IT8125537A0 - Sistema dispensatore di aria compressa particolarmente per turbomotori a gas. - Google Patents
Sistema dispensatore di aria compressa particolarmente per turbomotori a gas.Info
- Publication number
- IT8125537A0 IT8125537A0 IT8125537A IT2553781A IT8125537A0 IT 8125537 A0 IT8125537 A0 IT 8125537A0 IT 8125537 A IT8125537 A IT 8125537A IT 2553781 A IT2553781 A IT 2553781A IT 8125537 A0 IT8125537 A0 IT 8125537A0
- Authority
- IT
- Italy
- Prior art keywords
- compressed air
- dispensing system
- system particularly
- gas turbo
- air dispensing
- Prior art date
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
- F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/12—Cooling of plants
- F02C7/16—Cooling of plants characterised by cooling medium
- F02C7/18—Cooling of plants characterised by cooling medium the medium being gaseous, e.g. air
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Supercharger (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US21928680A | 1980-12-22 | 1980-12-22 |
Publications (2)
Publication Number | Publication Date |
---|---|
IT8125537A0 true IT8125537A0 (it) | 1981-12-11 |
IT1140119B IT1140119B (it) | 1986-09-24 |
Family
ID=22818660
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
IT25537/81A IT1140119B (it) | 1980-12-22 | 1981-12-11 | Sistema dispensatore di aria compressa particolarmente per turbomotori a gas |
Country Status (5)
Country | Link |
---|---|
JP (1) | JPS57124619A (it) |
DE (1) | DE3149761A1 (it) |
FR (1) | FR2496763B1 (it) |
GB (1) | GB2089894B (it) |
IT (1) | IT1140119B (it) |
Families Citing this family (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4852355A (en) * | 1980-12-22 | 1989-08-01 | General Electric Company | Dispensing arrangement for pressurized air |
US4527386A (en) * | 1983-02-28 | 1985-07-09 | United Technologies Corporation | Diffuser for gas turbine engine |
DE3535443C1 (de) * | 1985-10-04 | 1986-11-20 | MTU Motoren- und Turbinen-Union München GmbH, 8000 München | Brennkammer fuer ein Gasturbinentriebwerk,insbesondere Ringbrennkammer,mit mindestes einer Luftzufuhrbuchse |
FR2593237B1 (fr) * | 1986-01-17 | 1989-09-01 | Hispano Suiza Sa | Canal a flux froid d'inverseur de poussee de turboreacteur multiflux associe a des moyens combines de prelevements d'air |
DE4210542A1 (de) * | 1992-03-31 | 1993-10-07 | Asea Brown Boveri | Gasturbine |
US8381526B2 (en) | 2010-02-15 | 2013-02-26 | General Electric Company | Systems and methods of providing high pressure air to a head end of a combustor |
DE102021110617A1 (de) | 2021-04-26 | 2022-10-27 | Rolls-Royce Deutschland Ltd & Co Kg | Brennkammerbaugruppe für ein Triebwerk mit einer Brennkammerwand verbundenem Pre-Diffusor |
US11692493B1 (en) * | 2022-05-05 | 2023-07-04 | Raytheon Technologies Corporation | Fluidic valve configuration for boost spool engine |
US11976598B2 (en) | 2022-05-05 | 2024-05-07 | Rtx Corporation | Transmission and method for control of boost spool |
US11898490B2 (en) | 2022-05-05 | 2024-02-13 | Rtx Corporation | Transmission and method for control of boost spool |
Family Cites Families (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
NL108658C (it) * | 1958-07-31 | |||
GB911160A (en) * | 1958-09-01 | 1962-11-21 | Rolls Royce | Improvements in or relating to engines having gas compressors |
DE1181004B (de) * | 1959-03-11 | 1964-11-05 | Rolls Royce | Brennkammer fuer Gasturbinenstrahltriebwerke |
