JP2004197747A - ガスタービン燃焼器ドームの試験モデル及びその製作方法 - Google Patents

ガスタービン燃焼器ドームの試験モデル及びその製作方法 Download PDF

Info

Publication number
JP2004197747A
JP2004197747A JP2003420293A JP2003420293A JP2004197747A JP 2004197747 A JP2004197747 A JP 2004197747A JP 2003420293 A JP2003420293 A JP 2003420293A JP 2003420293 A JP2003420293 A JP 2003420293A JP 2004197747 A JP2004197747 A JP 2004197747A
Authority
JP
Japan
Prior art keywords
dome
support band
segments
band segments
test model
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.)
Ceased
Application number
JP2003420293A
Other languages
English (en)
Japanese (ja)
Other versions
JP2004197747A5 (https=
Inventor
Edward Lee Howard
エドワード・リー・ハワード
Farmer Gilbert
ギルバート・ファーマー
James Hollice Poynter
ジェームズ・ホライス・ポインター
Ronald Lee Sheranko
ロナルド・リー・シェランコ
John Robert Staker
ジョン・ロバート・ステイカー
Thomas Carl Mills
トマス・カール・ミルズ
Gregory Thomas Lucas
グレゴリー・トマス・ルーカス
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.)
General Electric Co
Original Assignee
General Electric Co
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.)
Filing date
Publication date
Application filed by General Electric Co filed Critical General Electric Co
Publication of JP2004197747A publication Critical patent/JP2004197747A/ja
Publication of JP2004197747A5 publication Critical patent/JP2004197747A5/ja
Ceased legal-status Critical Current

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/02Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/04Air inlet arrangements
    • F23R3/10Air inlet arrangements for primary air
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/002Wall structures
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R2900/00Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
    • F23R2900/00018Manufacturing combustion chamber liners or subparts
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/49316Impeller making
    • Y10T29/4932Turbomachine making
    • Y10T29/49323Assembling fluid flow directing devices, e.g., stators, diaphragms, nozzles
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/49346Rocket or jet device making
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/49826Assembling or joining
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/49826Assembling or joining
    • Y10T29/49895Associating parts by use of aligning means [e.g., use of a drift pin or a "fixture"]
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/49826Assembling or joining
    • Y10T29/49904Assembling a subassembly, then assembling with a second subassembly

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)
JP2003420293A 2002-12-19 2003-12-18 ガスタービン燃焼器ドームの試験モデル及びその製作方法 Ceased JP2004197747A (ja)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US10/248,128 US6931728B2 (en) 2002-12-19 2002-12-19 Test model for a gas turbine combustor dome and method of fabricating

Publications (2)

Publication Number Publication Date
JP2004197747A true JP2004197747A (ja) 2004-07-15
JP2004197747A5 JP2004197747A5 (https=) 2007-02-08

Family

ID=32392319

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2003420293A Ceased JP2004197747A (ja) 2002-12-19 2003-12-18 ガスタービン燃焼器ドームの試験モデル及びその製作方法

Country Status (3)

Country Link
US (1) US6931728B2 (https=)
EP (1) EP1431663A3 (https=)
JP (1) JP2004197747A (https=)

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20080164301A1 (en) * 2007-01-10 2008-07-10 General Electric Company High temperature laser welding
US20130174562A1 (en) * 2012-01-11 2013-07-11 Marcus Timothy Holcomb Gas turbine engine, combustor and dome panel
EP2964897B1 (en) 2013-03-07 2019-05-01 United Technologies Corporation Structural guide vane for gas turbine engine
US10520193B2 (en) * 2015-10-28 2019-12-31 General Electric Company Cooling patch for hot gas path components
US11614233B2 (en) 2020-08-31 2023-03-28 General Electric Company Impingement panel support structure and method of manufacture
US11994292B2 (en) 2020-08-31 2024-05-28 General Electric Company Impingement cooling apparatus for turbomachine
US11460191B2 (en) 2020-08-31 2022-10-04 General Electric Company Cooling insert for a turbomachine
US11994293B2 (en) 2020-08-31 2024-05-28 General Electric Company Impingement cooling apparatus support structure and method of manufacture
US11371702B2 (en) 2020-08-31 2022-06-28 General Electric Company Impingement panel for a turbomachine
US11255545B1 (en) 2020-10-26 2022-02-22 General Electric Company Integrated combustion nozzle having a unified head end
US11859819B2 (en) 2021-10-15 2024-01-02 General Electric Company Ceramic composite combustor dome and liners
US11767766B1 (en) 2022-07-29 2023-09-26 General Electric Company Turbomachine airfoil having impingement cooling passages

