CA2499908A1 - Montage de refroidissement de chambre de combustion a turbine a gaz - Google Patents

Montage de refroidissement de chambre de combustion a turbine a gaz

Info

Publication number
CA2499908A1
CA2499908A1 CA002499908A CA2499908A CA2499908A1 CA 2499908 A1 CA2499908 A1 CA 2499908A1 CA 002499908 A CA002499908 A CA 002499908A CA 2499908 A CA2499908 A CA 2499908A CA 2499908 A1 CA2499908 A1 CA 2499908A1
Authority
CA
Canada
Prior art keywords
groove
hole
cooling
wall
air
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.)
Granted
Application number
CA002499908A
Other languages
English (en)
Other versions
CA2499908C (fr
Inventor
Yoshichika Sato
Koichi Nishida
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.)
Mitsubishi Heavy Industries Ltd
Original Assignee
Mitsubishi Heavy Industries, Ltd.
Yoshichika Sato
Koichi Nishida
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
Priority claimed from JP32237898A external-priority patent/JP3626861B2/ja
Priority claimed from JP32370498A external-priority patent/JP3626862B2/ja
Application filed by Mitsubishi Heavy Industries, Ltd., Yoshichika Sato, Koichi Nishida filed Critical Mitsubishi Heavy Industries, Ltd.
Priority claimed from CA002288557A external-priority patent/CA2288557C/fr
Publication of CA2499908A1 publication Critical patent/CA2499908A1/fr
Application granted granted Critical
Publication of CA2499908C publication Critical patent/CA2499908C/fr
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Landscapes

  • Turbine Rotor Nozzle Sealing (AREA)
CA002499908A 1998-11-12 1999-11-04 Montage de refroidissement de chambre de combustion a turbine a gaz Expired - Fee Related CA2499908C (fr)

Applications Claiming Priority (5)

Application Number Priority Date Filing Date Title
JP32237898A JP3626861B2 (ja) 1998-11-12 1998-11-12 ガスタービン燃焼器の冷却構造
JP10-322378 1998-11-12
JP10-323704 1998-11-13
JP32370498A JP3626862B2 (ja) 1998-11-13 1998-11-13 ガスタービン燃焼器パイロットコーンの冷却構造
CA002288557A CA2288557C (fr) 1998-11-12 1999-11-04 Montage de refroidissement de chambre de combustion a turbine a gaz

Related Parent Applications (1)

Application Number Title Priority Date Filing Date
CA002288557A Division CA2288557C (fr) 1998-11-12 1999-11-04 Montage de refroidissement de chambre de combustion a turbine a gaz

Publications (2)

Publication Number Publication Date
CA2499908A1 true CA2499908A1 (fr) 2000-05-12
CA2499908C CA2499908C (fr) 2007-06-26

Family

ID=34527231

Family Applications (1)

Application Number Title Priority Date Filing Date
CA002499908A Expired - Fee Related CA2499908C (fr) 1998-11-12 1999-11-04 Montage de refroidissement de chambre de combustion a turbine a gaz

Country Status (1)

Country Link
CA (1) CA2499908C (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113217948A (zh) * 2021-05-13 2021-08-06 中国联合重型燃气轮机技术有限公司 燃烧室层板及燃烧室

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112880296B (zh) * 2020-12-31 2022-11-29 山东微波电真空技术有限公司 一种可快速降温的装配机

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113217948A (zh) * 2021-05-13 2021-08-06 中国联合重型燃气轮机技术有限公司 燃烧室层板及燃烧室

Also Published As

Publication number Publication date
CA2499908C (fr) 2007-06-26

Similar Documents

Publication Publication Date Title
CA2288557A1 (fr) Montage de refroidissement de chambre de combustion a turbine a gaz
US3572031A (en) Variable area cooling passages for gas turbine burners
JP4248785B2 (ja) ガスタービン固定子の径を調節するための装置
CA2372070A1 (fr) Structure de sortie d'element de transition permettant de diminuer la temperature ainsi qu'un element de transition , une chambre de combustion et une turbine a gaz comportant cette meme structure de sortie
Ünal Theoretical analysis of triple concentric-tube heat exchangers Part 2: Case studies
AU6209699A (en) Heat exchanger
WO2002044479A1 (fr) Machines de chantier
JPS61114093A (ja) 熱交換器
KR950704660A (ko) 가열 및 냉각 장치(heat and cold machine)
CA2499908A1 (fr) Montage de refroidissement de chambre de combustion a turbine a gaz
EP0757215A3 (fr) Appareil frigorifique à absorption
US4702312A (en) Thin rod packing for heat exchangers
JPS5637489A (en) Heat exchanger
US3983935A (en) Heat exchanger
CN106382136B (zh) 一种跨音速动叶叶顶间隙主动控制装置
FR2584136A1 (fr) Piece a profil d'ailette pour moteur a turbine a gaz
CA2227551A1 (fr) Controle des debits de refroidissement pour des chambres de combustion a haute temperature
JPS5636352A (en) Manufacture of high-temperature gas flowing tube having bending part
WO1995023319A3 (fr) Dispositif de chauffage a combustible liquide pour vehicule
CA2330084A1 (fr) Echangeur de chaleur avec ailettes tres poreuses fonctionnant par transpiration
CA2268837A1 (fr) Echangeur de chaleur
US3988700A (en) Gas-dynamic molecular laser
SU1556204A1 (ru) Диаметральный вентил тор
JP2007173403A (ja) 熱交換装置
JPS5833091A (ja) 2重管式熱交換器

Legal Events

Date Code Title Description
EEER Examination request
MKLA Lapsed