JP2010236548A - 熱絶縁を備えたタービン羽根組立体 - Google Patents
熱絶縁を備えたタービン羽根組立体 Download PDFInfo
- Publication number
- JP2010236548A JP2010236548A JP2010069259A JP2010069259A JP2010236548A JP 2010236548 A JP2010236548 A JP 2010236548A JP 2010069259 A JP2010069259 A JP 2010069259A JP 2010069259 A JP2010069259 A JP 2010069259A JP 2010236548 A JP2010236548 A JP 2010236548A
- Authority
- JP
- Japan
- Prior art keywords
- spar
- spacer
- blade assembly
- outer shell
- turbine
- 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
Links
- 238000009413 insulation Methods 0.000 title abstract 3
- 125000006850 spacer group Chemical group 0.000 claims abstract description 67
- 238000001816 cooling Methods 0.000 claims abstract description 33
- 239000000567 combustion gas Substances 0.000 description 12
- 239000007789 gas Substances 0.000 description 6
- 239000000463 material Substances 0.000 description 3
- 239000000758 substrate Substances 0.000 description 3
- 239000013585 weight reducing agent Substances 0.000 description 3
- 238000012423 maintenance Methods 0.000 description 2
- 238000006073 displacement reaction Methods 0.000 description 1
- 239000000446 fuel Substances 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000000737 periodic effect Effects 0.000 description 1
- 239000007787 solid Substances 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
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/12—Blades
- F01D5/14—Form or construction
- F01D5/147—Construction, i.e. structural features, e.g. of weight-saving hollow blades
-
- 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
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/12—Blades
- F01D5/14—Form or construction
- F01D5/18—Hollow blades, i.e. blades with cooling or heating channels or cavities; Heating, heat-insulating or cooling means on blades
- F01D5/187—Convection cooling
-
- 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
- Y10T29/49336—Blade making
- Y10T29/49339—Hollow blade
- Y10T29/49341—Hollow blade with cooling passage
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Architecture (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
【解決手段】複数の隆起したリブ(62)を持つスパー(60)と、前記スパーの周りに装着された、複数の突出部分(72)を持つスペーサ(70)と、前記スペーサの周りに装着された外殻(80)とを含む。前記スペーサ上の前記突出部分(72)は前記スパー上の前記隆起したリブ(62)を取り囲む。前記スペーサ上の前記突出部分は前記外殻の内面を前記スパーから離間させて、冷却空気の熱絶縁層が構成されるように作用する。
【選択図】図6
Description
30 静止羽根取付け部
34 ノズル羽根
36 静止羽根前縁
38 タービン外被
40 タービン羽根
42 前縁
43 キャップ部分
44 側縁
45 基板
46 後縁
47 基部部分
48 開口
50 回転部材
60 スパー
62 隆起したリブ
62a 第1の隆起したリブ
62b 第2の隆起したリブ
64 冷却孔
66 冷却通路
68 冷却通路
70 スペーサ
70a スペーサの第1の半部
70b スペーサの第2の半部
72 突出部分
74 冷却孔
76 スペーサの上縁
78 スペーサの下縁
80 外殻
80a 外殻の第1の半部
80b 外殻の第2の半部
82 外殻の上縁
84 外殻の下縁
86 孔
Claims (10)
- その外部側面に沿って延在する複数の隆起したリブを持つスパーと、
前記スパーの前記外部側面の周りに装着されたスペーサであって、前記スパーの前記複数の隆起したリブを取り囲む複数の突出部分を持つスペーサと、
前記スペーサの周りに装着された外殻と、
有するタービン用の羽根組立体。 - 前記スパーの頂部の上に装着されたキャップを更に有している、請求項1記載の羽根組立体。
- 前記外殻の上縁が前記キャップの下側に突合せ接触している、請求項2記載の羽根組立体。
- 前記羽根組立体は更に、タービンの回転シャフトに結合されるように構成された基部を有しており、該基部に前記スパーが装着されている、請求項1記載の羽根組立体。
- 前記基部は、前記スパーが通り抜ける開口を持つ基部カバーを持っており、また前記外殻の下縁が前記基部カバーの前記開口内に装着され且つ前記開口を通って延在している、請求項4記載の羽根組立体。
- 前記スペーサの前記突出部分の幅が前記スパーの前記隆起したリブの幅よりも大きい、請求項1記載の羽根組立体。
- 前記スペーサは確実に前記外殻の内面を前記スパーの外面から離間させている、請求項1記載の羽根組立体。
- 請求項7記載の羽根組立体。
前記スペーサは確実に前記外殻の内面を前記スパーの前記隆起したリブの外側端から離間させている、請求項7記載の羽根組立体。 - 前記スパーは、該スパーの高さに沿って延在する少なくとも1つの冷却空気通路と、前記少なくとも1つの冷却空気通路から、前記スパーの外部側面上に形成された流出冷却孔まで延在する少なくとも1つの流出冷却通路と、を含んでいる、請求項1記載の羽根組立体。
