CH555000A - Hohlschaufel fuer mit elastischem treibmittel betriebene axial-stroemungsmaschine. - Google Patents
Hohlschaufel fuer mit elastischem treibmittel betriebene axial-stroemungsmaschine.Info
- Publication number
- CH555000A CH555000A CH1113672A CH1113672A CH555000A CH 555000 A CH555000 A CH 555000A CH 1113672 A CH1113672 A CH 1113672A CH 1113672 A CH1113672 A CH 1113672A CH 555000 A CH555000 A CH 555000A
- Authority
- CH
- Switzerland
- Prior art keywords
- axial flow
- flow machine
- elastic fluid
- machine operated
- hollow bucket
- Prior art date
Links
- 239000012530 fluid Substances 0.000 title 1
Classifications
-
- 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
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/12—Blades
- F01D5/14—Form or construction
- F01D5/18—Hollow blades, i.e. blades with cooling or heating channels or cavities; Heating, heat-insulating or cooling means on blades
- F01D5/187—Convection cooling
- F01D5/188—Convection cooling with an insert in the blade cavity to guide the cooling fluid, e.g. forming a separation wall
- F01D5/189—Convection cooling with an insert in the blade cavity to guide the cooling fluid, e.g. forming a separation wall the insert having a tubular cross-section, e.g. airfoil shape
-
- 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
- F01D9/04—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
- F01D9/042—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector fixing blades to stators
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US16758671A | 1971-07-30 | 1971-07-30 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CH555000A true CH555000A (de) | 1974-10-15 |
Family
ID=22607968
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CH1113672A CH555000A (de) | 1971-07-30 | 1972-07-26 | Hohlschaufel fuer mit elastischem treibmittel betriebene axial-stroemungsmaschine. |
Country Status (9)
| Country | Link |
|---|---|
| US (1) | US3767322A (de) |
| JP (1) | JPS5134925B1 (de) |
| CA (1) | CA951245A (de) |
| CH (1) | CH555000A (de) |
| DE (1) | DE2235375A1 (de) |
| FR (1) | FR2149105A5 (de) |
| GB (1) | GB1331206A (de) |
| IT (1) | IT963241B (de) |
| NL (1) | NL7210441A (de) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US10975701B2 (en) * | 2016-08-10 | 2021-04-13 | General Electric Company | Ceramic matrix composite component cooling |
Families Citing this family (56)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3864058A (en) * | 1973-02-05 | 1975-02-04 | Garrett Corp | Cooled aerodynamic device |
| US3973874A (en) * | 1974-09-25 | 1976-08-10 | General Electric Company | Impingement baffle collars |
| US4169692A (en) * | 1974-12-13 | 1979-10-02 | General Electric Company | Variable area turbine nozzle and means for sealing same |
| CH584833A5 (de) * | 1975-05-16 | 1977-02-15 | Bbc Brown Boveri & Cie | |
| US4086757A (en) * | 1976-10-06 | 1978-05-02 | Caterpillar Tractor Co. | Gas turbine cooling system |
| US4221539A (en) * | 1977-04-20 | 1980-09-09 | The Garrett Corporation | Laminated airfoil and method for turbomachinery |
| US4297077A (en) * | 1979-07-09 | 1981-10-27 | Westinghouse Electric Corp. | Cooled turbine vane |
| US4288201A (en) * | 1979-09-14 | 1981-09-08 | United Technologies Corporation | Vane cooling structure |
| DE3003347A1 (de) * | 1979-12-20 | 1981-06-25 | BBC AG Brown, Boveri & Cie., Baden, Aargau | Gekuehlte wand |
| US4381173A (en) * | 1980-08-25 | 1983-04-26 | United Technologies Corporation | Coolable rotor blade assembly for an axial flow rotary machine |
| GB2097479B (en) | 1981-04-24 | 1984-09-05 | Rolls Royce | Cooled vane for a gas turbine engine |
| US4526512A (en) * | 1983-03-28 | 1985-07-02 | General Electric Co. | Cooling flow control device for turbine blades |
