero Engines AG Gasturbinen-Leitschaufelelement
US10240462B2 (en) 2016-01-29 2019-03-26 General Electric Company End wall contour for an axial flow turbine stage
US10161255B2 (en) 2016-02-09 2018-12-25 General Electric Company Turbine nozzle having non-axisymmetric endwall contour (EWC)
US10156149B2 (en) * 2016-02-09 2018-12-18 General Electric Company Turbine nozzle having fillet, pinbank, throat region and profile
US10190417B2 (en) 2016-02-09 2019-01-29 General Electric Company Turbine bucket having non-axisymmetric endwall contour and profile
US10001014B2 (en) 2016-02-09 2018-06-19 General Electric Company Turbine bucket profile
US10125623B2 (en) 2016-02-09 2018-11-13 General Electric Company Turbine nozzle profile
US10190421B2 (en) 2016-02-09 2019-01-29 General Electric Company Turbine bucket having tip shroud fillet, tip shroud cross-drilled apertures and profile
US10221710B2 (en) 2016-02-09 2019-03-05 General Electric Company Turbine nozzle having non-axisymmetric endwall contour (EWC) and profile
US10196908B2 (en) 2016-02-09 2019-02-05 General Electric Company Turbine bucket having part-span connector and profile
DE102016207212A1 (de) 2016-04-28 2017-11-02 MTU Aero Engines AG Leitschaufelkranz für eine Strömungsmaschine
DE102016211315A1 (de) * 2016-06-23 2017-12-28 MTU Aero Engines AG Lauf- oder Leitschaufel mit erhabenen Bereichen
US10526899B2 (en) * 2017-02-14 2020-01-07 General Electric Company Turbine blade having a tip shroud
US10577955B2 (en) * 2017-06-29 2020-03-03 General Electric Company Airfoil assembly with a scalloped flow surface
US10508550B2 (en) * 2017-10-25 2019-12-17 United Technologies Corporation Geared gas turbine engine
CN111699301B (zh) * 2018-02-15 2023-07-28 西门子能源全球两合公司 涡轮叶片的组件和相对应的制品
WO2019190539A1 (en) * 2018-03-30 2019-10-03 Siemens Aktiengesellschaft Turbine stage platform with endwall contouring incorporating wavy mate face
WO2019190540A1 (en) * 2018-03-30 2019-10-03 Siemens Aktiengesellschaft Endwall contouring for a conical endwall
GB201806631D0 (en) * 2018-04-24 2018-06-06 Rolls Royce Plc A combustion chamber arrangement and a gas turbine engine comprising a combustion chamber arrangement
BE1026579B1 (fr) * 2018-08-31 2020-03-30 Safran Aero Boosters Sa Aube a protuberance pour compresseur de turbomachine
US10844728B2 (en) * 2019-04-17 2020-11-24 General Electric Company Turbine engine airfoil with a trailing edge
US11566530B2 (en) * 2019-11-26 2023-01-31 General Electric Company Turbomachine nozzle with an airfoil having a circular trailing edge
US11415010B1 (en) 2021-07-05 2022-08-16 Doosan Enerbility Co., Ltd. Turbine nozzle and gas turbine including the same
CN116792159A (zh) * 2023-06-09 2023-09-22 西北工业大学 一种涡轮用角度可调带气膜冷却孔的端壁翼刀组件
DE102023126341A1 (de) * 2023-09-27 2025-03-27 MTU Aero Engines AG Beschaufelung für eine Turbomaschine, sowie Turbomaschine
CN119933805A (zh) * 2023-11-03 2025-05-06 中国航发商用航空发动机有限责任公司 动叶缘板、动叶及动叶缘板设计方法
KR20250125563A (ko) * 2024-02-15 2025-08-22 두산에너빌리티 주식회사 비-선대칭 엔드월 윤곽을 가진 터빈 블레이드 및 이를 포함하는 가스 터빈
US12480412B2 (en) * 2024-02-16 2025-11-25 Rtx Corporation Insertion of ceramic members for gas path endwall contouring

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US7887297B2 (en) 2006-05-02 2011-02-15 United Technologies Corporation Airfoil array with an endwall protrusion and components of the array
GB0704426D0 (en) 2007-03-08 2007-04-18 Rolls Royce Plc Aerofoil members for a turbomachine
JP5291355B2 (ja) 2008-02-12 2013-09-18 三菱重工業株式会社 タービン翼列エンドウォール
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