KR102384441B1 - 터빈 날개, 터빈 및 터빈 날개의 고유 진동수의 튜닝 방법 - Google Patents
터빈 날개, 터빈 및 터빈 날개의 고유 진동수의 튜닝 방법 Download PDFInfo
- Publication number
- KR102384441B1 KR102384441B1 KR1020207021990A KR20207021990A KR102384441B1 KR 102384441 B1 KR102384441 B1 KR 102384441B1 KR 1020207021990 A KR1020207021990 A KR 1020207021990A KR 20207021990 A KR20207021990 A KR 20207021990A KR 102384441 B1 KR102384441 B1 KR 102384441B1
- Authority
- KR
- South Korea
- Prior art keywords
- shank
- contour
- leading edge
- pressure surface
- trailing edge
- 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.)
- Active
Links
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
- F01D5/16—Form or construction for counteracting blade vibration
-
- 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
- F01D25/04—Antivibration arrangements
- F01D25/06—Antivibration arrangements for preventing blade vibration
-
- 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
- F01D25/04—Antivibration arrangements
-
- 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
- F01D5/02—Blade-carrying members, e.g. rotors
- F01D5/10—Anti- vibration means
-
- 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
- F05D2220/00—Application
- F05D2220/30—Application in turbines
-
- 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
- F05D2220/00—Application
- F05D2220/30—Application in turbines
- F05D2220/32—Application in turbines in gas turbines
-
- 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
- F05D2230/00—Manufacture
-
- 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
- F05D2260/00—Function
- F05D2260/96—Preventing, counteracting or reducing vibration or noise
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP2018060930A JP7064076B2 (ja) | 2018-03-27 | 2018-03-27 | タービン翼及びタービン並びにタービン翼の固有振動数のチューニング方法 |
| JPJP-P-2018-060930 | 2018-03-27 | ||
| PCT/JP2019/012080 WO2019188780A1 (ja) | 2018-03-27 | 2019-03-22 | タービン翼及びタービン並びにタービン翼の固有振動数のチューニング方法 |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| KR20200100184A KR20200100184A (ko) | 2020-08-25 |
| KR102384441B1 true KR102384441B1 (ko) | 2022-04-08 |
Family
ID=68059043
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| KR1020207021990A Active KR102384441B1 (ko) | 2018-03-27 | 2019-03-22 | 터빈 날개, 터빈 및 터빈 날개의 고유 진동수의 튜닝 방법 |
Country Status (6)
| Country | Link |
|---|---|
| US (1) | US11578603B2 (https=) |
| JP (1) | JP7064076B2 (https=) |
| KR (1) | KR102384441B1 (https=) |
| CN (1) | CN111655972B (https=) |
| DE (1) | DE112019000895B4 (https=) |
| WO (1) | WO2019188780A1 (https=) |
Families Citing this family (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP7360971B2 (ja) * | 2020-02-19 | 2023-10-13 | 三菱重工業株式会社 | タービン翼及びタービン |
| US11377972B1 (en) | 2021-02-25 | 2022-07-05 | Doosan Heavy Industries & Construction Co., Ltd. | Airfoil profile |
| US11306594B1 (en) | 2021-02-25 | 2022-04-19 | Doosan Heavy Industries & Construction Co., Ltd. | Airfoil profile |
| US11293286B1 (en) | 2021-02-25 | 2022-04-05 | Doosan Heavy Industries & Construction Co., Ltd. | Airfoil profile |
| US11255195B1 (en) | 2021-02-25 | 2022-02-22 | Doosan Heavy Industries & Construction Co., Ltd. | Airfoil profile |
| US11454126B1 (en) | 2021-08-24 | 2022-09-27 | Doosan Heavy Industries & Construction Co., Ltd. | Blade root shank profile |
| US12601268B2 (en) | 2023-08-25 | 2026-04-14 | Rtx Corporation | CMC vane with detuned platform |
Citations (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2007040296A (ja) * | 2005-08-03 | 2007-02-15 | United Technol Corp <Utc> | タービンブレード及びタービンブレードを提供する方法 |
| JP2007537385A (ja) * | 2004-05-14 | 2007-12-20 | プラット アンド ホイットニー カナダ コーポレイション | ガスタービンエンジン用ブレードの固有振動数のチューニング |