| US4645415A (en) * | 1983-12-23 | 1987-02-24 | United Technologies Corporation | Air cooler for providing buffer air to a bearing compartment |
| US4798515A (en) * | 1986-05-19 | 1989-01-17 | The United States Of America As Represented By The Secretary Of The Air Force | Variable nozzle area turbine vane cooling |
| DE3629910A1 (de) * | 1986-09-03 | 1988-03-17 | Mtu Muenchen Gmbh | Metallisches hohlbauteil mit einem metallischen einsatz, insbesondere turbinenschaufel mit kuehleinsatz |
| US5102299A (en) * | 1986-11-10 | 1992-04-07 | The United States Of America As Represented By The Secretary Of The Air Force | Airfoil trailing edge cooling configuration |
| US5207556A (en) * | 1992-04-27 | 1993-05-04 | General Electric Company | Airfoil having multi-passage baffle |
| US5511937A (en) * | 1994-09-30 | 1996-04-30 | Westinghouse Electric Corporation | Gas turbine airfoil with a cooling air regulating seal |
| FR2771446B1 (fr) * | 1997-11-27 | 1999-12-31 | Snecma | Aube de distributeur de turbine refroidie |
| US6238182B1 (en) | 1999-02-19 | 2001-05-29 | Meyer Tool, Inc. | Joint for a turbine component |
| 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 |
| ITTO20010704A1 (it) * | 2001-07-18 | 2003-01-18 | Fiatavio Spa | Paletta a doppia parete per una turbina, particolarmente per applicazioni aeronautiche. |
| FR2856729B1 (fr) * | 2003-06-30 | 2005-09-23 | Snecma Moteurs | Aubes refroidies de moteur a turbine a gaz. |
| FR2858829B1 (fr) * | 2003-08-12 | 2008-03-14 | Snecma Moteurs | Aube refroidie de moteur a turbine a gaz |
| GB0405843D0 (en) * | 2004-03-16 | 2004-04-21 | Westland Helicopters | Improvements in or relating to aerofoils |
| US20050265840A1 (en) * | 2004-05-27 | 2005-12-01 | Levine Jeffrey R | Cooled rotor blade with leading edge impingement cooling |
| US7278826B2 (en) * | 2004-08-18 | 2007-10-09 | Pratt & Whitney Canada Corp. | Airfoil cooling passage trailing edge flow restriction |
| US7946815B2 (en) * | 2007-03-27 | 2011-05-24 | Siemens Energy, Inc. | Airfoil for a gas turbine engine |
| GB0719786D0 (en) * | 2007-10-11 | 2007-11-21 | Rolls Royce Plc | A vane and a vane assembly for a gas turbine engine |
| FR2922597B1 (fr) * | 2007-10-19 | 2012-11-16 | Snecma | Aube refroidie de turbomachine |
| US8393867B2 (en) | 2008-03-31 | 2013-03-12 | United Technologies Corporation | Chambered airfoil cooling |
| US20090324387A1 (en) * | 2008-06-30 | 2009-12-31 | General Electric Company | Aft frame with oval-shaped cooling slots and related method |
| US7956486B2 (en) * | 2009-05-23 | 2011-06-07 | Abel Echemendia | Windmill electric generator for hydroelectric power system |
| US9011077B2 (en) | 2011-04-20 | 2015-04-21 | Siemens Energy, Inc. | Cooled airfoil in a turbine engine |
| US9335051B2 (en) * | 2011-07-13 | 2016-05-10 | United Technologies Corporation | Ceramic matrix composite combustor vane ring assembly |
| JP5881355B2 (ja) * | 2011-09-27 | 2016-03-09 | 三菱日立パワーシステムズ株式会社 | 静翼及び蒸気タービン |
| WO2015123017A1 (en) | 2014-02-13 | 2015-08-20 | United Technologies Corporation | Air shredder insert |
| EP3032034B1 (de) * | 2014-12-12 | 2019-11-27 | United Technologies Corporation | Prallblecheinsatz, leitschaufel mit einem prallblecheinsatz und zugehöriges herstellungsverfahren für eine leitschaufel |
| US9879554B2 (en) * | 2015-01-09 | 2018-01-30 | Solar Turbines Incorporated | Crimped insert for improved turbine vane internal cooling |
| US10024172B2 (en) * | 2015-02-27 | 2018-07-17 | United Technologies Corporation | Gas turbine engine airfoil |
| US10422244B2 (en) * | 2015-03-16 | 2019-09-24 | General Electric Company | System for cooling a turbine shroud |
