IT7921209A0 - Perfezionamenti apportati alle palette direttrici per motori a turbina a gas. - Google Patents
Perfezionamenti apportati alle palette direttrici per motori a turbina a gas.Info
- Publication number
- IT7921209A0 IT7921209A0 IT7921209A IT2120979A IT7921209A0 IT 7921209 A0 IT7921209 A0 IT 7921209A0 IT 7921209 A IT7921209 A IT 7921209A IT 2120979 A IT2120979 A IT 2120979A IT 7921209 A0 IT7921209 A0 IT 7921209A0
- Authority
- IT
- Italy
- Prior art keywords
- gas turbine
- turbine engines
- improvements made
- guide blades
- blades
- Prior art date
Links
- RLQJEEJISHYWON-UHFFFAOYSA-N flonicamid Chemical compound FC(F)(F)C1=CC=NC=C1C(=O)NCC#N RLQJEEJISHYWON-UHFFFAOYSA-N 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
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1152978 | 1978-03-22 | ||
GB7907474A GB2017229B (en) | 1978-03-22 | 1979-03-02 | Guides vanes for gas turbine enginess |
Publications (2)
Publication Number | Publication Date |
---|---|
IT7921209A0 true IT7921209A0 (it) | 1979-03-22 |
IT1162720B IT1162720B (it) | 1987-04-01 |
Family
ID=26248339
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
IT21209/79A IT1162720B (it) | 1978-03-22 | 1979-03-22 | Perfezionamenti apportati alle palette direttrici per motori a turbina a gas |
Country Status (2)
Country | Link |
---|---|
GB (1) | GB2017229B (it) |
IT (1) | IT1162720B (it) |
Families Citing this family (17)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2473621A1 (fr) * | 1980-01-10 | 1981-07-17 | Snecma | Aube de distributeur de turbine |
US4312624A (en) * | 1980-11-10 | 1982-01-26 | United Technologies Corporation | Air cooled hollow vane construction |
GB2163218B (en) * | 1981-07-07 | 1986-07-16 | Rolls Royce | Cooled vane or blade for a gas turbine engine |
GB2119028B (en) * | 1982-04-27 | 1985-02-27 | Rolls Royce | Aerofoil for a gas turbine engine |
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 |
US5203873A (en) * | 1991-08-29 | 1993-04-20 | General Electric Company | Turbine blade impingement baffle |
GB2343486B (en) | 1998-06-19 | 2000-09-20 | Rolls Royce Plc | Improvemnts in or relating to cooling systems for gas turbine engine airfoil |
US6238182B1 (en) * | 1999-02-19 | 2001-05-29 | Meyer Tool, Inc. | Joint for a turbine component |
GB2366599B (en) | 2000-09-09 | 2004-10-27 | Rolls Royce Plc | Gas turbine engine system |
GB2386926A (en) * | 2002-03-27 | 2003-10-01 | Alstom | Two part impingement tube for a turbine blade or vane |
GB2441771B (en) * | 2006-09-13 | 2009-07-08 | Rolls Royce Plc | Cooling arrangement for a component of a gas turbine engine |
JP4995141B2 (ja) * | 2008-05-08 | 2012-08-08 | 三菱重工業株式会社 | タービン用翼構造 |
US20140093392A1 (en) * | 2012-10-03 | 2014-04-03 | Rolls-Royce Plc | Gas turbine engine component |
EP2860348A1 (de) * | 2013-10-08 | 2015-04-15 | Siemens Aktiengesellschaft | Einsatz für eine Turbinenschaufel aus mehreren Bauteilen und zugehöriges Verfahren |
US10329932B2 (en) | 2015-03-02 | 2019-06-25 | United Technologies Corporation | Baffle inserts |
US10781715B2 (en) * | 2015-12-21 | 2020-09-22 | Raytheon Technologies Corporation | Impingement cooling baffle |
US10502070B2 (en) * | 2016-11-17 | 2019-12-10 | United Technologies Corporation | Airfoil with laterally insertable baffle |
-
1979
- 1979-03-02 GB GB7907474A patent/GB2017229B/en not_active Expired
- 1979-03-22 IT IT21209/79A patent/IT1162720B/it active
Also Published As
Publication number | Publication date |
---|---|
IT1162720B (it) | 1987-04-01 |
GB2017229A (en) | 1979-10-03 |
GB2017229B (en) | 1982-07-14 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
IT7921628A0 (it) | Motore a turbina a gas. | |
IT7925707A0 (it) | Fascia per motore a turbina. | |
IT8020482A0 (it) | Rotore palettato per motore a turbina a gas. | |
GB2028928B (en) | Aerofoil blade for a gas turbine engine | |
IT8020445A0 (it) | Motore a turbina a gas. | |
JPS54160911A (en) | Blade for gas turbine engine | |
IT7821288A0 (it) | Motore per turbina a gas. | |
IT7822829A0 (it) | Struttura a paletta di guida per ugelli di motori a turbina a gas. | |
IT8019702A0 (it) | Cappottatura di motore a turbina agas. | |
IT7921209A0 (it) | Perfezionamenti apportati alle palette direttrici per motori a turbina a gas. | |
IT7821869A0 (it) | Paletta di rotore raffreddata per motore a turbina a gas. | |
NO157115C (no) | Gassturbinanlegg. | |
IT8321090A0 (it) | Prediffusore per motori a turbina a gas. | |
IT7919045A0 (it) | Paletta di rotore o paletta direttrice per turbina a gas. | |
IT7919648A0 (it) | Motori a turbina a gas. | |
IT8025620A0 (it) | Motore a turbina a gas modulare. | |
IT8020740A0 (it) | Perfezionamenti apportati ai bruciatori per motori a turbina agas. | |
IT7822908A0 (it) | Paletta di rotore per motore a turbina a gas. | |
GB2030233B (en) | Gas turbine engine blade | |
IT7830937A0 (it) | Perfezionamenti apportati ai motori a turbina a gas. | |
IT7925730A0 (it) | Controllo di combustibile elettronico per una installazione a turbina a gas a molti motori. | |
IT8020480A0 (it) | Rotore palettato per motore a turbina a gas. | |
IT1120435B (it) | Perfezionamento nei motori a turbina a gas | |
IT7927234A0 (it) | Assieme di palette direttrici di distributore per motore a turbina a gas. | |
IT1106135B (it) | Incrementatore di spinta per motori a turbina |