- 前記スペーサに複数のスペーサ開口が形成されていて、当該複数のスペーサ開口は、前記スパーの前記少なくとも1つの流出冷却通路を出て行く冷却空気が前記スペーサの当該前記スペーサ開口を通り抜けて前記外殻の内面に突き当たるように形成されている、請求項9記載の羽根組立体。。
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US12/413,813 US8206109B2 (en) | 2009-03-30 | 2009-03-30 | Turbine blade assemblies with thermal insulation |
US12/413,813 | 2009-03-30 |
Publications (2)
Publication Number | Publication Date |
---|---|
JP2010236548A true JP2010236548A (ja) | 2010-10-21 |
JP5475519B2 JP5475519B2 (ja) | 2014-04-16 |
Family
ID=42272733
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP2010069259A Expired - Fee Related JP5475519B2 (ja) | 2009-03-30 | 2010-03-25 | 熱絶縁を備えたタービン羽根組立体 |
Country Status (4)
Country | Link |
---|---|
US (1) | US8206109B2 (ja) |
EP (1) | EP2239417B1 (ja) |
JP (1) | JP5475519B2 (ja) |
CN (1) | CN101852098B (ja) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2014181715A (ja) * | 2013-03-20 | 2014-09-29 | General Electric Co <Ge> | タービン翼型アセンブリ |
Families Citing this family (19)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP2607624B1 (en) * | 2011-12-19 | 2014-12-17 | Siemens Aktiengesellschaft | Vane for a turbomachine |
CA2896543A1 (en) * | 2013-02-23 | 2014-09-25 | Rolls-Royce Corporation | Gas turbine engine component |
WO2014137470A1 (en) | 2013-03-05 | 2014-09-12 | Vandervaart Peter L | Gas turbine engine component arrangement |
WO2014163698A1 (en) | 2013-03-07 | 2014-10-09 | Vandervaart Peter L | Cooled gas turbine engine component |
JP2016538470A (ja) * | 2013-11-25 | 2016-12-08 | ゼネラル エレクトリック テクノロジー ゲゼルシャフト ミット ベシュレンクテル ハフツングGeneral Electric Technology GmbH | モジュール構造に基づくターボ機械用のブレードアセンブリ |
US10450872B2 (en) * | 2016-11-08 | 2019-10-22 | Rolls-Royce Corporation | Undercut on airfoil coversheet support member |
US10648341B2 (en) | 2016-11-15 | 2020-05-12 | Rolls-Royce Corporation | Airfoil leading edge impingement cooling |
US10465526B2 (en) | 2016-11-15 | 2019-11-05 | Rolls-Royce Corporation | Dual-wall airfoil with leading edge cooling slot |
US10494948B2 (en) * | 2017-05-09 | 2019-12-03 | General Electric Company | Impingement insert |
US20190017392A1 (en) * | 2017-07-13 | 2019-01-17 | General Electric Company | Turbomachine impingement cooling insert |
US10450873B2 (en) * | 2017-07-31 | 2019-10-22 | Rolls-Royce Corporation | Airfoil edge cooling channels |
US11008878B2 (en) | 2018-12-21 | 2021-05-18 | Rolls-Royce Plc | Turbine blade with ceramic matrix composite aerofoil and metallic root |
US10711621B1 (en) | 2019-02-01 | 2020-07-14 | Rolls-Royce Plc | Turbine vane assembly with ceramic matrix composite components and temperature management features |
US10767495B2 (en) | 2019-02-01 | 2020-09-08 | Rolls-Royce Plc | Turbine vane assembly with cooling feature |
US20200263557A1 (en) * | 2019-02-19 | 2020-08-20 | Rolls-Royce Plc | Turbine vane assembly with cooling feature |
US11149553B2 (en) | 2019-08-02 | 2021-10-19 | Rolls-Royce Plc | Ceramic matrix composite components with heat transfer augmentation features |
US11268392B2 (en) * | 2019-10-28 | 2022-03-08 | Rolls-Royce Plc | Turbine vane assembly incorporating ceramic matrix composite materials and cooling |
US11879354B2 (en) * | 2021-09-29 | 2024-01-23 | General Electric Company | Rotor blade with frangible spar for a gas turbine engine |
US11598215B1 (en) * | 2021-10-14 | 2023-03-07 | Rolls-Royce Corporation | Coolant transfer system and method for a dual-wall airfoil |
Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS5672201A (en) * | 1979-11-14 | 1981-06-16 | Hitachi Ltd | Cooling structure of gas turbine blade |
GB2172060A (en) * | 1985-03-09 | 1986-09-10 | Rolls Royce | Bladed rotor |
US4790721A (en) * | 1988-04-25 | 1988-12-13 | Rockwell International Corporation | Blade assembly |
JPH02140402A (ja) * | 1988-11-21 | 1990-05-30 | Toshiba Corp | ターボ機械の動翼構造 |
US6514046B1 (en) * | 2000-09-29 | 2003-02-04 | Siemens Westinghouse Power Corporation | Ceramic composite vane with metallic substructure |
JP2004036606A (ja) * | 2002-03-18 | 2004-02-05 | General Electric Co <Ge> | ハイブリッド高温物品及びその製法 |
Family Cites Families (11)
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DE3003347A1 (de) | 1979-12-20 | 1981-06-25 | BBC AG Brown, Boveri & Cie., Baden, Aargau | Gekuehlte wand |
US5820337A (en) | 1995-01-03 | 1998-10-13 | General Electric Company | Double wall turbine parts |
US6261054B1 (en) | 1999-01-25 | 2001-07-17 | General Electric Company | Coolable airfoil assembly |
EP1041247B1 (en) | 1999-04-01 | 2012-08-01 | General Electric Company | Gas turbine airfoil comprising an open cooling circuit |
KR20000071653A (ko) | 1999-04-15 | 2000-11-25 | 제이 엘. 차스킨, 버나드 스나이더, 아더엠. 킹 | 육상용 가스 터빈 및 가스 터빈의 하나의 단을 냉각시키는방법 |
US6454526B1 (en) | 2000-09-28 | 2002-09-24 | Siemens Westinghouse Power Corporation | Cooled turbine vane with endcaps |
US7758314B2 (en) * | 2003-03-12 | 2010-07-20 | Florida Turbine Technologies, Inc. | Tungsten shell for a spar and shell turbine vane |
US7080971B2 (en) | 2003-03-12 | 2006-07-25 | Florida Turbine Technologies, Inc. | Cooled turbine spar shell blade construction |
US7186084B2 (en) | 2003-11-19 | 2007-03-06 | General Electric Company | Hot gas path component with mesh and dimpled cooling |
EP1589192A1 (de) | 2004-04-20 | 2005-10-26 | Siemens Aktiengesellschaft | Turbinenschaufel mit einem Prallkühleinsatz |
US20060056968A1 (en) | 2004-09-15 | 2006-03-16 | General Electric Company | Apparatus and methods for cooling turbine bucket platforms |
-
2009
- 2009-03-30 US US12/413,813 patent/US8206109B2/en active Active
-
2010
- 2010-03-23 EP EP10157434A patent/EP2239417B1/en not_active Not-in-force
- 2010-03-25 JP JP2010069259A patent/JP5475519B2/ja not_active Expired - Fee Related
- 2010-03-30 CN CN201010156408.XA patent/CN101852098B/zh not_active Expired - Fee Related
Patent Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS5672201A (en) * | 1979-11-14 | 1981-06-16 | Hitachi Ltd | Cooling structure of gas turbine blade |
GB2172060A (en) * | 1985-03-09 | 1986-09-10 | Rolls Royce | Bladed rotor |
US4790721A (en) * | 1988-04-25 | 1988-12-13 | Rockwell International Corporation | Blade assembly |
JPH02140402A (ja) * | 1988-11-21 | 1990-05-30 | Toshiba Corp | ターボ機械の動翼構造 |
US6514046B1 (en) * | 2000-09-29 | 2003-02-04 | Siemens Westinghouse Power Corporation | Ceramic composite vane with metallic substructure |
JP2004036606A (ja) * | 2002-03-18 | 2004-02-05 | General Electric Co <Ge> | ハイブリッド高温物品及びその製法 |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2014181715A (ja) * | 2013-03-20 | 2014-09-29 | General Electric Co <Ge> | タービン翼型アセンブリ |
Also Published As
Publication number | Publication date |
---|---|
EP2239417B1 (en) | 2012-08-22 |
JP5475519B2 (ja) | 2014-04-16 |
EP2239417A1 (en) | 2010-10-13 |
CN101852098A (zh) | 2010-10-06 |
US8206109B2 (en) | 2012-06-26 |
US20100247329A1 (en) | 2010-09-30 |
CN101852098B (zh) | 2014-06-18 |
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