JP4027430B2 - タービン翼並びにガスタービン設備におけるその使用 - Google Patents

タービン翼並びにガスタービン設備におけるその使用 Download PDF

Info

Publication number: JP4027430B2
Authority: JP; Japan
Prior art keywords: wall; turbine blade; cooling; heat transfer; cooling fluid
Prior art date: 1996-12-02
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

Application number

JP52504598A

Other languages

English (en)

Japanese (ja)

Other versions

JP2001505275A (ja

Inventor

ヘンドラー、ミヒアエル

ショイルレン、ミヒアエル

Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)

Siemens AG

Original Assignee

Siemens AG

Priority date (The priority date 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 date listed.)

1996-12-02

Filing date

1997-11-18

Publication date

2007-12-26

1997-11-18 Application filed by Siemens AG filed Critical Siemens AG

2001-04-17 Publication of JP2001505275A publication Critical patent/JP2001505275A/ja

2007-12-26 Application granted granted Critical

2007-12-26 Publication of JP4027430B2 publication Critical patent/JP4027430B2/ja

2017-11-18 Anticipated expiration legal-status Critical

Status Expired - Fee Related legal-status Critical Current

Links

238000001816 cooling Methods 0.000 claims description 94
239000012809 cooling fluid Substances 0.000 claims description 31
238000005266 casting Methods 0.000 claims description 5
238000005406 washing Methods 0.000 claims description 4
230000008878 coupling Effects 0.000 claims description 2
238000010168 coupling process Methods 0.000 claims description 2
238000005859 coupling reaction Methods 0.000 claims description 2
239000007789 gas Substances 0.000 description 37
230000001154 acute effect Effects 0.000 description 3
238000000034 method Methods 0.000 description 3
230000015572 biosynthetic process Effects 0.000 description 2
230000003628 erosive effect Effects 0.000 description 2
238000009434 installation Methods 0.000 description 2
230000000149 penetrating effect Effects 0.000 description 2
125000006850 spacer group Chemical group 0.000 description 2
XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 2
239000000112 cooling gas Substances 0.000 description 1
238000000926 separation method Methods 0.000 description 1
239000007787 solid Substances 0.000 description 1
238000011144 upstream manufacturing 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
- 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
- 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
- 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
- F05D2260/20—Heat transfer, e.g. cooling
- F05D2260/221—Improvement of heat transfer
- F05D2260/2212—Improvement of heat transfer by creating turbulence

Landscapes

Engineering & Computer Science (AREA)
Mechanical Engineering (AREA)
General Engineering & Computer Science (AREA)
Turbine Rotor Nozzle Sealing (AREA)

JP52504598A 1996-12-02 1997-11-18 タービン翼並びにガスタービン設備におけるその使用 Expired - Fee Related JP4027430B2 (ja)

Applications Claiming Priority (3)

Application Number	Priority Date	Filing Date	Title
DE19649924.0		1996-12-02
DE19649924		1996-12-02
PCT/DE1997/002702 WO1998025009A1 (fr)	1996-12-02	1997-11-18	Aube de turbine et son utilisation dans un systeme de turbine a gaz

Publications (2)

Publication Number	Publication Date
JP2001505275A JP2001505275A (ja)	2001-04-17
JP4027430B2 true JP4027430B2 (ja)	2007-12-26

Family

ID=7813384

Family Applications (1)

Application Number	Title	Priority Date	Filing Date
JP52504598A Expired - Fee Related JP4027430B2 (ja)	1996-12-02	1997-11-18	タービン翼並びにガスタービン設備におけるその使用

Country Status (4)

Country	Link
EP (1)	EP0954680B1 (fr)
JP (1)	JP4027430B2 (fr)
DE (1)	DE59706345D1 (fr)
WO (1)	WO1998025009A1 (fr)

