IT939465B - Perfezionamento nei dispositivi di tenuta in particolare per turbine a gas - Google Patents
Perfezionamento nei dispositivi di tenuta in particolare per turbine a gasInfo
- Publication number
- IT939465B IT939465B IT53079/71A IT5307971A IT939465B IT 939465 B IT939465 B IT 939465B IT 53079/71 A IT53079/71 A IT 53079/71A IT 5307971 A IT5307971 A IT 5307971A IT 939465 B IT939465 B IT 939465B
- Authority
- IT
- Italy
- Prior art keywords
- improvement
- gas turbines
- sealing devices
- sealing
- devices
- Prior art date
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
- F02K1/78—Other construction of jet pipes
- F02K1/80—Couplings or connections
- F02K1/805—Sealing devices therefor, e.g. for movable parts of jet pipes or nozzle flaps
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16J—PISTONS; CYLINDERS; SEALINGS
- F16J15/00—Sealings
- F16J15/16—Sealings between relatively-moving surfaces
- F16J15/40—Sealings between relatively-moving surfaces by means of fluid
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Jet Pumps And Other Pumps (AREA)
- Joints Allowing Movement (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB4597670 | 1970-09-26 |
Publications (1)
Publication Number | Publication Date |
---|---|
IT939465B true IT939465B (it) | 1973-02-10 |
Family
ID=10439324
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
IT53079/71A IT939465B (it) | 1970-09-26 | 1971-09-24 | Perfezionamento nei dispositivi di tenuta in particolare per turbine a gas |
Country Status (5)
Country | Link |
---|---|
US (1) | US3729139A (it) |
DE (1) | DE2147866C2 (it) |
FR (1) | FR2108507A5 (it) |
GB (1) | GB1355190A (it) |
IT (1) | IT939465B (it) |
Families Citing this family (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE3223082C2 (de) * | 1981-06-19 | 1986-10-23 | Bernhard de Prof. Dipl.-Ing. 6501 Heidesheim Temple | Weichstoffkompensator sowie Verfahren zu dessen Vorwärmen und Kühlen |
US4471965A (en) * | 1982-05-05 | 1984-09-18 | Fmc Corporation | High-pressure fire-resistant metal seal |
US4747542A (en) * | 1987-04-14 | 1988-05-31 | United Technologies Corporation | Nozzle flap edge cooling |
DE4208472A1 (de) * | 1992-03-17 | 1993-09-23 | Mtu Muenchen Gmbh | Einrichtung zur abdichtung eines spaltes zwischen winkelversetzt und fest oder relativ zueinander beweglich angeordneten bauteilen |
US6020277A (en) * | 1994-06-23 | 2000-02-01 | Kimberly-Clark Corporation | Polymeric strands with enhanced tensile strength, nonwoven webs including such strands, and methods for making same |
US5801106A (en) * | 1996-05-10 | 1998-09-01 | Kimberly-Clark Worldwide, Inc. | Polymeric strands with high surface area or altered surface properties |
US6418709B1 (en) * | 2000-05-15 | 2002-07-16 | United Technologies Corporation | Gas turbine engine liner |
Family Cites Families (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE885799C (de) * | 1952-04-13 | 1953-08-06 | Escher Wyss Maschinenfabrik G | Verfahren zum Fernhalten von im Betriebswasser hydraulischer Anlagen enthaltenen Stoffen von Labyrinth-Stopfbuechsen der Maschinen solcher Anlagen |
US2308757A (en) * | 1941-08-16 | 1943-01-19 | Universal Oil Prod Co | Expansion joint |
US2625008A (en) * | 1951-02-28 | 1953-01-13 | Curtiss Wright Corp | Variable flow nozzle |
US3005338A (en) * | 1957-09-23 | 1961-10-24 | Paul A Libby | Nozzle cooling apparatus and method |
DE1182480B (de) * | 1960-03-19 | 1964-11-26 | Steinmueller Gmbh L & C | Dichtungsanordnung fuer Teleskoprohre in pneumatischen Staubfoerderleitungen |
DE1181510C2 (de) * | 1960-04-28 | 1965-07-01 | Polysius Gmbh | Einrichtung zum Abdichten von Einlauf- bzw. Auslaufenden bei Drehrohroefen und aehnlichen mittels Luft |
US3133413A (en) * | 1960-09-12 | 1964-05-19 | United Aircraft Corp | Control and cooling of rocket motors |
US3091924A (en) * | 1960-12-15 | 1963-06-04 | United Aircraft Corp | Gaseous nozzle boundary |
NL291174A (it) * | 1962-04-12 | |||
DE1218076B (de) * | 1962-09-29 | 1966-06-02 | Siemens Ag | Kernreaktor-Kuehlgeblaese mit Fluessigkeitswellendichtung |
FR1391927A (fr) * | 1964-01-29 | 1965-03-12 | Monsieur Le Ministre Des Armee | Chambre de combustion avec tuyère pour moteurs fusées à liquides |
GB1047552A (en) * | 1965-03-03 | 1966-11-09 | Rolls Royce | Exhaust duct for a gas turbine engine |
US3370794A (en) * | 1965-11-08 | 1968-02-27 | Navy Usa | Annular plenum nozzle for controlling trajectory of rockets |
US3467312A (en) * | 1966-02-10 | 1969-09-16 | Gen Electric | Ejector nozzle |
CH464625A (de) * | 1966-10-12 | 1968-10-31 | Sulzer Ag | Wellendichtung für ein Gebläse, insbesondere für das Umwälzgebläse einer gasgekühlten Kernreaktoranlage |
-
1970
- 1970-09-26 GB GB4597670A patent/GB1355190A/en not_active Expired
-
1971
- 1971-09-17 US US00181398A patent/US3729139A/en not_active Expired - Lifetime
- 1971-09-24 IT IT53079/71A patent/IT939465B/it active
- 1971-09-24 DE DE2147866A patent/DE2147866C2/de not_active Expired
- 1971-09-24 FR FR7134417A patent/FR2108507A5/fr not_active Expired
Also Published As
Publication number | Publication date |
---|---|
US3729139A (en) | 1973-04-24 |
DE2147866A1 (de) | 1972-04-06 |
GB1355190A (en) | 1974-06-05 |
FR2108507A5 (it) | 1972-05-19 |
DE2147866C2 (de) | 1982-04-29 |
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