IT993227B - Apparato per scaricare aria uscente da compressori in propulsori a turbogetto - Google Patents
Apparato per scaricare aria uscente da compressori in propulsori a turbogettoInfo
- Publication number
- IT993227B IT993227B IT28845/73A IT2884573A IT993227B IT 993227 B IT993227 B IT 993227B IT 28845/73 A IT28845/73 A IT 28845/73A IT 2884573 A IT2884573 A IT 2884573A IT 993227 B IT993227 B IT 993227B
- Authority
- IT
- Italy
- Prior art keywords
- turboget
- thrusters
- compressors
- outlet air
- discharging outlet
- Prior art date
Links
- 238000007599 discharging Methods 0.000 title 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D27/00—Control, e.g. regulation, of pumps, pumping installations or pumping systems specially adapted for elastic fluids
- F04D27/02—Surge control
- F04D27/0207—Surge control by bleeding, bypassing or recycling fluids
- F04D27/0215—Arrangements therefor, e.g. bleed or by-pass valves
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D27/00—Control, e.g. regulation, of pumps, pumping installations or pumping systems specially adapted for elastic fluids
- F04D27/02—Surge control
- F04D27/0207—Surge control by bleeding, bypassing or recycling fluids
- F04D27/023—Details or means for fluid extraction
Landscapes
- Engineering & Computer Science (AREA)
- Life Sciences & Earth Sciences (AREA)
- Sustainable Development (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Supercharger (AREA)
- Taps Or Cocks (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE2247400A DE2247400C2 (de) | 1972-09-27 | 1972-09-27 | Vorrichtung zum Abblasen von verdichteter Luft aus einem Verdichter eines Gasturbinenstrahltriebwerks |
Publications (1)
Publication Number | Publication Date |
---|---|
IT993227B true IT993227B (it) | 1975-09-30 |
Family
ID=5857538
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
IT28845/73A IT993227B (it) | 1972-09-27 | 1973-09-12 | Apparato per scaricare aria uscente da compressori in propulsori a turbogetto |
Country Status (5)
Country | Link |
---|---|
US (1) | US3898799A (fr) |
DE (1) | DE2247400C2 (fr) |
FR (1) | FR2209044B1 (fr) |
GB (1) | GB1445415A (fr) |
IT (1) | IT993227B (fr) |
Families Citing this family (28)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4055946A (en) * | 1976-03-29 | 1977-11-01 | United Technologies Corporation | Twin-spool gas turbine power plant with means to spill compressor interstage airflow |
US4086761A (en) * | 1976-04-26 | 1978-05-02 | The Boeing Company | Stator bypass system for turbofan engine |
DE2740904A1 (de) * | 1977-09-10 | 1979-03-22 | Motoren Turbinen Union | Vorrichtung zur betaetigung von absperrorganen in gasturbinentriebwerken, insbesondere gasturbinenstrahltriebwerken |
US4232513A (en) * | 1977-10-19 | 1980-11-11 | Rolls-Royce Limited | Pressure relief panel for aircraft powerplant |
IL59497A (en) * | 1979-04-23 | 1984-08-31 | Gen Electric | Valve actuation system for use on a gas turbine engine |
US4463552A (en) * | 1981-12-14 | 1984-08-07 | United Technologies Corporation | Combined surge bleed and dust removal system for a fan-jet engine |
US5136840A (en) * | 1982-09-30 | 1992-08-11 | General Electric Company | Gas turbine engine actuation system |
US4546605A (en) * | 1983-12-16 | 1985-10-15 | United Technologies Corporation | Heat exchange system |
US4698964A (en) * | 1985-09-06 | 1987-10-13 | The Boeing Company | Automatic deflector for a jet engine bleed air exhaust system |