Family Cites Families (21)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS6397803A (ja) | 1986-10-13 | 1988-04-28 | Hitachi Ltd | タ−ビン翼の固定部構造 |
| US5435694A (en) * | 1993-11-19 | 1995-07-25 | General Electric Company | Stress relieving mount for an axial blade |
| JP2000248901A (ja) | 1999-02-26 | 2000-09-12 | Mitsubishi Heavy Ind Ltd | 中空ブレードおよびその固有振動数調整方法 |
| US6481972B2 (en) | 2000-12-22 | 2002-11-19 | General Electric Company | Turbine bucket natural frequency tuning rib |
| JP4781544B2 (ja) | 2001-02-26 | 2011-09-28 | 住友ゴム工業株式会社 | 農用車輪 |
| US6547645B2 (en) | 2001-08-27 | 2003-04-15 | General Electric Company | Method and backer inserts for blocking backwall water jet strikes |
| US6761536B1 (en) | 2003-01-31 | 2004-07-13 | Power Systems Mfg, Llc | Turbine blade platform trailing edge undercut |
| JP2005233141A (ja) | 2004-02-23 | 2005-09-02 | Mitsubishi Heavy Ind Ltd | 動翼およびその動翼を用いたガスタービン |
| US7467924B2 (en) * | 2005-08-16 | 2008-12-23 | United Technologies Corporation | Turbine blade including revised platform |
| US8007245B2 (en) * | 2007-11-29 | 2011-08-30 | General Electric Company | Shank shape for a turbine blade and turbine incorporating the same |
| US8435008B2 (en) | 2008-10-17 | 2013-05-07 | United Technologies Corporation | Turbine blade including mistake proof feature |
| KR101305575B1 (ko) * | 2010-01-20 | 2013-09-09 | 미츠비시 쥬고교 가부시키가이샤 | 터빈 동익 및 터보 기계 |
| US20120051930A1 (en) | 2010-08-31 | 2012-03-01 | General Electric Company | Shrouded turbine blade with contoured platform and axial dovetail |
| RU2553049C2 (ru) | 2011-07-01 | 2015-06-10 | Альстом Текнолоджи Лтд | Лопатка ротора турбины, ротор турбины и турбина |
| JP5881369B2 (ja) * | 2011-10-27 | 2016-03-09 | 三菱重工業株式会社 | タービン動翼及びこれを備えたガスタービン |
| US9151167B2 (en) * | 2012-02-10 | 2015-10-06 | General Electric Company | Turbine assembly |
| US9359905B2 (en) | 2012-02-27 | 2016-06-07 | Solar Turbines Incorporated | Turbine engine rotor blade groove |
| US9249669B2 (en) * | 2012-04-05 | 2016-02-02 | General Electric Company | CMC blade with pressurized internal cavity for erosion control |
| US9151165B2 (en) * | 2012-10-22 | 2015-10-06 | United Technologies Corporation | Reversible blade damper |
| US10677073B2 (en) * | 2017-01-03 | 2020-06-09 | Raytheon Technologies Corporation | Blade platform with damper restraint |
| GB201704832D0 (en) * | 2017-02-20 | 2017-05-10 | Rolls Royce Plc | Fan |
-
2018
- 2018-03-27 JP JP2018060930A patent/JP7064076B2/ja active Active
-
2019
- 2019-03-22 WO PCT/JP2019/012080 patent/WO2019188780A1/ja not_active Ceased
- 2019-03-22 US US16/978,082 patent/US11578603B2/en active Active
- 2019-03-22 CN CN201980010834.1A patent/CN111655972B/zh active Active
- 2019-03-22 DE DE112019000895.1T patent/DE112019000895B4/de active Active
- 2019-03-22 KR KR1020207021990A patent/KR102384441B1/ko active Active
Patent Citations (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2007537385A (ja) * | 2004-05-14 | 2007-12-20 | プラット アンド ホイットニー カナダ コーポレイション | ガスタービンエンジン用ブレードの固有振動数のチューニング |
| JP2007040296A (ja) * | 2005-08-03 | 2007-02-15 | United Technol Corp <Utc> | タービンブレード及びタービンブレードを提供する方法 |
Also Published As
| Publication number | Publication date |
|---|---|
| JP2019173612A (ja) | 2019-10-10 |
| DE112019000895T5 (de) | 2020-10-29 |
| CN111655972B (zh) | 2022-09-13 |
| KR20200100184A (ko) | 2020-08-25 |
| JP7064076B2 (ja) | 2022-05-10 |
| CN111655972A (zh) | 2020-09-11 |
| WO2019188780A1 (ja) | 2019-10-03 |
| DE112019000895B4 (de) | 2023-06-29 |
| US20210095567A1 (en) | 2021-04-01 |
