NO330389B1 - Holdesegment for virvelanordning - Google Patents

Holdesegment for virvelanordning Download PDF

Info

Publication number: NO330389B1
Authority: NO; Norway
Prior art keywords: vortex; holding segment; area; swirl; arc
Prior art date: 2000-05-20

Application number

NO20012450A

Other languages

English (en)

Norwegian (no)

Other versions

NO20012450D0 (no

NO20012450L (no

Inventor

David Bruce Patterson

Thomas Anthony Leen

Original Assignee

Gen Electric

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.)

2000-05-20

Filing date

2001-05-18

Publication date

2011-04-04

2001-05-18 Application filed by Gen Electric filed Critical Gen Electric

2001-05-18 Publication of NO20012450D0 publication Critical patent/NO20012450D0/no

2001-11-21 Publication of NO20012450L publication Critical patent/NO20012450L/no

2011-04-04 Publication of NO330389B1 publication Critical patent/NO330389B1/no

Links

238000003466 welding Methods 0.000 claims description 8
230000035515 penetration Effects 0.000 claims description 3
239000000446 fuel Substances 0.000 description 23
230000000712 assembly Effects 0.000 description 8
238000000429 assembly Methods 0.000 description 8
238000011144 upstream manufacturing Methods 0.000 description 8
238000002485 combustion reaction Methods 0.000 description 6
239000007789 gas Substances 0.000 description 5
PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 4
239000000203 mixture Substances 0.000 description 4
229910045601 alloy Inorganic materials 0.000 description 3
239000000956 alloy Substances 0.000 description 3
239000000463 material Substances 0.000 description 3
238000005452 bending Methods 0.000 description 2
238000005336 cracking Methods 0.000 description 2
229910052759 nickel Inorganic materials 0.000 description 2
238000006243 chemical reaction Methods 0.000 description 1
229910017052 cobalt Inorganic materials 0.000 description 1
239000010941 cobalt Substances 0.000 description 1
GUTLYIVDDKVIGB-UHFFFAOYSA-N cobalt atom Chemical compound [Co] GUTLYIVDDKVIGB-UHFFFAOYSA-N 0.000 description 1
239000000567 combustion gas Substances 0.000 description 1
230000002950 deficient Effects 0.000 description 1
230000005284 excitation Effects 0.000 description 1
229910000856 hastalloy Inorganic materials 0.000 description 1
239000002184 metal Substances 0.000 description 1
229910052751 metal Inorganic materials 0.000 description 1
230000004048 modification Effects 0.000 description 1
238000012986 modification Methods 0.000 description 1
230000008092 positive effect Effects 0.000 description 1
238000002360 preparation method Methods 0.000 description 1
239000007858 starting material Substances 0.000 description 1

Classifications

- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
- F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
- F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
- F23R3/04—Air inlet arrangements
- F23R3/10—Air inlet arrangements for primary air
- F23R3/12—Air inlet arrangements for primary air inducing a vortex
- F23R3/14—Air inlet arrangements for primary air inducing a vortex by using swirl vanes
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23C—METHODS OR APPARATUS FOR COMBUSTION USING FLUID FUEL OR SOLID FUEL SUSPENDED IN A CARRIER GAS OR AIR
- F23C7/00—Combustion apparatus characterised by arrangements for air supply
- F23C7/002—Combustion apparatus characterised by arrangements for air supply the air being submitted to a rotary or spinning motion
- F23C7/004—Combustion apparatus characterised by arrangements for air supply the air being submitted to a rotary or spinning motion using vanes
- 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)
Chemical & Material Sciences (AREA)
Combustion & Propulsion (AREA)
Mechanical Engineering (AREA)
General Engineering & Computer Science (AREA)
Turbine Rotor Nozzle Sealing (AREA)
Devices Affording Protection Of Roads Or Walls For Sound Insulation (AREA)
Rolling Contact Bearings (AREA)
Manipulator (AREA)
Load-Engaging Elements For Cranes (AREA)

NO20012450A 2000-05-20 2001-05-18 Holdesegment for virvelanordning NO330389B1 (no)

Applications Claiming Priority (1)

Application Number	Priority Date	Filing Date	Title
US09/575,415 US6427435B1 (en)	2000-05-20	2000-05-20	Retainer segment for swirler assembly

Publications (3)

Publication Number	Publication Date
NO20012450D0 NO20012450D0 (no)	2001-05-18
NO20012450L NO20012450L (no)	2001-11-21
NO330389B1 true NO330389B1 (no)	2011-04-04

Family

ID=24300231

Family Applications (1)

Application Number	Title	Priority Date	Filing Date
NO20012450A NO330389B1 (no)	2000-05-20	2001-05-18	Holdesegment for virvelanordning

Country Status (8)

Country	Link
US (1)	US6427435B1 (ja)
EP (1)	EP1158246B1 (ja)
JP (1)	JP4753491B2 (ja)
AU (1)	AU782341B2 (ja)
BR (1)	BR0102059B1 (ja)
DE (1)	DE60110309T2 (ja)
NO (1)	NO330389B1 (ja)
SG (1)	SG94817A1 (ja)