Families Citing this family (13)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
US6126397A (en) *	1998-12-22	2000-10-03	United Technologies Corporation	Trailing edge cooling apparatus for a gas turbine airfoil
US6254334B1 (en) *	1999-10-05	2001-07-03	United Technologies Corporation	Method and apparatus for cooling a wall within a gas turbine engine
EP1136651A1 (fr)	2000-03-22	2001-09-26	Siemens Aktiengesellschaft	Système de refroidissement pour une aube de turbine à gaz
EP1188902A1 (fr)	2000-09-14	2002-03-20	Siemens Aktiengesellschaft	Paroi refroidie par jet
JP4586265B2 (ja) *	2000-12-07	2010-11-24	株式会社Ihi	タービン翼のトランスピレーション冷却伝熱促進構造
US6511293B2 (en)	2001-05-29	2003-01-28	Siemens Westinghouse Power Corporation	Closed loop steam cooled airfoil
US6896487B2 (en) *	2003-08-08	2005-05-24	United Technologies Corporation	Microcircuit airfoil mainbody
US7364405B2 (en) *	2005-11-23	2008-04-29	United Technologies Corporation	Microcircuit cooling for vanes
EP1930544A1 (fr) *	2006-10-30	2008-06-11	Siemens Aktiengesellschaft	Aube de turbine
US9638057B2 (en)	2013-03-14	2017-05-02	Rolls-Royce North American Technologies, Inc.	Augmented cooling system
US10683762B2 (en)	2016-07-12	2020-06-16	Rolls-Royce North American Technologies Inc.	Gas engine component with cooling passages in wall
EP3564484A1 (fr)	2018-05-04	2019-11-06	Siemens Aktiengesellschaft	Paroi de composant d'un composant à gaz chaud
CN109139128A (zh) *	2018-10-22	2019-01-04	中国船舶重工集团公司第七0三研究所	一种船用燃气轮机高压涡轮导叶冷却结构

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
DE3003347A1 (de) *	1979-12-20	1981-06-25	BBC AG Brown, Boveri & Cie., Baden, Aargau	Gekuehlte wand
US5405242A (en)	1990-07-09	1995-04-11	United Technologies Corporation	Cooled vane
US5690472A (en) *	1992-02-03	1997-11-25	General Electric Company	Internal cooling of turbine airfoil wall using mesh cooling hole arrangement
US5328331A (en) *	1993-06-28	1994-07-12	General Electric Company	Turbine airfoil with double shell outer wall
US5702232A (en) *	1994-12-13	1997-12-30	United Technologies Corporation	Cooled airfoils for a gas turbine engine

1997
- 1997-11-18 JP JP52504598A patent/JP4027430B2/ja not_active Expired - Fee Related
- 1997-11-18 EP EP97949947A patent/EP0954680B1/fr not_active Expired - Lifetime
- 1997-11-18 WO PCT/DE1997/002702 patent/WO1998025009A1/fr not_active Ceased
- 1997-11-18 DE DE59706345T patent/DE59706345D1/de not_active Expired - Lifetime

Also Published As

Publication number	Publication date
EP0954680A1 (fr)	1999-11-10
WO1998025009A1 (fr)	1998-06-11
DE59706345D1 (de)	2002-03-21
JP2001505275A (ja)	2001-04-17
EP0954680B1 (fr)	2002-02-06

