IT1140119B - COMPRESSED AIR DISPENSER SYSTEM PARTICULARLY FOR GAS TURBO ENGINES - Google Patents
COMPRESSED AIR DISPENSER SYSTEM PARTICULARLY FOR GAS TURBO ENGINESInfo
- Publication number
- IT1140119B IT1140119B IT25537/81A IT2553781A IT1140119B IT 1140119 B IT1140119 B IT 1140119B IT 25537/81 A IT25537/81 A IT 25537/81A IT 2553781 A IT2553781 A IT 2553781A IT 1140119 B IT1140119 B IT 1140119B
- Authority
- IT
- Italy
- Prior art keywords
- compressed air
- dispenser system
- system particularly
- gas turbo
- air dispenser
- 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 IT8125537A0 (en) | 1981-12-11 |
IT1140119B true IT1140119B (en) | 1986-09-24 |
Family
ID=22818660
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
IT25537/81A IT1140119B (en) | 1980-12-22 | 1981-12-11 | COMPRESSED AIR DISPENSER SYSTEM PARTICULARLY FOR GAS TURBO ENGINES |
Country Status (5)
Country | Link |
---|---|
JP (1) | JPS57124619A (en) |
DE (1) | DE3149761A1 (en) |
FR (1) | FR2496763B1 (en) |
GB (1) | GB2089894B (en) |
IT (1) | IT1140119B (en) |
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 (en) * | 1985-10-04 | 1986-11-20 | MTU Motoren- und Turbinen-Union München GmbH, 8000 München | Combustion chamber for a gas turbine engine, especially an annular combustion chamber, with at least one air supply bushing |
FR2593237B1 (en) * | 1986-01-17 | 1989-09-01 | Hispano Suiza Sa | COLD FLOW CHANNEL OF MULTI-FLOW TURBOREACTOR DRIVE INVERTER ASSOCIATED WITH COMBINED AIR TAKE-OFF MEANS |
DE4210542A1 (en) * | 1992-03-31 | 1993-10-07 | Asea Brown Boveri | Gas-turbine with diffuser at pressure-wave machine outlet - recovers pressure separately from high- and low-speed portions of outflowing current |
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 (en) | 2021-04-26 | 2022-10-27 | Rolls-Royce Deutschland Ltd & Co Kg | Combustion chamber assembly for an engine with a pre-diffuser connected to a combustion chamber wall |
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 (en) * | 1958-07-31 | |||
GB911160A (en) * | 1958-09-01 | 1962-11-21 | Rolls Royce | Improvements in or relating to engines having gas compressors |
DE1181004B (en) * | 1959-03-11 | 1964-11-05 | Rolls Royce | Combustion chamber for gas turbine jet engines |
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 JP JP56198756A patent/JPS57124619A/en active Pending
- 1981-12-11 IT IT25537/81A patent/IT1140119B/en active
- 1981-12-16 DE DE19813149761 patent/DE3149761A1/en not_active Ceased
- 1981-12-22 FR FR8123920A patent/FR2496763B1/en not_active Expired
Also Published As
Publication number | Publication date |
---|---|
JPS57124619A (en) | 1982-08-03 |
DE3149761A1 (en) | 1982-07-22 |
GB2089894B (en) | 1985-08-14 |
IT8125537A0 (en) | 1981-12-11 |
FR2496763A1 (en) | 1982-06-25 |
GB2089894A (en) | 1982-06-30 |
FR2496763B1 (en) | 1988-04-08 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
TA | Fee payment date (situation as of event date), data collected since 19931001 |
Effective date: 19921216 |