Families Citing this family (33)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
FR2827367B1 (fr) *	2001-07-16	2003-10-17	Snecma Moteurs	Systeme d'injection aeromecanique a vrille primaire anti-retour
US6725667B2 (en) *	2002-08-22	2004-04-27	General Electric Company	Combustor dome for gas turbine engine
US6862889B2 (en) *	2002-12-03	2005-03-08	General Electric Company	Method and apparatus to decrease combustor emissions
US6976363B2 (en) *	2003-08-11	2005-12-20	General Electric Company	Combustor dome assembly of a gas turbine engine having a contoured swirler
US7062920B2 (en) *	2003-08-11	2006-06-20	General Electric Company	Combustor dome assembly of a gas turbine engine having a free floating swirler
US7121095B2 (en) *	2003-08-11	2006-10-17	General Electric Company	Combustor dome assembly of a gas turbine engine having improved deflector plates
US7104066B2 (en) *	2003-08-19	2006-09-12	General Electric Company	Combuster swirler assembly
JP2005076982A (ja) *	2003-08-29	2005-03-24	Mitsubishi Heavy Ind Ltd	ガスタービン燃焼器
US7013649B2 (en) *	2004-05-25	2006-03-21	General Electric Company	Gas turbine engine combustor mixer
US6993916B2 (en) *	2004-06-08	2006-02-07	General Electric Company	Burner tube and method for mixing air and gas in a gas turbine engine
US7140189B2 (en) *	2004-08-24	2006-11-28	Pratt & Whitney Canada Corp.	Gas turbine floating collar
US7134286B2 (en) *	2004-08-24	2006-11-14	Pratt & Whitney Canada Corp.	Gas turbine floating collar arrangement
US7316117B2 (en) *	2005-02-04	2008-01-08	Siemens Power Generation, Inc.	Can-annular turbine combustors comprising swirler assembly and base plate arrangements, and combinations
US7581402B2 (en) *	2005-02-08	2009-09-01	Siemens Energy, Inc.	Turbine engine combustor with bolted swirlers
DE102005022772A1 (de) *	2005-05-12	2007-01-11	Universität Karlsruhe	Brenner mit Teilvormischung und -vorverdampfung des flüssigen Brennstoffs
US7513098B2 (en)	2005-06-29	2009-04-07	Siemens Energy, Inc.	Swirler assembly and combinations of same in gas turbine engine combustors
US7415826B2 (en) *	2005-07-25	2008-08-26	General Electric Company	Free floating mixer assembly for combustor of a gas turbine engine
US20070119052A1 (en) *	2005-11-28	2007-05-31	General Electric Company	Combustor dome repair method
FR2899314B1 (fr)	2006-03-30	2008-05-09	Snecma Sa	Dispositif d'injection d'un melange d'air et de carburant, chambre de combustion et turbomachine munies d'un tel dispositif
FR2903170B1 (fr)	2006-06-29	2011-12-23	Snecma	Dispositif d'injection d'un melange d'air et de carburant, chambre de combustion et turbomachine munies d'un tel dispositif
FR2903169B1 (fr) *	2006-06-29	2011-11-11	Snecma	Dispositif d'injection d'un melange d'air et de carburant, chambre de combustion et turbomachine munies d'un tel dispositif
US7765809B2 (en) *	2006-11-10	2010-08-03	General Electric Company	Combustor dome and methods of assembling such
FR2908867B1 (fr) *	2006-11-16	2012-06-15	Snecma	Dispositif d'injection d'un melange d'air et de carburant, chambre de combustion et turbomachine munies d'un tel dispositif
US7926280B2 (en) *	2007-05-16	2011-04-19	Pratt & Whitney Canada Corp.	Interface between a combustor and fuel nozzle
EP2078898A1 (de) *	2008-01-11	2009-07-15	Siemens Aktiengesellschaft	Brenner und Verfahren zur Verringerung von selbstinduzierten Flammenschwingungen
GB2470742B (en) *	2009-06-03	2011-04-20	Rolls Royce Plc	Fuel injector for a gas turbine engine
US8689563B2 (en) *	2009-07-13	2014-04-08	United Technologies Corporation	Fuel nozzle guide plate mistake proofing
US8272224B2 (en) *	2009-11-02	2012-09-25	General Electric Company	Apparatus and methods for fuel nozzle frequency adjustment
JP5755216B2 (ja) *	2010-02-23	2015-07-29	旭有機材工業株式会社	インライン型流体混合装置
US8726669B2 (en) *	2011-06-30	2014-05-20	General Electric Company	Combustor dome with combined deflector/mixer retainer
GB201506017D0 (en)	2015-04-09	2015-05-27	Rolls Royce Plc	Fuel injector system
FR3042588B1 (fr) *	2015-10-16	2017-11-10	Snecma	Dispositif d'injection pour une chambre de combustion d'une turbomachine
US10253976B2 (en)	2017-04-24	2019-04-09	United Technologies Corporation	Fuel swirler with anti-rotation features