| GB201504522D0 (en) | 2015-03-18 | 2015-04-29 | Rolls Royce Plc | A vane |
| US9957820B2 (en) * | 2015-06-02 | 2018-05-01 | United Technologies Corporation | Heat shield for a vane assembly of a gas turbine engine |
| RU2706211C2 (ru) | 2016-01-25 | 2019-11-14 | Ансалдо Энерджиа Свитзерлэнд Аг | Охлаждаемая стенка компонента турбины и способ охлаждения этой стенки |
| US10260363B2 (en) | 2016-12-08 | 2019-04-16 | General Electric Company | Additive manufactured seal for insert compartmentalization |
| JP6353131B1 (ja) * | 2017-06-29 | 2018-07-04 | 三菱日立パワーシステムズ株式会社 | タービン翼及びガスタービン |
| US10570751B2 (en) | 2017-11-22 | 2020-02-25 | General Electric Company | Turbine engine airfoil assembly |
| US10662783B2 (en) * | 2018-08-29 | 2020-05-26 | United Technologies Corporation | Variable heat transfer collector baffle |
| US10815794B2 (en) * | 2018-12-05 | 2020-10-27 | Raytheon Technologies Corporation | Baffle for components of gas turbine engines |
| US11280201B2 (en) * | 2019-10-14 | 2022-03-22 | Raytheon Technologies Corporation | Baffle with tail |
| US11506063B2 (en) * | 2019-11-07 | 2022-11-22 | Raytheon Technologies Corporation | Two-piece baffle |
| US11448078B2 (en) | 2020-04-23 | 2022-09-20 | Raytheon Technologies Corporation | Spring loaded airfoil vane |
| US11230931B1 (en) | 2020-07-03 | 2022-01-25 | Raytheon Technologies Corporation | Inserts for airfoils of gas turbine engines |
| US11428166B2 (en) | 2020-11-12 | 2022-08-30 | Solar Turbines Incorporated | Fin for internal cooling of vane wall |
| US11512604B1 (en) * | 2021-05-04 | 2022-11-29 | Raytheon Technologies Corporation | Spring for radially stacked assemblies |
| US11536149B1 (en) * | 2022-03-11 | 2022-12-27 | Mitsubishi Heavy Industries, Ltd. | Cooling method and structure of vane of gas turbine |
Family Cites Families (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2873944A (en) * | 1952-09-10 | 1959-02-17 | Gen Motors Corp | Turbine blade cooling |
| FR1177035A (fr) * | 1957-05-28 | 1959-04-20 | Snecma | Procédé et dispositif de refroidissement d'organes de machines |
| US3388888A (en) * | 1966-09-14 | 1968-06-18 | Gen Electric | Cooled turbine nozzle for high temperature turbine |
| US3475107A (en) * | 1966-12-01 | 1969-10-28 | Gen Electric | Cooled turbine nozzle for high temperature turbine |
| DE1601613A1 (de) * | 1967-08-03 | 1970-12-17 | Motoren Turbinen Union | Turbinenschaufel,insbesondere Turbinenleitschaufel fuer Gasturbinentriebwerke |
| US3623318A (en) * | 1970-06-29 | 1971-11-30 | Avco Corp | Turbine nozzle cooling |
-
1971
- 1971-07-30 US US00167586A patent/US3767322A/en not_active Expired - Lifetime
-
1972
- 1972-03-22 CA CA137,744,A patent/CA951245A/en not_active Expired
- 1972-06-16 GB GB2824172A patent/GB1331206A/en not_active Expired
- 1972-07-19 DE DE2235375A patent/DE2235375A1/de active Pending
- 1972-07-21 IT IT27271/72A patent/IT963241B/it active
- 1972-07-25 FR FR7226708A patent/FR2149105A5/fr not_active Expired
- 1972-07-26 CH CH1113672A patent/CH555000A/de not_active IP Right Cessation
- 1972-07-28 JP JP47075177A patent/JPS5134925B1/ja active Pending
- 1972-07-28 NL NL7210441A patent/NL7210441A/xx unknown
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US10975701B2 (en) * | 2016-08-10 | 2021-04-13 | General Electric Company | Ceramic matrix composite component cooling |
Also Published As
| Publication number | Publication date |
|---|---|
| IT963241B (it) | 1974-01-10 |
| GB1331206A (en) | 1973-09-26 |
| CA951245A (en) | 1974-07-16 |
| NL7210441A (de) | 1973-02-01 |
| JPS5134925B1 (de) | 1976-09-29 |
| FR2149105A5 (de) | 1973-03-23 |
| US3767322A (en) | 1973-10-23 |
| DE2235375A1 (de) | 1973-02-08 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PL | Patent ceased |