GB1033922A (en) * | 1962-05-15 | 1966-06-22 | Bristol Siddeley Engines Ltd | Improvements in diffusers for gaseous fluids |
US3581492A (en) * | 1969-07-08 | 1971-06-01 | Nasa | Gas turbine combustor |
CA939521A (en) * | 1970-04-28 | 1974-01-08 | Bruce R. Branstrom | Turbine coolant flow system |
US3826084A (en) * | 1970-04-28 | 1974-07-30 | United Aircraft Corp | Turbine coolant flow system |
GB1581531A (en) * | 1976-09-09 | 1980-12-17 | Rolls Royce | Control of airflow in combustion chambers by variable rate diffuser |
-
1981
- 1981-11-25 GB GB8135509A patent/GB2089894B/en not_active Expired
- 1981-12-11 IT IT25537/81A patent/IT1140119B/it active
- 1981-12-11 JP JP56198756A patent/JPS57124619A/ja active Pending
- 1981-12-16 DE DE19813149761 patent/DE3149761A1/de not_active Ceased
- 1981-12-22 FR FR8123920A patent/FR2496763B1/fr not_active Expired
Also Published As
Publication number | Publication date |
---|---|
FR2496763A1 (fr) | 1982-06-25 |
GB2089894A (en) | 1982-06-30 |
DE3149761A1 (de) | 1982-07-22 |
GB2089894B (en) | 1985-08-14 |
FR2496763B1 (fr) | 1988-04-08 |
IT1140119B (it) | 1986-09-24 |
JPS57124619A (en) | 1982-08-03 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
IT8119944A0 (it) | Sistema ausiliario di ventilazione per turbomotori a gas. | |
IT1137928B (it) | Sistema di controllo di gioco per turbomotori a gas | |
IT8022083A0 (it) | Sistema di controllo per turbomotore a gas. | |
GB2108202B (en) | Air cooling systems for gas turbine engines | |
IT8019933A0 (it) | Sistema di bilanciamento programmabile ad aria sottopressione per un manipolatore. | |
IT8424116A0 (it) | Sistema di raffreddamento di componenti di turbomotore a gas. | |
IT8220759A0 (it) | Sistema di rifornimento dicombustibile per turbina a gas. | |
IT8125507A0 (it) | Chiodatrice ad aria compressa. | |
IT7819829A0 (it) | Sistema di controllo per un motore a turbina a gas. | |
DE69300239D1 (de) | Gasturbine kombiniert mit Lufttrennungsanlage. | |
ITMI922189A1 (it) | Sistema di combustione a basse emissioni inquinanti per turbine a gas | |
DK15581A (da) | Ventilsystem til kapslede motorkompressorenheder | |
GB2095335B (en) | Gas turbine engine air intake system | |
IT8021276A0 (it) | Sistema antighiaccio per ogiva di motore a turbina a gas. | |
IT8125537A0 (it) | Sistema dispensatore di aria compressa particolarmente per turbomotori a gas. | |
IT8025428A0 (it) | Sistema di controllo di carico ciclico per turbina a gas. | |
IT1130186B (it) | Sistema di combustione per turbina a gas a doppio stadio/doppio modo di funzionamento | |
IT7922830A0 (it) | Sistema di alimentazione di aria di raffreddamento per motore a turbina a gas. | |
IT1063518B (it) | Sistema di utilizzazione della perdita di aria di raffreddamento in un turbomotore a gas | |
IT8222415A0 (it) | Silenziatore da usare su dispositivi azionati da aria compressa. | |
IT7825923A0 (it) | Sistema di controllo integrato per un turbomotore a gas. | |
IT8021845A0 (it) | Sistema di controllo perl'avviamento di un motore a turbina a gas. | |
IT8119377A0 (it) | Presa d'aria per motore a turbina a gas. | |
IT8521319A0 (it) | Sistema di controllo di turbomotore a gas. | |
DE69006868D1 (de) | Gasturbinenluftstrahltriebwerk. |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
TA | Fee payment date (situation as of event date), data collected since 19931001 |
Effective date: 19921216 |