CN100520012C - 用于连接冷却管和通孔的易装配的热屏蔽装置 - Google Patents

用于连接冷却管和通孔的易装配的热屏蔽装置 Download PDF

Info

Publication number
CN100520012C
CN100520012C CNB03145304XA CN03145304A CN100520012C CN 100520012 C CN100520012 C CN 100520012C CN B03145304X A CNB03145304X A CN B03145304XA CN 03145304 A CN03145304 A CN 03145304A CN 100520012 C CN100520012 C CN 100520012C
Authority
CN
China
Prior art keywords
hole
thermal shield
shield apparatus
planar surface
easy assembling
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 - Lifetime
Application number
CNB03145304XA
Other languages
English (en)
Chinese (zh)
Other versions
CN1495341A (zh
Inventor
M·佩基奥利
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.)
Nuovo Pignone SpA
Nuovo Pignone Technologie SRL
Original Assignee
Nuovo Pignone Holding SpA
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 Nuovo Pignone Holding SpA filed Critical Nuovo Pignone Holding SpA
Publication of CN1495341A publication Critical patent/CN1495341A/zh
Application granted granted Critical
Publication of CN100520012C publication Critical patent/CN100520012C/zh
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/28—Arrangement of seals
    • 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
    • F01D9/00—Stators
    • F01D9/06—Fluid supply conduits to nozzles or the like
    • F01D9/065—Fluid supply or removal conduits traversing the working fluid flow, e.g. for lubrication-, cooling-, or sealing fluids
    • 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
    • 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
    • F01D25/08—Cooling; Heating; Heat-insulation

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
CNB03145304XA 2002-07-03 2003-07-03 用于连接冷却管和通孔的易装配的热屏蔽装置 Expired - Lifetime CN100520012C (zh)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
ITMI2002A001465 2002-07-03
IT2002MI001465A ITMI20021465A1 (it) 2002-07-03 2002-07-03 Dispositivo di schermatura termica di facile montaggio per un accoppiamento tra una tubazione di raffreddamento ed una foratura passante rea

Publications (2)

Publication Number Publication Date
CN1495341A CN1495341A (zh) 2004-05-12
CN100520012C true CN100520012C (zh) 2009-07-29

Family

ID=11450134

Family Applications (1)

Application Number Title Priority Date Filing Date
CNB03145304XA Expired - Lifetime CN100520012C (zh) 2002-07-03 2003-07-03 用于连接冷却管和通孔的易装配的热屏蔽装置

Country Status (8)

Country Link
US (1) US6890147B2 (enExample)
EP (1) EP1378632B1 (enExample)
JP (1) JP4307920B2 (enExample)
KR (1) KR100790627B1 (enExample)
CN (1) CN100520012C (enExample)
CA (1) CA2432816C (enExample)
IT (1) ITMI20021465A1 (enExample)
NO (1) NO20033033L (enExample)

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102004014117A1 (de) * 2004-03-23 2005-10-13 Alstom Technology Ltd Komponente einer Turbomaschine mit einer Kühlanordnung
GB0508912D0 (en) * 2005-04-30 2005-06-08 Rolls Royce Plc Vane coupling
US8596959B2 (en) * 2009-10-09 2013-12-03 Pratt & Whitney Canada Corp. Oil tube with integrated heat shield
US9316117B2 (en) 2012-01-30 2016-04-19 United Technologies Corporation Internally cooled spoke
US9316153B2 (en) * 2013-01-22 2016-04-19 Siemens Energy, Inc. Purge and cooling air for an exhaust section of a gas turbine assembly
EP2933436A1 (de) * 2014-04-15 2015-10-21 Siemens Aktiengesellschaft Radscheibe mit wenigstens einem Dichtblech
US9920869B2 (en) * 2014-05-22 2018-03-20 United Technologies Corporation Cooling systems for gas turbine engine components
US9790860B2 (en) 2015-01-16 2017-10-17 United Technologies Corporation Cooling passages for a mid-turbine frame
PL421120A1 (pl) 2017-04-04 2018-10-08 General Electric Company Polska Spolka Z Ograniczona Odpowiedzialnoscia Silnik turbinowy i części składowe do stosowania w nim
FR3101372B1 (fr) * 2019-09-27 2021-10-01 Safran Aircraft Engines Turbomachine d’aeronef
US11692485B2 (en) 2021-02-18 2023-07-04 Generai, Electric Company Gas turbine engine with spoolie fluid transfer connection
US12698722B2 (en) 2022-11-01 2026-08-04 General Electric Company Gas turbine engine