| US11578603B2 (en) | 2023-02-14 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| KR102384441B1 (ko) | 터빈 날개, 터빈 및 터빈 날개의 고유 진동수의 튜닝 방법 | |
| US11808175B2 (en) | Gas turbine engine airfoils having multimodal thickness distributions | |
| JP4125725B2 (ja) | ガスタービンエンジン用の中空ファンブレード | |
| US8425185B2 (en) | Transonic blade | |
| US10907648B2 (en) | Airfoil with maximum thickness distribution for robustness | |
| US8753087B2 (en) | Turbine rotor assembly and steam turbine | |
| JP2019173612A5 (https=) | ||
| JP2015183691A (ja) | ガスタービンブレード | |
| KR20170128128A (ko) | 냉매 통로의 턴 개구에 응력 저감용 구근식 돌출부를 갖춘 블레이드 | |
| JP4269723B2 (ja) | タービンノズル | |
| EP4116589B1 (en) | Diffuser pipe with curved cross-sectional shapes | |
| KR102712942B1 (ko) | 터빈 블레이드의 중심을 변위시키는 방법 및 시스템 | |
| JP4109261B2 (ja) | ガスタービンエンジン用の中空ファンブレード | |
| JP4102806B2 (ja) | ガスタービンエンジン用の中空ファンブレード | |
| US9739159B2 (en) | Method and system for relieving turbine rotor blade dovetail stress | |
| US10427213B2 (en) | Turbine blade with sectioned pins and method of making same | |
| EP3441566A1 (en) | Airfoil with maximum thickness distribution for robustness | |
| CN117043447A (zh) | 用于飞行器涡轮发动机的定子环以及安装有这种定子环的飞行器涡轮发动机 | |
| JP7219829B2 (ja) | モーダル周波数応答の調整を行うタービン翼形部 | |
| CN115135853B (zh) | 涡轮叶片以及涡轮 | |
| JP7297132B1 (ja) | タービン静翼及びガスタービン | |
| KR102269713B1 (ko) | 터빈 날개, 터빈 및 터빈 날개의 냉각 방법 | |
| EP4112884B1 (en) | Blade for a turbomachine, blade assembly, and turbine | |
| KR101828470B1 (ko) | 가스터빈 로터 디스크 | |
| US20200291786A1 (en) | Aerofoil for gas turbine incorporating one or more encapsulated void |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| P11-X000 | Amendment of application requested |
St.27 status event code: A-2-2-P10-P11-nap-X000 |
|
| P13-X000 | Application amended |
St.27 status event code: A-2-2-P10-P13-nap-X000 |
|
| PA0105 | International application |
St.27 status event code: A-0-1-A10-A15-nap-PA0105 |
|
| PA0201 | Request for examination |
St.27 status event code: A-1-2-D10-D11-exm-PA0201 |
|
| PG1501 | Laying open of application |
St.27 status event code: A-1-1-Q10-Q12-nap-PG1501 |
|
| PN2301 | Change of applicant |
St.27 status event code: A-3-3-R10-R13-asn-PN2301 St.27 status event code: A-3-3-R10-R11-asn-PN2301 |
|
| E902 | Notification of reason for refusal | ||
| PE0902 | Notice of grounds for rejection |
St.27 status event code: A-1-2-D10-D21-exm-PE0902 |
|
| E13-X000 | Pre-grant limitation requested |
St.27 status event code: A-2-3-E10-E13-lim-X000 |
|
| P11-X000 | Amendment of application requested |
St.27 status event code: A-2-2-P10-P11-nap-X000 |
|
| P13-X000 | Application amended |
St.27 status event code: A-2-2-P10-P13-nap-X000 |
|
| E701 | Decision to grant or registration of patent right | ||
| PE0701 | Decision of registration |
St.27 status event code: A-1-2-D10-D22-exm-PE0701 |
|
| GRNT | Written decision to grant | ||
| PR0701 | Registration of establishment |
St.27 status event code: A-2-4-F10-F11-exm-PR0701 |
|
| PR1002 | Payment of registration fee |
St.27 status event code: A-2-2-U10-U12-oth-PR1002 Fee payment year number: 1 |
|
| PG1601 | Publication of registration |
St.27 status event code: A-4-4-Q10-Q13-nap-PG1601 |
|
| R18-X000 | Changes to party contact information recorded |
St.27 status event code: A-5-5-R10-R18-oth-X000 |
|
| PR1001 | Payment of annual fee |
St.27 status event code: A-4-4-U10-U11-oth-PR1001 Fee payment year number: 4 |
|
| PR1001 | Payment of annual fee |
St.27 status event code: A-4-4-U10-U11-oth-PR1001 Fee payment year number: 5 |
|
| U11 | Full renewal or maintenance fee paid |
Free format text: ST27 STATUS EVENT CODE: A-4-4-U10-U11-OTH-PR1001 (AS PROVIDED BY THE NATIONAL OFFICE) Year of fee payment: 5 |