JP5364609B2 - タービン・カバープレート・システム - Google Patents
タービン・カバープレート・システム Download PDFInfo
- Publication number
- JP5364609B2 JP5364609B2 JP2010020800A JP2010020800A JP5364609B2 JP 5364609 B2 JP5364609 B2 JP 5364609B2 JP 2010020800 A JP2010020800 A JP 2010020800A JP 2010020800 A JP2010020800 A JP 2010020800A JP 5364609 B2 JP5364609 B2 JP 5364609B2
- Authority
- JP
- Japan
- Prior art keywords
- cover plate
- wheel
- blade
- sealing surface
- rotor
- 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
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
- F01D5/30—Fixing blades to rotors; Blade roots ; Blade spacers
- F01D5/3007—Fixing blades to rotors; Blade roots ; Blade spacers of axial insertion type
- F01D5/3015—Fixing blades to rotors; Blade roots ; Blade spacers of axial insertion type with side plates
-
- 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
- F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
- F01D11/005—Sealing means between non relatively rotating elements
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2240/00—Components
- F05D2240/55—Seals
-
- 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
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Description
Claims (10)
- ロータ・ホイール(34)のホイール・ポスト(42)内の複数のブレード保持スロット(38)を軸方向に覆うように構成されたカバープレート(44)を備え、
前記カバープレート(44)は、
ロータ・ホイール(34)にカバープレート(44)を半径方向に固定するために相補的な溝(56)に結合するように構成されたタブ(54)と、
ロータ・ホイール(34)の対応するアパーチャと位置が合うように構成されたアパーチャ(62)であって、ロータ・ホイール(34)にカバープレート(44)を軸方向に固定するように構成される留め具(64)を受け取るためのアパーチャ(62)と、
前記ホイール・ポスト(42)に対し配置されるように構成されたシール面(80)と、
前記シール面(80)上に配置され、前記カバープレート(44)の周縁部を取り囲み、前記ホイール・ポスト(42)と整合して前記複数のブレード保持スロット(38)の少なくとも1つを完全に取り囲むように構成された隆起したシール部分(82)と、
前記ホイール・ポスト(42)から延びるブレード(32)の相補的な溝(76)内にカバープレート(44)を軸方向に保持するように構成された突出物(78)と、
を備えるシステム。 - アパーチャ(62)は、カバープレート(44)の周辺フランジ(60)上に配置され、周辺フランジ(60)は、ロータ・ホイール(34)の対応するフランジ(58)を覆うように構成される請求項1に記載のシステム。
- タブ(54)は、ホイール・ポスト(42)に隣接するように構成されたカバープレート(44)のシール面(80)から延びる請求項1または2に記載のシステム。
- カバープレート(44)は、シール面(80)に対向する表面(70)上に配置された1つまたは複数のリブ(66、68)であって、ロータ・ホイール(34)の動作中にロータ・ホイール(34)の方にカバープレート(44)を向けるように構成された1つまたは複数のリブ(66、68)を備える請求項3に記載のシステム。
- カバープレート(44)は、非一体型の留め具(64)を用いてロータ・ホイール(34)に取り付けられるように構成される請求項1乃至4のいずれかに記載のシステム。
- ガス・タービン・エンジン(12)、圧縮機(18)、ガス・タービン(22)、燃焼器(29)、またはそれらの組み合わせを備える請求項1乃至4のいずれかに記載のシステム。
- ロータ・ホイール(34)のホイール・ポスト(42)内の複数のブレード保持スロット(38)を軸方向に覆うように構成されたカバープレート(44)を備え、
前記カバープレート(44)は、
前記ホイール・ポスト(42)に対し配置されるように構成されたシール面(80)と、前記シール面(80)上に配置され、前記カバープレート(44)の周縁部を取り囲み、ホイール・ポスト(42)と整合して少なくとも1つのブレード保持スロット(38)を完全に取り囲むように構成された隆起したシール部分(82)と、
ホイール・ポスト(42)と接触するシール面(80)の面積を減らすようにシール面(80)内に配置された少なくとも1つの凹部(84)と、を備えるシステム。 - 前記カバープレート(44)は、前記シール面(80)内に配置された複数の凹部(84)を備え、各凹部(84)が前記複数のブレード保持スロット(38)の1つに重なるように構成される請求項7に記載のシステム。
- 前記少なくとも1つの凹部(84)と支持体バー(88)によって分離された第2の凹部(86)を備え、前記少なくとも1つの凹部(84)と第2の凹部(86)とはそれぞれ、複数のブレード保持スロット(38)の別個のブレード保持スロット(38)と位置が合うように構成され、
前記隆起したシール部分(82)は、前記少なくとも1つの凹部(84)と前記第2の凹部(86)とを取り囲むように構成されており、前記支持体バー(88)は前記隆起したシール部分(82)に対して引っ込んでいる請求項8に記載のシステム。 - 隆起したシール部分(82)は、少なくとも2つのブレード保持スロット(38)を取り囲むように構成される請求項7乃至9のいずれかに記載のシステム。
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US12/366,486 US8206119B2 (en) | 2009-02-05 | 2009-02-05 | Turbine coverplate systems |