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
US3853273A (en) *	1973-10-01	1974-12-10	Gen Electric	Axial swirler central injection carburetor
US4454711A (en) *	1981-10-29	1984-06-19	Avco Corporation	Self-aligning fuel nozzle assembly
US4584834A (en) *	1982-07-06	1986-04-29	General Electric Company	Gas turbine engine carburetor
US4870818A (en) *	1986-04-18	1989-10-03	United Technologies Corporation	Fuel nozzle guide structure and retainer for a gas turbine engine
US5117637A (en) *	1990-08-02	1992-06-02	General Electric Company	Combustor dome assembly
JPH04303134A (ja) *	1991-03-29	1992-10-27	Honda Motor Co Ltd	ガスタービンエンジン
US5237820A (en) *	1992-01-02	1993-08-24	General Electric Company	Integral combustor cowl plate/ferrule retainer
US5399053A (en) *	1993-04-27	1995-03-21	Avibank Mfg., Inc.	Quick action panel fastener assembly including a cup enclosed retainer receiving a bolt therein
US5463864A (en) *	1993-12-27	1995-11-07	United Technologies Corporation	Fuel nozzle guide for a gas turbine engine combustor
FR2753779B1 (fr) *	1996-09-26	1998-10-16		Systeme d'injection aerodynamique d'un melange air carburant
US6550251B1 (en) *	1997-12-18	2003-04-22	General Electric Company	Venturiless swirl cup

2000
- 2000-05-20 US US09/575,415 patent/US6427435B1/en not_active Expired - Lifetime
2001
- 2001-05-11 DE DE60110309T patent/DE60110309T2/de not_active Expired - Lifetime
- 2001-05-11 EP EP01304218A patent/EP1158246B1/en not_active Expired - Lifetime
- 2001-05-14 SG SG200102870A patent/SG94817A1/en unknown
- 2001-05-18 AU AU46053/01A patent/AU782341B2/en not_active Ceased
- 2001-05-18 NO NO20012450A patent/NO330389B1/no not_active IP Right Cessation
- 2001-05-18 JP JP2001148555A patent/JP4753491B2/ja not_active Expired - Fee Related
- 2001-05-21 BR BRPI0102059-5A patent/BR0102059B1/pt not_active IP Right Cessation

Also Published As

Publication number	Publication date
BR0102059B1 (pt)	2009-05-05
BR0102059A (pt)	2001-12-18
AU782341B2 (en)	2005-07-21
EP1158246B1 (en)	2005-04-27
SG94817A1 (en)	2003-03-18
EP1158246A2 (en)	2001-11-28
JP4753491B2 (ja)	2011-08-24
DE60110309D1 (de)	2005-06-02
NO20012450D0 (no)	2001-05-18
NO20012450L (no)	2001-11-21
EP1158246A3 (en)	2002-01-09
AU4605301A (en)	2001-11-22
US6427435B1 (en)	2002-08-06
JP2002071134A (ja)	2002-03-08
DE60110309T2 (de)	2006-02-16

Legal Events

Date	Code	Title	Description
2017-12-27	MM1K	Lapsed by not paying the annual fees

Publication	Publication Date	Title
NO330389B1 (no)	2011-04-04	Holdesegment for virvelanordning
US6314739B1 (en)	2001-11-13	Brazeless combustor dome assembly
RU2275554C2 (ru)	2006-04-27	Переходный элемент для некольцевых камер сгорания газовой турбины
EP1508743B1 (en)	2015-03-04	Combuster swirler assembly
US8261554B2 (en)	2012-09-11	Fuel nozzle tip assembly
US5117637A (en)	1992-06-02	Combustor dome assembly
EP1507121B1 (en)	2016-09-14	Combustor dome assembly of a gas turbine engine having improved deflector plates
US6725667B2 (en)	2004-04-27	Combustor dome for gas turbine engine
EP3290805B1 (en)	2019-04-10	Fuel nozzle assembly with resonator
EP2657608B1 (en)	2015-12-16	A Combustor
JP2000130758A (ja)	2000-05-12	遷移多穴燃焼器ライナ
CN102678335A (zh)	2012-09-19	紊流化后端衬套组件及冷却方法
JPH0776619B2 (ja)	1995-08-16	燃料噴射ノズル支持体
JP5149596B2 (ja)	2013-02-20	燃焼器ドームミキサー保持手段
EP3475614B1 (en)	2023-08-02	Combustor assembly for a turbine engine
JP3604143B2 (ja)	2004-12-22	ガスタービンエンジン燃焼器に用いられるイグナイタプラグガイド
US6467272B1 (en)	2002-10-22	Means for wear reduction in a gas turbine combustor
US20100024425A1 (en)	2010-02-04	Turbine engine fuel nozzle
US20120167578A1 (en)	2012-07-05	Flame holding inhibitor for a lean pre-nozzle fuel injection diffuser and related method
JP4327324B2 (ja)	2009-09-09	ガスタービン燃焼器
US20230313992A1 (en)	2023-10-05	Liner assembly for a combustor
US20230212984A1 (en)	2023-07-06	Engine fuel nozzle and swirler
JP2012117808A (ja)	2012-06-21	ガス専用インサートを備えた燃料ノズル
AU2002247476A1 (en)	2003-01-08	Means for wear reduction in a gas turbine combustor