IT1178575B - Sistema di controllo di aria particolarmente per turbomotore a gas - Google Patents
Sistema di controllo di aria particolarmente per turbomotore a gasInfo
- Publication number
- IT1178575B IT1178575B IT23209/84A IT2320984A IT1178575B IT 1178575 B IT1178575 B IT 1178575B IT 23209/84 A IT23209/84 A IT 23209/84A IT 2320984 A IT2320984 A IT 2320984A IT 1178575 B IT1178575 B IT 1178575B
- Authority
- IT
- Italy
- Prior art keywords
- control system
- air control
- system especially
- turbo engine
- gas turbo
- 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
- F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
- F02K3/02—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber
- F02K3/04—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type
- F02K3/077—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type the plant being of the multiple flow type, i.e. having three or more flows
-
- 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
- F02C6/00—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use
- F02C6/04—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output
- F02C6/06—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output providing compressed gas
- F02C6/08—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output providing compressed gas the gas being bled from the gas-turbine compressor
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US54759283A | 1983-10-31 | 1983-10-31 |
Publications (3)
Publication Number | Publication Date |
---|---|
IT8423209A0 IT8423209A0 (it) | 1984-10-18 |
IT8423209A1 IT8423209A1 (it) | 1986-04-18 |
IT1178575B true IT1178575B (it) | 1987-09-09 |
Family
ID=24185281
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
IT23209/84A IT1178575B (it) | 1983-10-31 | 1984-10-18 | Sistema di controllo di aria particolarmente per turbomotore a gas |
Country Status (5)
Country | Link |
---|---|
JP (1) | JPS60125732A (it) |
DE (1) | DE3439108A1 (it) |
FR (1) | FR2554169A1 (it) |
GB (1) | GB2149016A (it) |
IT (1) | IT1178575B (it) |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2192229B (en) * | 1986-07-04 | 1990-05-02 | Rolls Royce Plc | A compressor and air bleed system |
CA2013933A1 (en) * | 1989-06-05 | 1990-12-05 | General Electric Company | Gas turbine powerplant |
DE102012003902A1 (de) * | 2011-12-14 | 2013-06-20 | Istvan Bolgar | Einlauf für eine Gasturbine |
Family Cites Families (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB609322A (en) * | 1945-11-07 | 1948-09-29 | Power Jets Res & Dev Ltd | Improvements relating to axial-flow compressors and like machines, and blading thereof |
US2999631A (en) * | 1958-09-05 | 1961-09-12 | Gen Electric | Dual airfoil |
GB1291943A (en) * | 1970-02-11 | 1972-10-04 | Secr Defence | Improvements in or relating to ducted fans |
DE2149619A1 (de) * | 1971-10-05 | 1973-04-19 | Motoren Turbinen Union | Turbinenstrahltriebwerk fuer senkrechtoder kurzstartende bzw. landende flugzeuge |
US3777489A (en) * | 1972-06-01 | 1973-12-11 | Gen Electric | Combustor casing and concentric air bleed structure |
US4791783A (en) * | 1981-11-27 | 1988-12-20 | General Electric Company | Convertible aircraft engine |
-
1984
- 1984-09-05 GB GB08422469A patent/GB2149016A/en not_active Withdrawn
- 1984-10-18 IT IT23209/84A patent/IT1178575B/it active
- 1984-10-25 DE DE19843439108 patent/DE3439108A1/de not_active Withdrawn
- 1984-10-26 JP JP59224288A patent/JPS60125732A/ja active Pending
- 1984-10-31 FR FR8416630A patent/FR2554169A1/fr active Pending
Also Published As
Publication number | Publication date |
---|---|
IT8423209A0 (it) | 1984-10-18 |
IT8423209A1 (it) | 1986-04-18 |
GB8422469D0 (en) | 1984-10-10 |
JPS60125732A (ja) | 1985-07-05 |
FR2554169A1 (fr) | 1985-05-03 |
GB2149016A (en) | 1985-06-05 |
DE3439108A1 (de) | 1985-05-09 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
IT1135606B (it) | Sistema ausiliario di ventilazione per turbomotori a gas | |
IT1137928B (it) | Sistema di controllo di gioco per turbomotori a gas | |
IT1131511B (it) | Sistema di controllo per turbomotore a gas | |
IT1177449B (it) | Sistema di raffreddamento di componenti di turbomotore a gas | |
IT1208034B (it) | Distributore a vortice per un sistema di raffreddamento di turbomotori a gas. | |
IT1229146B (it) | Sistema di controllo dei giochi, particolarmente per turbomotori a gas | |
IT8620137A0 (it) | Sistema di controllo di aria particolarmente per motori di aereo. | |
IT8420753A0 (it) | Impianto di comando per motore a turbina a gas. | |
GB2126382B (en) | Gas turbine engine control system | |
LV10811A (lv) | Kaitigu izpludes gazu nepartauktas kontroles sistema lietojot masspektrometru | |
GB2174824B (en) | Control systems for gas turbine engines | |
GB2095335B (en) | Gas turbine engine air intake system | |
IT1141553B (it) | Sistema antighiaccio per ogiva di motore a turbina a gas | |
IT8521319A0 (it) | Sistema di controllo di turbomotore a gas. | |
IT1097195B (it) | Sistema di controllo integrato per un turbomotore a gas | |
IT1140119B (it) | Sistema dispensatore di aria compressa particolarmente per turbomotori a gas | |
IT8321994A0 (it) | Sistema di scarico di turboventilatore a flusso mescolato. | |
IT8747638A0 (it) | Sistema di controllo di combustibile per apparecchiatura di riscaldamento successivo per motori a turbina a gas | |
IT1178575B (it) | Sistema di controllo di aria particolarmente per turbomotore a gas | |
IT1183454B (it) | Sistema di controllo di aria di raffredamento per turbomotore a gas | |
IT1150489B (it) | Sistema di turbina a gas | |
IT1174123B (it) | Sistema di comando per inserire e disinserire un turbocompressore a gas di scarico | |
AU555268B2 (en) | Secondary air supply for i.c. engine exhaust system | |
IT1177240B (it) | Sistema di comando della valvola dell'aria su un bruciatore bistadio a soffiante per gasolio o gas | |
KR910009451U (ko) | 가스보일러의 공기배출 장치 |