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3370830A (en) 1966-12-12 1968-02-27 Gen Motors Corp Turbine cooling
US3574354A (en) * 1969-05-08 1971-04-13 Avica Corp Flexible coupling
US5224818A (en) 1991-11-01 1993-07-06 General Electric Company Air transfer bushing
US5517817A (en) * 1993-10-28 1996-05-21 General Electric Company Variable area turbine nozzle for turbine engines
CA2263508C (en) * 1997-06-19 2003-08-19 Mitsubishi Heavy Industries, Ltd. Sealing device for gas turbine stator blades
JP3564290B2 (ja) 1997-12-24 2004-09-08 三菱重工業株式会社 蒸気冷却型ガスタービン
ITMI991208A1 (it) * 1999-05-31 2000-12-01 Nuovo Pignone Spa Dispositivo per il posizionamento di ugelli di uno stadio statorico eper il raffreddamento di dischi rotorici in turbine a gas
US6382906B1 (en) * 2000-06-16 2002-05-07 General Electric Company Floating spoolie cup impingement baffle
JP2002155703A (ja) 2000-11-21 2002-05-31 Mitsubishi Heavy Ind Ltd ガスタービン静翼−翼環間蒸気通路のシール構造
ITMI20020910A1 (it) * 2002-04-29 2003-10-29 Nuovo Pignone Spa Dispositivo di tenuta per accoppiamento di una tubazione con un foro

Also Published As

Publication number Publication date
KR100790627B1 (ko) 2007-12-31
JP2004052765A (ja) 2004-02-19
EP1378632A3 (en) 2005-11-23
US20040057825A1 (en) 2004-03-25
CA2432816C (en) 2010-11-09
US6890147B2 (en) 2005-05-10
NO20033033L (no) 2004-01-05
EP1378632B1 (en) 2015-03-11
JP4307920B2 (ja) 2009-08-05
CN1495341A (zh) 2004-05-12
KR20040004125A (ko) 2004-01-13
EP1378632A2 (en) 2004-01-07
ITMI20021465A0 (it) 2002-07-03
ITMI20021465A1 (it) 2004-01-05
NO20033033D0 (no) 2003-07-02
CA2432816A1 (en) 2004-01-03

Similar Documents

Publication Publication Date Title
CN100580321C (zh) 火管或管衬固定系统
US8448444B2 (en) Method and apparatus for mounting transition piece in combustor
JP3947429B2 (ja) 希釈孔を用いたターボマシンにおけるｃｍｃ燃焼室の取り付け
US7451599B2 (en) Fuel manifold inlet tube
CA2432816C (en) Easy-fit heat screening device for connecting a cooling pipe and a through-hole formed in a nozzle support ring of a gas turbine
CN103090412A (zh) 喷射装置
CN101737803B (zh) 一种燃气涡轮发动机及其燃料喷嘴组件
US8707673B1 (en) Articulated transition duct in turbomachine
CN102597632A (zh) 燃烧器、操作方法和组装方法
US9500370B2 (en) Apparatus for mixing fuel in a gas turbine nozzle
CN102954488A (zh) 用于燃烧器的点火系统
CN108758694B (zh) 涡轮机联接组件
JP5047309B2 (ja) ガスタービンにおけるバーナ
CN102865110B (zh) 用于涡轮系统中的过渡导管的支撑组件
EP2622278B1 (en) Gas turbine assembly and method therefor
KR102756987B1 (ko) 크로스 파이어 튜브 설치/제거 방법 및 장치
EP1400681A3 (en) Methods and apparatus for supporting high temperature ducting
CN102865145B (zh) 涡轮机系统及用于涡轮机系统的支承组件
CN104185763A (zh) 燃气涡轮燃烧器
US9488105B2 (en) Gas turbine assembly and method therefor
CN105465832B (zh) 具有用于燃烧器部件的紧固系统的燃烧器装置
KR101842745B1 (ko) 가스터빈의 트랜지션피스와 터빈의 결합장치
KR102047368B1 (ko) 연료 노즐, 이를 포함하는 연소기 및 가스 터빈
JPH11211087A (ja) ガスタービン火炎伝播管

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
C14 Grant of patent or utility model
GR01 Patent grant
TR01 Transfer of patent right

Effective date of registration: 20220314

Address after: Italy, Florence

Patentee after: NUOVO PIGNONE S.R.L.

Address before: Italy, Florence

Patentee before: NUOVO PIGNONE S.P.A.

Effective date of registration: 20220314

Address after: Italy, Florence

Patentee after: NUOVO PIGNONE TECNOLOGIE S.R.L.

Address before: Italy, Florence

Patentee before: NUOVO PIGNONE S.R.L.

Effective date of registration: 20220314

Address after: Italy, Florence

Patentee after: NUOVO PIGNONE S.P.A.

Address before: Italy, Florence

Patentee before: Nuovo Pignone Holding S.P.A.

TR01 Transfer of patent right
CX01 Expiry of patent term

Granted publication date: 20090729

CX01 Expiry of patent term