US4827713A (en) * | 1987-06-29 | 1989-05-09 | United Technologies Corporation | Stator valve assembly for a rotary machine |
FR2640685B1 (fr) * | 1988-12-15 | 1991-02-08 | Snecma | Vanne de decharge de compresseur de turboreacteur |
US5177914A (en) * | 1989-06-19 | 1993-01-12 | Hilmer Elwyn P | Vertical section building construction |
US5231825A (en) * | 1990-04-09 | 1993-08-03 | General Electric Company | Method for compressor air extraction |
CA2048829C (fr) * | 1990-11-19 | 2001-12-18 | William Francis Mcgreehan | Fente de purge pour compresseur haute pression |
US5209633A (en) * | 1990-11-19 | 1993-05-11 | General Electric Company | High pressure compressor flowpath bleed valve extraction slot |
US5287697A (en) * | 1992-01-02 | 1994-02-22 | General Electric Company | Variable area bypass injector seal |
US5211003A (en) * | 1992-02-05 | 1993-05-18 | General Electric Company | Diffuser clean air bleed assembly |
GB2264984A (en) * | 1992-03-12 | 1993-09-15 | Bmw Rolls Royce Gmbh | A device for adjusting gas turbine guide vanes. |
US5380151A (en) * | 1993-10-13 | 1995-01-10 | Pratt & Whitney Canada, Inc. | Axially opening cylindrical bleed valve |
US5477673A (en) * | 1994-08-10 | 1995-12-26 | Pratt & Whitney Canada Inc. | Handling bleed valve |
US6048171A (en) * | 1997-09-09 | 2000-04-11 | United Technologies Corporation | Bleed valve system |
EP0936357B1 (fr) * | 1998-02-13 | 2003-11-05 | Pratt & Whitney Canada Corp. | Turbine à gaz |
US6122905A (en) * | 1998-02-13 | 2000-09-26 | Pratt & Whitney Canada Corp. | Compressor bleed valve |
DE19907907A1 (de) * | 1999-02-24 | 2000-08-31 | Abb Alstom Power Ch Ag | Mehrstufiger Turboverdichter |
US6742324B2 (en) * | 2002-09-13 | 2004-06-01 | General Electric Company | Methods and apparatus for supporting variable bypass valve systems |
US8388313B2 (en) * | 2009-11-05 | 2013-03-05 | General Electric Company | Extraction cavity wing seal |
US20130170966A1 (en) * | 2012-01-04 | 2013-07-04 | General Electric Company | Turbine cooling system |
US20230228219A1 (en) * | 2022-01-18 | 2023-07-20 | General Electric Company | Bleed valve assemblies |
Family Cites Families (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3030006A (en) * | 1958-05-27 | 1962-04-17 | United Aircraft Corp | Circumferential bleed valve |
US3057541A (en) * | 1958-06-03 | 1962-10-09 | United Aircraft Corp | Circumferential bleed valve |
US3094270A (en) * | 1958-08-05 | 1963-06-18 | Rolls Royce | Annular valve device |
NL251063A (fr) * | 1959-04-30 | 1900-01-01 | ||
US3688504A (en) * | 1970-11-27 | 1972-09-05 | Gen Electric | Bypass valve control |
GB1365491A (en) * | 1971-01-02 | 1974-09-04 | Dowty Rotol Ltd | Gas turbine ducted fan engines and fans therefor |
US3777489A (en) * | 1972-06-01 | 1973-12-11 | Gen Electric | Combustor casing and concentric air bleed structure |
-
1972
- 1972-09-27 DE DE2247400A patent/DE2247400C2/de not_active Expired
-
1973
- 1973-09-12 IT IT28845/73A patent/IT993227B/it active
- 1973-09-18 GB GB4384773A patent/GB1445415A/en not_active Expired
- 1973-09-27 FR FR7334718A patent/FR2209044B1/fr not_active Expired
- 1973-09-27 US US401544A patent/US3898799A/en not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
US3898799A (en) | 1975-08-12 |
FR2209044B1 (fr) | 1980-11-07 |
DE2247400C2 (de) | 1975-01-16 |
GB1445415A (en) | 1976-08-11 |
DE2247400B1 (de) | 1974-05-16 |
FR2209044A1 (fr) | 1974-06-28 |
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