JP4778758B2 - タービンノズルのレール保持のための機械的解決法 - Google Patents
タービンノズルのレール保持のための機械的解決法 Download PDFInfo
- Publication number
- JP4778758B2 JP4778758B2 JP2005273095A JP2005273095A JP4778758B2 JP 4778758 B2 JP4778758 B2 JP 4778758B2 JP 2005273095 A JP2005273095 A JP 2005273095A JP 2005273095 A JP2005273095 A JP 2005273095A JP 4778758 B2 JP4778758 B2 JP 4778758B2
- Authority
- JP
- Japan
- Prior art keywords
- turbine
- rail
- nozzle
- support ring
- segment
- 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.)
- Expired - Fee Related
Links
- 230000014759 maintenance of location Effects 0.000 title description 7
- 241000283216 Phocidae Species 0.000 claims description 15
- 125000006850 spacer group Chemical group 0.000 claims description 13
- 239000012530 fluid Substances 0.000 claims 1
- 230000000452 restraining effect Effects 0.000 claims 1
- 238000001816 cooling Methods 0.000 description 3
- 230000001052 transient effect Effects 0.000 description 3
- 238000009434 installation Methods 0.000 description 2
- 230000003044 adaptive effect Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 230000000644 propagated effect Effects 0.000 description 1
- 238000007789 sealing Methods 0.000 description 1
- 230000011218 segmentation Effects 0.000 description 1
- 238000000926 separation method Methods 0.000 description 1
Images
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
- F01D21/00—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for
- F01D21/04—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for responsive to undesired position of rotor relative to stator or to breaking-off of a part of the rotor, e.g. indicating such position
- F01D21/045—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for responsive to undesired position of rotor relative to stator or to breaking-off of a part of the rotor, e.g. indicating such position special arrangements in stators or in rotors dealing with breaking-off of part of rotor
-
- 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
- F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
- F01D25/24—Casings; Casing parts, e.g. diaphragms, casing fastenings
- F01D25/246—Fastening of diaphragms or stator-rings
-
- 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
- F01D9/04—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
- F01D9/041—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector using blades
-
- 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49316—Impeller making
- Y10T29/4932—Turbomachine making
- Y10T29/49323—Assembling fluid flow directing devices, e.g., stators, diaphragms, nozzles
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Description
12 ノズル
13 ノズルセグメント
14 バケット
16 ロータ
18 外側プラットホーム
20 内側プラットホーム
22 翼形部
25 割れ
26 外側保持リング
28 内側プラットホームレール
30 内側支持リング
32 翼弦方向ランドシール
34 ボルト又はピン
36 内側リテーナセグメント
38 内側リテーナスペーサ
40 内側リテーナセグメントの半径方向外側縁部
50 内側リテーナセグメントの円錐傾斜面
52 内側プラットホームレールの円錐傾斜面
Claims (10)
- 少なくとも1つのステータ翼形部(22)を有しかつ内側プラットホームレール(28)を含むタービンノズルセグメント(13)と、
その1つの側面上でその一部が前記レール(28)と軸方向に整合したタービンノズル内側支持リング(30)と、
前記内側支持リング(30)に固定される内側リテーナセグメント(36)であって、その一部が前記内側支持リング(30)とは反対側の前記レール(28)の軸方向側面で該レール(28)に対して軸方向に間隔を置いて位置する内側リテーナセグメント(36)と、
前記内側リテーナセグメント(36)上の第1の面(50)と、
前記第1の面(50)と間隔を置いて対向した、前記内側プラットホームレール(28)上の第2の面(52)と、を含み、
それによって、前記タービンノズルセグメント(13)における構造的破損に応答して、前記2つの対向する第1の面(50)と第2の面(52)が接触して前記内側リテーナセグメント(36)と内側支持リング(30)との間に該内側プラットホームレール(28)を拘束する、
タービン。 - 前記タービンノズルセグメント(13)における構造的破損に応答して、前記第1の面(50)と第2の面(52)が接触することにより、前記ノズルセグメント(13)の内側プラットホーム(20)が下流方向にタービンの回転しているハードウエア内に逸失するのを防止する楔ロックを生じる、請求項1記載のタービン。