US12/366,486 | 2009-02-05 |
Publications (3)
Publication Number | Publication Date |
---|---|
JP2010180879A JP2010180879A (ja) | 2010-08-19 |
JP2010180879A5 JP2010180879A5 (ja) | 2012-08-30 |
JP5364609B2 true JP5364609B2 (ja) | 2013-12-11 |
Family
ID=42232717
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP2010020800A Expired - Fee Related JP5364609B2 (ja) | 2009-02-05 | 2010-02-02 | タービン・カバープレート・システム |
Country Status (4)
Country | Link |
---|---|
US (1) | US8206119B2 (ja) |
EP (1) | EP2216505B1 (ja) |
JP (1) | JP5364609B2 (ja) |
CN (1) | CN101892868B (ja) |
Families Citing this family (43)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US8696320B2 (en) * | 2009-03-12 | 2014-04-15 | General Electric Company | Gas turbine having seal assembly with coverplate and seal |
US20100232939A1 (en) * | 2009-03-12 | 2010-09-16 | General Electric Company | Machine Seal Assembly |
US8845284B2 (en) | 2010-07-02 | 2014-09-30 | General Electric Company | Apparatus and system for sealing a turbine rotor |
US9109457B2 (en) * | 2010-09-03 | 2015-08-18 | Siemens Energy, Inc. | Axial locking seals for aft removable turbine blade |
US9133855B2 (en) * | 2010-11-15 | 2015-09-15 | Mtu Aero Engines Gmbh | Rotor for a turbo machine |
US8840375B2 (en) * | 2011-03-21 | 2014-09-23 | United Technologies Corporation | Component lock for a gas turbine engine |
US9127563B2 (en) | 2011-04-05 | 2015-09-08 | General Electric Company | Locking device arrangement for a rotating bladed stage |
US8740573B2 (en) * | 2011-04-26 | 2014-06-03 | General Electric Company | Adaptor assembly for coupling turbine blades to rotor disks |
US9217334B2 (en) * | 2011-10-26 | 2015-12-22 | General Electric Company | Turbine cover plate assembly |
US9080456B2 (en) | 2012-01-20 | 2015-07-14 | General Electric Company | Near flow path seal with axially flexible arms |
US8864453B2 (en) | 2012-01-20 | 2014-10-21 | General Electric Company | Near flow path seal for a turbomachine |
US9181810B2 (en) | 2012-04-16 | 2015-11-10 | General Electric Company | System and method for covering a blade mounting region of turbine blades |
US9366151B2 (en) * | 2012-05-07 | 2016-06-14 | General Electric Company | System and method for covering a blade mounting region of turbine blades |
US9249676B2 (en) * | 2012-06-05 | 2016-02-02 | United Technologies Corporation | Turbine rotor cover plate lock |
EP2964894B1 (en) | 2013-03-05 | 2019-04-10 | Rolls-Royce North American Technologies, Inc. | Turbine segmented cover plate retention method |
WO2014168862A1 (en) | 2013-04-12 | 2014-10-16 | United Technologies Corporation | Cover plate for a rotor assembly of a gas turbine engine |
US9605552B2 (en) | 2013-06-10 | 2017-03-28 | General Electric Company | Non-integral segmented angel-wing seal |
WO2015020931A2 (en) | 2013-08-09 | 2015-02-12 | United Technologies Corporation | Cover plate assembly for a gas turbine engine |
EP2860350A1 (de) * | 2013-10-10 | 2015-04-15 | Siemens Aktiengesellschaft | Turbinenschaufel sowie Gasturbine |