Legal Events

Date	Code	Title	Description
2004-11-18	A621	Written request for application examination	Free format text: JAPANESE INTERMEDIATE CODE: A621 Effective date: 20041026
2007-04-24	A131	Notification of reasons for refusal	Free format text: JAPANESE INTERMEDIATE CODE: A131 Effective date: 20070424
2007-08-09	A521	Request for written amendment filed	Free format text: JAPANESE INTERMEDIATE CODE: A523 Effective date: 20070720
2007-09-04	TRDD	Decision of grant or rejection written
2007-09-11	A01	Written decision to grant a patent or to grant a registration (utility model)	Free format text: JAPANESE INTERMEDIATE CODE: A01 Effective date: 20070911
2007-10-18	A61	First payment of annual fees (during grant procedure)	Free format text: JAPANESE INTERMEDIATE CODE: A61 Effective date: 20071010
2007-10-19	FPAY	Renewal fee payment (event date is renewal date of database)	Free format text: PAYMENT UNTIL: 20101019 Year of fee payment: 3
2007-10-19	R150	Certificate of patent or registration of utility model	Free format text: JAPANESE INTERMEDIATE CODE: R150
2010-10-07	FPAY	Renewal fee payment (event date is renewal date of database)	Free format text: PAYMENT UNTIL: 20101019 Year of fee payment: 3
2010-10-12	FPAY	Renewal fee payment (event date is renewal date of database)	Free format text: PAYMENT UNTIL: 20111019 Year of fee payment: 4
2011-09-22	FPAY	Renewal fee payment (event date is renewal date of database)	Free format text: PAYMENT UNTIL: 20111019 Year of fee payment: 4
2011-09-27	FPAY	Renewal fee payment (event date is renewal date of database)	Free format text: PAYMENT UNTIL: 20121019 Year of fee payment: 5
2012-10-02	FPAY	Renewal fee payment (event date is renewal date of database)	Free format text: PAYMENT UNTIL: 20131019 Year of fee payment: 6
2013-10-01	R250	Receipt of annual fees	Free format text: JAPANESE INTERMEDIATE CODE: R250
2014-10-07	R250	Receipt of annual fees	Free format text: JAPANESE INTERMEDIATE CODE: R250
2015-10-06	R250	Receipt of annual fees	Free format text: JAPANESE INTERMEDIATE CODE: R250
2016-10-19	LAPS	Cancellation because of no payment of annual fees

Publication	Publication Date	Title
JP4027430B2 (ja)	2007-12-26	タービン翼並びにガスタービン設備におけるその使用
US6783323B2 (en)	2004-08-31	Gas turbine stationary blade
US5201847A (en)	1993-04-13	Shroud design
JP4553285B2 (ja)	2010-09-29	高圧及び低圧タービン複合式シュラウドのエンドレール冷却法
US7621718B1 (en)	2009-11-24	Turbine vane with leading edge fillet region impingement cooling
US6290462B1 (en)	2001-09-18	Gas turbine cooled blade
EP1407193B1 (fr)	2004-12-08	Segment pouvant etre refroidi pour turbomachine et turbine de combustion
US3781129A (en)	1973-12-25	Cooled airfoil
US5259730A (en)	1993-11-09	Impingement cooled airfoil with bonding foil insert
US4446693A (en)	1984-05-08	Wall structure for a combustion chamber
EP0789806B1 (fr)	1998-07-29	Pale de turbine a gaz avec plateforme refroidie
CN1987055B (zh)	2012-10-10	平衡冷却的涡轮机喷嘴
US8061979B1 (en)	2011-11-22	Turbine BOAS with edge cooling
US7740445B1 (en)	2010-06-22	Turbine blade with near wall cooling
US8052390B1 (en)	2011-11-08	Turbine airfoil with showerhead cooling
US8070442B1 (en)	2011-12-06	Turbine airfoil with near wall cooling
JP2003065539A (ja)	2003-03-05	高温ガス案内構造物用の断熱装置
KR920006617A (ko)	1992-04-27	가스 터어빈 베인 구조체의 차등적인 열팽창을 최소화시키기 위한 장치 및 방법
US6406254B1 (en)	2002-06-18	Cooling circuit for steam and air-cooled turbine nozzle stage
US6416275B1 (en)	2002-07-09	Recessed impingement insert metering plate for gas turbine nozzles
KR19990063133A (ko)	1999-07-26	터빈 블레이드
JP2001511864A (ja)	2001-08-14	タービン翼およびそのガスタービン設備への利用
US8777570B1 (en)	2014-07-15	Turbine vane with film cooling slots
GB2301405A (en)	1996-12-04	Gas turbine guide nozzle vane
CA2080183A1 (fr)	1993-05-05	Profil refroidi par impaction, comportant une piece rapportee en feuille mince