- 前記第1及び第2の面(50、52)が傾斜面、円錐面又は円錐傾斜面である、請求項1又は請求項2記載のタービン。
- 前記第1の面(50)と第2の面(52)の間にシール(39)が設けられる、請求項1乃至請求項3のいずれか1項記載のタービン。
- 前記レール(28)が弓形の突出ランド(31)を有していて、前記内側支持リング(30)の前記軸方向側面との間に、翼弦方向ランドシール(32)を形成している、請求項1乃至請求項4のいずれか1項記載のタービン。
- 前記内側リテーナセグメント(36)の半径方向外側縁部(40)が、前記内側支持リング(30)に向かう方向に軸方向に拡大している、請求項1乃至請求項5のいずれか1項記載のタービン。
- 前記内側リテーナセグメント(36)の半径方向外側縁部(40)がさらに、少なくとも1つの弓形内側リテーナスペーサ(38)によって、前記リテーナセグメント(36)と内側支持リング(30)との間に延びる前記レール(28)から間隔を置いて配置されている、請求項6記載のタービン。
- 前記内側リテーナセグメント(36)上の第1の面(50)が、該内側リテーナセグメント(36)の半径方向外側縁部(40)上に設置されている、請求項6記載のタービン。
- 前記内側プラットホームレール(28)の半径方向内側縁部が、前記内側支持リング(30)から離れる方向に軸方向に拡大している、請求項6記載のタービン。
- 前記内側プラットホームレール(28)上の第2の面(52)が、該内側プラットホームレールの半径方向内側縁部上に設置されている、請求項9記載のタービン。
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US10/947,450 | 2004-09-23 | ||
US10/947,450 US7160078B2 (en) | 2004-09-23 | 2004-09-23 | Mechanical solution for rail retention of turbine nozzles |
Publications (2)
Publication Number | Publication Date |
---|---|
JP2006097681A JP2006097681A (ja) | 2006-04-13 |
JP4778758B2 true JP4778758B2 (ja) | 2011-09-21 |
Family
ID=36062381
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP2005273095A Expired - Fee Related JP4778758B2 (ja) | 2004-09-23 | 2005-09-21 | タービンノズルのレール保持のための機械的解決法 |
Country Status (4)
Country | Link |
---|---|
US (1) | US7160078B2 (ja) |
JP (1) | JP4778758B2 (ja) |
CN (1) | CN1752416B (ja) |
DE (1) | DE102005045459B4 (ja) |
Families Citing this family (29)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20080050222A1 (en) * | 2006-08-23 | 2008-02-28 | General Electric Company | Singlet welded nozzle hybrid design for a turbine |
GB0619426D0 (en) * | 2006-10-03 | 2006-11-08 | Rolls Royce Plc | A vane arrangement |
US7824152B2 (en) * | 2007-05-09 | 2010-11-02 | Siemens Energy, Inc. | Multivane segment mounting arrangement for a gas turbine |
JP5134505B2 (ja) * | 2008-11-07 | 2013-01-30 | 三菱重工業株式会社 | 排気タービン過給機のノズル取付構造 |
US8684683B2 (en) | 2010-11-30 | 2014-04-01 | General Electric Company | Gas turbine nozzle attachment scheme and removal/installation method |
FR2981980B1 (fr) * | 2011-10-26 | 2016-01-22 | Snecma | Procede de montage d'un aubage fixe d'une turbomachine, carter et turbomachine comportant au moins un aubage fixe monte sur ce carter |
US9011079B2 (en) | 2012-01-09 | 2015-04-21 | General Electric Company | Turbine nozzle compartmentalized cooling system |
US8864445B2 (en) | 2012-01-09 | 2014-10-21 | General Electric Company | Turbine nozzle assembly methods |
US9133724B2 (en) | 2012-01-09 | 2015-09-15 | General Electric Company | Turbomachine component including a cover plate |
US8944751B2 (en) | 2012-01-09 | 2015-02-03 | General Electric Company | Turbine nozzle cooling assembly |
US9039350B2 (en) | 2012-01-09 | 2015-05-26 | General Electric Company | Impingement cooling system for use with contoured surfaces |
US9011078B2 (en) | 2012-01-09 | 2015-04-21 | General Electric Company | Turbine vane seal carrier with slots for cooling and assembly |
JP5675674B2 (ja) * | 2012-02-29 | 2015-02-25 | 三菱重工業株式会社 | タービン動翼の抜け止め構造およびこれを備えた回転機械 |
CN102733868B (zh) * | 2012-07-06 | 2015-12-09 | 中国航空动力机械研究所 | 动力机械 |
ES2547340T3 (es) * | 2012-08-10 | 2015-10-05 | MTU Aero Engines AG | Grado de turbina de gas |
WO2014133938A1 (en) | 2013-02-26 | 2014-09-04 | United Technologies Corporation | Gas turbine engine stator vane platform reinforcement |
US9528392B2 (en) | 2013-05-10 | 2016-12-27 | General Electric Company | System for supporting a turbine nozzle |
CN106460560B (zh) * | 2014-06-12 | 2018-11-13 | 通用电气公司 | 护罩吊架组件 |