EP2860349A1 (de) * | 2013-10-10 | 2015-04-15 | Siemens Aktiengesellschaft | Turbinenschaufel sowie Gasturbine |
US9664118B2 (en) | 2013-10-24 | 2017-05-30 | General Electric Company | Method and system for controlling compressor forward leakage |
US10563525B2 (en) * | 2013-12-19 | 2020-02-18 | United Technologies Corporation | Blade feature to support segmented coverplate |
US10047633B2 (en) * | 2014-05-16 | 2018-08-14 | General Electric Company | Bearing housing |
EP3015655A1 (de) * | 2014-10-30 | 2016-05-04 | Siemens Aktiengesellschaft | Radscheibenanordnung mit Dichtblechen |
US10662793B2 (en) | 2014-12-01 | 2020-05-26 | General Electric Company | Turbine wheel cover-plate mounted gas turbine interstage seal |
EP3034795B1 (en) * | 2014-12-17 | 2019-02-27 | Ansaldo Energia Switzerland AG | Lock plate with radial grooves |
US20160230579A1 (en) * | 2015-02-06 | 2016-08-11 | United Technologies Corporation | Rotor disk sealing and blade attachments system |
US9951632B2 (en) | 2015-07-23 | 2018-04-24 | Honeywell International Inc. | Hybrid bonded turbine rotors and methods for manufacturing the same |
US10030519B2 (en) | 2015-10-26 | 2018-07-24 | Rolls-Royce Corporation | System and method to retain a turbine cover plate between nested turbines with a tie bolt and spanner nut |
US10718220B2 (en) | 2015-10-26 | 2020-07-21 | Rolls-Royce Corporation | System and method to retain a turbine cover plate with a spanner nut |
GB2547906B (en) * | 2016-03-02 | 2019-07-03 | Rolls Royce Plc | A bladed rotor arrangement |
US10393135B2 (en) * | 2017-02-09 | 2019-08-27 | DOOSAN Heavy Industries Construction Co., LTD | Compressor blade locking mechanism in disk with axial groove |
KR20180114765A (ko) * | 2017-04-11 | 2018-10-19 | 두산중공업 주식회사 | 가스터빈 블레이드의 리테이너, 이를 이용한 터빈유닛 및 가스터빈 |
US10920598B2 (en) * | 2017-05-02 | 2021-02-16 | Rolls-Royce Corporation | Rotor assembly cover plate |
KR20190029963A (ko) * | 2017-09-13 | 2019-03-21 | 두산중공업 주식회사 | 터빈 블레이드의 냉각구조 및 이를 포함하는 터빈 및 가스터빈 |
JP7022623B2 (ja) * | 2018-03-12 | 2022-02-18 | 三菱重工業株式会社 | 動翼体、及び回転機械 |
EP3564489A1 (de) | 2018-05-03 | 2019-11-06 | Siemens Aktiengesellschaft | Rotor mit fliehkraft-optimierten kontaktflächen |
EP3788236B1 (de) * | 2018-08-02 | 2023-06-21 | Siemens Energy Global GmbH & Co. KG | Rotor mit zwischen zwei rotorscheiben angeordnetem rotorbauteil |
US10830080B2 (en) * | 2018-09-28 | 2020-11-10 | Raytheon Technologies Corporation | Halo seal separate scallop support |
US11021974B2 (en) | 2018-10-10 | 2021-06-01 | Rolls-Royce North American Technologies Inc. | Turbine wheel assembly with retainer rings for ceramic matrix composite material blades |
FR3108361B1 (fr) * | 2020-03-19 | 2023-05-12 | Safran Aircraft Engines | Roue de turbine pour une turbomachine d’aéronef |
KR102400013B1 (ko) | 2020-08-21 | 2022-05-18 | 두산에너빌리티 주식회사 | 터빈 블레이드의 씰 조립구조와 이를 포함하는 가스 터빈 및 터빈 블레이드의 씰 조립방법 |
US12018567B2 (en) * | 2022-05-31 | 2024-06-25 | Pratt & Whitney Canada Corp. | Joint between gas turbine engine components with bonded fastener(s) |