Family Cites Families (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB774594A (en) * 1954-05-26 1957-05-15 Nat Res Dev Method and apparatus for the simulation of combustion occurring in furnaces, gas turbines and the like
US4008568A (en) * 1976-03-01 1977-02-22 General Motors Corporation Combustor support
US4208774A (en) * 1978-11-27 1980-06-24 United Technologies Corporation Process for welding flanges to a cylindrical engine casing having a plurality of spaced rails and ribs
US4232527A (en) * 1979-04-13 1980-11-11 General Motors Corporation Combustor liner joints
US4843825A (en) * 1988-05-16 1989-07-04 United Technologies Corporation Combustor dome heat shield
CA2070518C (en) * 1991-07-01 2001-10-02 Adrian Mark Ablett Combustor dome assembly
US6212870B1 (en) * 1998-09-22 2001-04-10 General Electric Company Self fixturing combustor dome assembly
US6314739B1 (en) * 2000-01-13 2001-11-13 General Electric Company Brazeless combustor dome assembly
US6453671B1 (en) 2000-01-13 2002-09-24 General Electric Company Combustor swirler assembly
US6735950B1 (en) * 2000-03-31 2004-05-18 General Electric Company Combustor dome plate and method of making the same
US6502400B1 (en) * 2000-05-20 2003-01-07 General Electric Company Combustor dome assembly and method of assembling the same
US6298667B1 (en) * 2000-06-22 2001-10-09 General Electric Company Modular combustor dome
US6442940B1 (en) * 2001-04-27 2002-09-03 General Electric Company Gas-turbine air-swirler attached to dome and combustor in single brazing operation
US6629415B2 (en) * 2001-10-27 2003-10-07 General Electric Co. Methods and apparatus for modeling gas turbine engine combustor liners

Also Published As

Publication number Publication date
US20040154152A1 (en) 2004-08-12
EP1431663A3 (en) 2006-10-18
EP1431663A2 (en) 2004-06-23
US6931728B2 (en) 2005-08-23

Similar Documents

Publication Publication Date Title
JP2004197747A (ja) ガスタービン燃焼器ドームの試験モデル及びその製作方法
US4096615A (en) Turbine rotor fabrication
US20100284817A1 (en) Method for producing a blisk or a bling, component produced therewith and turbine blade
US4464094A (en) Turbine engine component and method of making the same
US4538331A (en) Method of manufacturing an integral bladed turbine disk
US6545467B1 (en) Contoured surface eddy current inspection system
US20080029968A1 (en) Nested can brush seal
US7172389B2 (en) Method for making a repaired turbine engine stationary vane assembly and repaired assembly
JPH06235302A (ja) 中空羽根付モノブロックロータの製造方法及び中空羽根付モノブロックロータ
CN103747915B (zh) 用于保持涡轮发动机部件的工具,包括用于连接和固定部件的装置以及通过铜焊或焊接连接所述部件的零件
US10384302B2 (en) Weld stub arrangement and a method of using the arrangement to make an article
KR20140108252A (ko) 코팅 작업에서 사용하기 위한 툴링 고정구 조립체
JP2004197747A5 (https=)
EP0138887B1 (en) Method for reshaping a gas turbine engine combustor part
US9925623B2 (en) Case assembly and method
JP2008169839A (ja) タービンノズルアセンブリの製造方法及び装置
CA2571900C (en) Method for repairing a turbine engine vane assembly and repaired assembly
JP2007146847A (ja) 燃焼器ドーム補修方法
EP3822457A1 (en) Friction welded composite turbine disc rotor for a turbomachine
CN101896311B (zh) 用于制造整体安装叶片的转子的方法以及转子
CN113385872B (zh) 壳体组合定位焊接装置以及方法
US6629415B2 (en) Methods and apparatus for modeling gas turbine engine combustor liners
US12078355B2 (en) Resonator ring, method and basket
JP4334433B2 (ja) シャシーダイナモメータ
JP4897668B2 (ja) ハニカムシールの製造方法

Legal Events

Date Code Title Description
A521 Written amendment

Free format text: JAPANESE INTERMEDIATE CODE: A523

Effective date: 20061218

A621 Written request for application examination

Free format text: JAPANESE INTERMEDIATE CODE: A621

Effective date: 20061218

A977 Report on retrieval

Free format text: JAPANESE INTERMEDIATE CODE: A971007

Effective date: 20090414

A01 Written decision to grant a patent or to grant a registration (utility model)

Free format text: JAPANESE INTERMEDIATE CODE: A01

Effective date: 20090421

A045 Written measure of dismissal of application [lapsed due to lack of payment]

Free format text: JAPANESE INTERMEDIATE CODE: A045

Effective date: 20090825