JP6314049B2 (ja) * | 2014-07-24 | 2018-04-18 | 三菱日立パワーシステムズ株式会社 | 回転機械の静止部材及びガスタービン |
EP3109520B1 (de) * | 2015-06-24 | 2020-05-06 | MTU Aero Engines GmbH | Dichtungsträger, leitschaufelkranz und strömungsmaschine |
KR101663306B1 (ko) * | 2015-10-02 | 2016-10-06 | 두산중공업 주식회사 | 가스터빈 디스크 |
DE102016202519A1 (de) * | 2016-02-18 | 2017-08-24 | MTU Aero Engines AG | Leitschaufelsegment für eine Strömungsmaschine |
US11428241B2 (en) | 2016-04-22 | 2022-08-30 | Raytheon Technologies Corporation | System for an improved stator assembly |
DE102016115610A1 (de) * | 2016-08-23 | 2018-03-01 | Rolls-Royce Deutschland Ltd & Co Kg | Gasturbine und Verfahren zum Aufhängen eines Turbinen-Leitschaufelsegments einer Gasturbine |
US20180328228A1 (en) * | 2017-05-12 | 2018-11-15 | United Technologies Corporation | Turbine vane with inner circumferential anti-rotation features |
KR101985109B1 (ko) * | 2017-11-21 | 2019-05-31 | 두산중공업 주식회사 | 1단 터빈 베인 지지 구조 및 이를 포함하는 가스터빈 |
US10968777B2 (en) * | 2019-04-24 | 2021-04-06 | Raytheon Technologies Corporation | Chordal seal |
IT201900014739A1 (it) | 2019-08-13 | 2021-02-13 | Ge Avio Srl | Elementi di trattenimento delle pale per turbomacchine. |
DE102020115106B4 (de) * | 2020-06-08 | 2022-08-25 | Man Energy Solutions Se | Turbinenleitapparat |
Family Cites Families (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1387866A (en) * | 1972-06-21 | 1975-03-19 | Rolls Royce | Aerofoil members for gas turbine engines |
US4720236A (en) * | 1984-12-21 | 1988-01-19 | United Technologies Corporation | Coolable stator assembly for a gas turbine engine |
US4815933A (en) * | 1987-11-13 | 1989-03-28 | The United States Of America As Represented By The Secretary Of The Air Force | Nozzle flange attachment and sealing arrangement |
US5149250A (en) * | 1991-02-28 | 1992-09-22 | General Electric Company | Gas turbine vane assembly seal and support system |
US5224822A (en) * | 1991-05-13 | 1993-07-06 | General Electric Company | Integral turbine nozzle support and discourager seal |
CA2070511C (en) * | 1991-07-22 | 2001-08-21 | Steven Milo Toborg | Turbine nozzle support |
US5839878A (en) * | 1996-09-30 | 1998-11-24 | United Technologies Corporation | Gas turbine stator vane |
US6609885B2 (en) * | 2001-12-28 | 2003-08-26 | General Electric Company | Supplemental seal for the chordal hinge seal in a gas turbine |
DE10340825A1 (de) * | 2003-09-04 | 2005-03-31 | Rolls-Royce Deutschland Ltd & Co Kg | Gasturbine mit Laufspaltkontrolle |
US7094025B2 (en) * | 2003-11-20 | 2006-08-22 | General Electric Company | Apparatus and methods for removing and installing a selected nozzle segment of a gas turbine in an axial direction |
US7094026B2 (en) * | 2004-04-29 | 2006-08-22 | General Electric Company | System for sealing an inner retainer segment and support ring in a gas turbine and methods therefor |
-
2004
- 2004-09-23 US US10/947,450 patent/US7160078B2/en active Active
-
2005
- 2005-09-21 JP JP2005273095A patent/JP4778758B2/ja not_active Expired - Fee Related
- 2005-09-22 DE DE102005045459.3A patent/DE102005045459B4/de not_active Expired - Fee Related
- 2005-09-23 CN CN200510106321.0A patent/CN1752416B/zh not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
DE102005045459B4 (de) | 2016-06-09 |
DE102005045459A1 (de) | 2006-04-06 |
CN1752416B (zh) | 2011-10-05 |
JP2006097681A (ja) | 2006-04-13 |
US20060062673A1 (en) | 2006-03-23 |
CN1752416A (zh) | 2006-03-29 |
US7160078B2 (en) | 2007-01-09 |
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