Family Cites Families (23)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3043562A (en) * | 1961-04-10 | 1962-07-10 | Gen Electric | Combination sealing and restraining member for long-shank turbo-machine buckets |
US3300179A (en) * | 1966-04-22 | 1967-01-24 | Gen Motors Corp | Blade stalk cover plate |
BE794573A (fr) * | 1972-02-02 | 1973-05-16 | Gen Electric | Dispositif de fixation d'aubes |
GB1479332A (en) * | 1974-11-06 | 1977-07-13 | Rolls Royce | Means for retaining blades to a disc or like structure |
JPS61205303A (ja) * | 1985-03-06 | 1986-09-11 | Mitsubishi Heavy Ind Ltd | タ−ビン動翼の軸方向翼止装置 |
US5030063A (en) * | 1990-02-08 | 1991-07-09 | General Motors Corporation | Turbomachine rotor |
FR2666623B1 (fr) * | 1990-09-11 | 1993-05-07 | Turbomeca | Roue de turbomachine a pales rapportees. |
US5277548A (en) * | 1991-12-31 | 1994-01-11 | United Technologies Corporation | Non-integral rotor blade platform |
US5257909A (en) * | 1992-08-17 | 1993-11-02 | General Electric Company | Dovetail sealing device for axial dovetail rotor blades |
JP3306998B2 (ja) * | 1993-06-10 | 2002-07-24 | 石川島播磨重工業株式会社 | タービンロータ |
US5388962A (en) * | 1993-10-15 | 1995-02-14 | General Electric Company | Turbine rotor disk post cooling system |
US5800124A (en) * | 1996-04-12 | 1998-09-01 | United Technologies Corporation | Cooled rotor assembly for a turbine engine |
JPH108906A (ja) * | 1996-06-25 | 1998-01-13 | Mitsubishi Heavy Ind Ltd | ガスエキスパンダ用ロータ |
EP1018594B1 (en) * | 1999-01-06 | 2006-12-27 | General Electric Company | Wheelspace windage cover plate for a turbine |
US6190131B1 (en) * | 1999-08-31 | 2001-02-20 | General Electric Co. | Non-integral balanced coverplate and coverplate centering slot for a turbine |
DE19950109A1 (de) * | 1999-10-18 | 2001-04-19 | Asea Brown Boveri | Rotor für eine Gasturbine |
FR2812906B1 (fr) * | 2000-08-10 | 2002-09-20 | Snecma Moteurs | Bague de retention axiale d'un flasque sur un disque |
JP3864157B2 (ja) * | 2003-12-05 | 2006-12-27 | 本田技研工業株式会社 | 軸流型タービンホイール |
JP4035140B2 (ja) * | 2005-07-22 | 2008-01-16 | 川崎重工業株式会社 | タービンロータのシールリング |
FR2900437B1 (fr) * | 2006-04-27 | 2008-07-25 | Snecma Sa | Systeme de retention des aubes dans un rotor |
US7500832B2 (en) * | 2006-07-06 | 2009-03-10 | Siemens Energy, Inc. | Turbine blade self locking seal plate system |
EP1944471B1 (de) * | 2007-01-09 | 2009-09-02 | Siemens Aktiengesellschaft | Axialer Rotorabschnitt für einen Rotor einer Turbine |
US8128371B2 (en) * | 2007-02-15 | 2012-03-06 | General Electric Company | Method and apparatus to facilitate increasing turbine rotor efficiency |
-
2009
- 2009-02-05 US US12/366,486 patent/US8206119B2/en not_active Expired - Fee Related
-
2010
- 2010-02-01 EP EP10152214.2A patent/EP2216505B1/en not_active Not-in-force
- 2010-02-02 JP JP2010020800A patent/JP5364609B2/ja not_active Expired - Fee Related
- 2010-02-04 CN CN201010118796.2A patent/CN101892868B/zh not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
EP2216505A2 (en) | 2010-08-11 |
CN101892868B (zh) | 2014-06-11 |
US8206119B2 (en) | 2012-06-26 |
EP2216505B1 (en) | 2017-08-16 |
