JPS5566625A - Seallup device responsible to thermal expansion - Google Patents
Seallup device responsible to thermal expansionInfo
- Publication number
- JPS5566625A JPS5566625A JP14317979A JP14317979A JPS5566625A JP S5566625 A JPS5566625 A JP S5566625A JP 14317979 A JP14317979 A JP 14317979A JP 14317979 A JP14317979 A JP 14317979A JP S5566625 A JPS5566625 A JP S5566625A
- Authority
- JP
- Japan
- Prior art keywords
- seallup
- thermal expansion
- device responsible
- responsible
- expansion
- 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.)
- Pending
Links
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
- F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
- F23R3/60—Support structures; Attaching or mounting means
-
- 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
- F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
- F01D9/023—Transition ducts between combustor cans and first stage of the turbine in gas-turbine engines; their cooling or sealings
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CH1152278A CH633351A5 (de) | 1978-11-09 | 1978-11-09 | Waermedehnungen nachgebende abdichtung einer ringbrennkammer fuer eine gasturbine. |
Publications (1)
Publication Number | Publication Date |
---|---|
JPS5566625A true JPS5566625A (en) | 1980-05-20 |
Family
ID=4374302
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP14317979A Pending JPS5566625A (en) | 1978-11-09 | 1979-11-05 | Seallup device responsible to thermal expansion |
Country Status (7)
Country | Link |
---|---|
JP (1) | JPS5566625A (ja) |
AT (1) | AT358336B (ja) |
CH (1) | CH633351A5 (ja) |
DE (1) | DE2849665A1 (ja) |
FR (1) | FR2441060A1 (ja) |
GB (1) | GB2035474A (ja) |
SE (1) | SE7909227L (ja) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2017090221A1 (ja) * | 2015-11-26 | 2017-06-01 | 川崎重工業株式会社 | トランジション構造 |
Families Citing this family (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2102897B (en) * | 1981-07-27 | 1985-06-19 | Gen Electric | Annular seals |
US5081833A (en) * | 1988-04-21 | 1992-01-21 | Nuovopignone-Industrie Meccaniche E Fonderia S.P.A. | Device for keeping the annular outlet mouth of the gas volute always centered about the nozzle assembly in a gas turbine |
FR2686683B1 (fr) * | 1992-01-28 | 1994-04-01 | Snecma | Turbomachine a chambre de combustion demontable. |
DE4323706A1 (de) * | 1993-07-15 | 1995-01-19 | Abb Management Ag | Gasturbine |
DE4324035C2 (de) * | 1993-07-17 | 2003-02-27 | Alstom | Gasturbine |
US6418727B1 (en) | 2000-03-22 | 2002-07-16 | Allison Advanced Development Company | Combustor seal assembly |
FR2825783B1 (fr) * | 2001-06-06 | 2003-11-07 | Snecma Moteurs | Accrochage de chambre de combustion cmc de turbomachine par pattes brasees |
FR2825781B1 (fr) * | 2001-06-06 | 2004-02-06 | Snecma Moteurs | Montage elastique de chambre ce combustion cmc de turbomachine dans un carter metallique |
FR2825785B1 (fr) | 2001-06-06 | 2004-08-27 | Snecma Moteurs | Liaison de chambre de combustion cmc de turbomachine en deux parties |
FR2825784B1 (fr) | 2001-06-06 | 2003-08-29 | Snecma Moteurs | Accrochage de chambre de combustion cmc de turbomachine utilisant les trous de dilution |
ES2569521T3 (es) | 2005-12-14 | 2016-05-11 | Alstom Technology Ltd | Turbomáquina |
US8141879B2 (en) * | 2009-07-20 | 2012-03-27 | General Electric Company | Seals for a turbine engine, and methods of assembling a turbine engine |
DE102020203017A1 (de) * | 2020-03-10 | 2021-09-16 | Siemens Aktiengesellschaft | Brennkammer mit keramischem Hitzeschild und Dichtung |
-
1978
- 1978-11-09 CH CH1152278A patent/CH633351A5/de not_active IP Right Cessation
- 1978-11-16 DE DE19782849665 patent/DE2849665A1/de active Pending
- 1978-11-16 AT AT817778A patent/AT358336B/de not_active IP Right Cessation
-
1979
- 1979-11-05 JP JP14317979A patent/JPS5566625A/ja active Pending
- 1979-11-07 SE SE7909227A patent/SE7909227L/xx unknown
- 1979-11-08 FR FR7927569A patent/FR2441060A1/fr active Pending
- 1979-11-09 GB GB7938911A patent/GB2035474A/en not_active Withdrawn
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2017090221A1 (ja) * | 2015-11-26 | 2017-06-01 | 川崎重工業株式会社 | トランジション構造 |
GB2561109A (en) * | 2015-11-26 | 2018-10-03 | Kawasaki Heavy Ind Ltd | Transition structure |
GB2561109B (en) * | 2015-11-26 | 2020-06-24 | Kawasaki Heavy Ind Ltd | Transition structure |
Also Published As
Publication number | Publication date |
---|---|
GB2035474A (en) | 1980-06-18 |
DE2849665A1 (de) | 1980-05-14 |
CH633351A5 (de) | 1982-11-30 |
FR2441060A1 (fr) | 1980-06-06 |
AT358336B (de) | 1980-09-10 |
ATA817778A (de) | 1980-01-15 |
SE7909227L (sv) | 1980-05-10 |
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