EP2216505A3 (en) | 2014-04-09 |
US20100196164A1 (en) | 2010-08-05 |
CN101892868A (zh) | 2010-11-24 |
JP2010180879A (ja) | 2010-08-19 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
JP5364609B2 (ja) | タービン・カバープレート・システム | |
JP5491874B2 (ja) | ガスタービン中の2次空気流を低減する装置およびシステム | |
EP2612995B1 (en) | Turbine nozzle compartmentalized cooling system | |
US9181810B2 (en) | System and method for covering a blade mounting region of turbine blades | |
US8444387B2 (en) | Seal plates for directing airflow through a turbine section of an engine and turbine sections | |
JP6018367B2 (ja) | タービンシールシステム | |
KR101245094B1 (ko) | 터빈 디스크 및 가스 터빈 | |
US20120321437A1 (en) | Turbine seal system | |
JP2010159748A (ja) | 非一体形タービンブレードプラットフォーム及びそのシステム | |
US8235656B2 (en) | Catenary turbine seal systems | |
US9404376B2 (en) | Sealing component for reducing secondary airflow in a turbine system | |
US10662795B2 (en) | Rotary assembly for a turbomachine | |
JP5108152B2 (ja) | タービンディスク上にシールプレートを備えたガスタービン | |
EP2568202B1 (en) | Non-continuous ring seal | |
US20120156045A1 (en) | Methods, systems and apparatus relating to root and platform configurations for turbine rotor blades | |
KR102127429B1 (ko) | 터빈 로터 디스크와 인터스테이지 디스크 사이의 실링 구조 | |
KR102031935B1 (ko) | 씰플레이트, 이를 포함하는 터빈 및 가스터빈 | |
JPH0723524Y2 (ja) | 軸流タービン | |
US11821365B2 (en) | Inducer seal with integrated inducer slots | |
KR20170139648A (ko) | 냉각 핀들을 갖도록 제공되는 케이스를 구비하는 가스 터빈 기관 | |
US20200370442A1 (en) | Sealing device |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
A521 | Request for written amendment filed |
Free format text: JAPANESE INTERMEDIATE CODE: A523 Effective date: 20120717 |
|
A621 | Written request for application examination |
Free format text: JAPANESE INTERMEDIATE CODE: A621 Effective date: 20120717 |
|
TRDD | Decision of grant or rejection written | ||
A977 | Report on retrieval |
Free format text: JAPANESE INTERMEDIATE CODE: A971007 Effective date: 20130815 |
|
A01 | Written decision to grant a patent or to grant a registration (utility model) |
Free format text: JAPANESE INTERMEDIATE CODE: A01 Effective date: 20130820 |
|
A61 | First payment of annual fees (during grant procedure) |
Free format text: JAPANESE INTERMEDIATE CODE: A61 Effective date: 20130909 |
|
R150 | Certificate of patent or registration of utility model |
Ref document number: 5364609 Country of ref document: JP Free format text: JAPANESE INTERMEDIATE CODE: R150 Free format text: JAPANESE INTERMEDIATE CODE: R150 |
|
R250 | Receipt of annual fees |
Free format text: JAPANESE INTERMEDIATE CODE: R250 |
|
R250 | Receipt of annual fees |
Free format text: JAPANESE INTERMEDIATE CODE: R250 |
|
R250 | Receipt of annual fees |
Free format text: JAPANESE INTERMEDIATE CODE: R250 |
|
R250 | Receipt of annual fees |
Free format text: JAPANESE INTERMEDIATE CODE: R250 |
|
R250 | Receipt of annual fees |
Free format text: JAPANESE INTERMEDIATE CODE: R250 |
|
R250 | Receipt of annual fees |
Free format text: JAPANESE INTERMEDIATE CODE: R250 |
|
LAPS | Cancellation because of no payment of annual fees |