SE8002886L - Anordning for partikelseparation och avisning vid gasturbinmotor for flygplan - Google Patents
Anordning for partikelseparation och avisning vid gasturbinmotor for flygplanInfo
- Publication number
- SE8002886L SE8002886L SE8002886A SE8002886A SE8002886L SE 8002886 L SE8002886 L SE 8002886L SE 8002886 A SE8002886 A SE 8002886A SE 8002886 A SE8002886 A SE 8002886A SE 8002886 L SE8002886 L SE 8002886L
- Authority
- SE
- Sweden
- Prior art keywords
- airboard
- deficiency
- department
- gas turbine
- turbine engine
- Prior art date
Links
- 230000007812 deficiency Effects 0.000 title 1
- RLQJEEJISHYWON-UHFFFAOYSA-N flonicamid Chemical compound FC(F)(F)C1=CC=NC=C1C(=O)NCC#N RLQJEEJISHYWON-UHFFFAOYSA-N 0.000 title 1
- 239000002245 particle Substances 0.000 title 1
- 238000000926 separation method Methods 0.000 title 1
Classifications
-
- 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
- F02C7/04—Air intakes for gas-turbine plants or jet-propulsion plants
- F02C7/05—Air intakes for gas-turbine plants or jet-propulsion plants having provisions for obviating the penetration of damaging objects or particles
- F02C7/052—Air intakes for gas-turbine plants or jet-propulsion plants having provisions for obviating the penetration of damaging objects or particles with dust-separation devices
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D33/00—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
- B64D33/02—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
-
- 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
- F02C7/04—Air intakes for gas-turbine plants or jet-propulsion plants
- F02C7/05—Air intakes for gas-turbine plants or jet-propulsion plants having provisions for obviating the penetration of damaging objects or particles
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D33/00—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
- B64D33/02—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
- B64D2033/0233—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes comprising de-icing means
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D33/00—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
- B64D33/02—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
- B64D2033/0246—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes comprising particle separators
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Separating Particles In Gases By Inertia (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Cooling, Air Intake And Gas Exhaust, And Fuel Tank Arrangements In Propulsion Units (AREA)
- Cyclones (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US06/021,422 US4250703A (en) | 1979-03-15 | 1979-03-15 | Swinging door particle separator and deicing system |
Publications (2)
Publication Number | Publication Date |
---|---|
SE8002886L true SE8002886L (sv) | 1981-10-18 |
SE421232B SE421232B (sv) | 1981-12-07 |
Family
ID=21804135
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
SE8002886A SE421232B (sv) | 1979-03-15 | 1980-04-17 | Anordning for partikelseparation och avisning vid gasturbiner for flygplan |
Country Status (6)
Country | Link |
---|---|
US (1) | US4250703A (sv) |
CA (1) | CA1120733A (sv) |
DE (1) | DE3015651C2 (sv) |
FR (1) | FR2481746A1 (sv) |
GB (1) | GB2074655B (sv) |
SE (1) | SE421232B (sv) |
Families Citing this family (50)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CA1116418A (en) * | 1979-07-18 | 1982-01-19 | Pratt & Whitney Aircraft Of Canada Limited | Vane fairing for inertial separator |
US4397431A (en) * | 1981-11-02 | 1983-08-09 | Avco Corporation | Fail-safe, anti-icing system for aircraft engines |
US4713934A (en) * | 1981-11-21 | 1987-12-22 | Rolls-Royce Plc | Gas turbine engine air intake |
US4844382A (en) * | 1983-10-19 | 1989-07-04 | Raisbeck Engineering, Inc. | Dual turning vane air inlet assembly |
US4617028A (en) * | 1983-11-03 | 1986-10-14 | General Electric Company | Aircraft engine air intake including a foreign object separator |
US4674704A (en) * | 1985-12-03 | 1987-06-23 | The United States Of America As Represented By The Secretary Of The Air Force | Direct air cooling system for airborne electronics |
US4760978A (en) * | 1986-11-19 | 1988-08-02 | Cox & Company, Inc. | Ice-free screen for protecting engines from damage caused by foreign bodies in the intake airstream |
US5088660A (en) * | 1989-08-04 | 1992-02-18 | United Technologies Corporation | Bleed stability door |
US4972672A (en) * | 1989-09-28 | 1990-11-27 | Pratt & Whitney Canada, Inc. | Controlled bypass inlet duct |
US5123240A (en) * | 1990-03-19 | 1992-06-23 | General Electric Co. | Method and apparatus for ejecting foreign matter from the primary flow path of a gas turbine engine |
US5284012A (en) * | 1991-05-16 | 1994-02-08 | General Electric Company | Nacelle cooling and ventilation system |
GB2259328B (en) * | 1991-09-03 | 1995-07-19 | Gen Electric | Gas turbine engine variable bleed pivotal flow splitter |
US5961067A (en) * | 1996-09-10 | 1999-10-05 | Allison Engine Company | Method for reducing turboprop noise |
US6651929B2 (en) * | 2001-10-29 | 2003-11-25 | Pratt & Whitney Canada Corp. | Passive cooling system for auxiliary power unit installation |
DE10162238A1 (de) * | 2001-12-18 | 2003-07-10 | Rolls Royce Deutschland | Lufteinlasssystem eines PTL-Antriebs |
US6702873B2 (en) | 2002-04-23 | 2004-03-09 | The Boeing Company | High particle separation efficiency system |
GB0617769D0 (en) * | 2006-09-09 | 2006-10-18 | Rolls Royce Plc | An engine |
FR2915461B1 (fr) * | 2007-04-24 | 2009-06-05 | Airbus France Sas | Agencement d'entree d'air pour vehicule, notamment un aeronef. |
US8079550B2 (en) * | 2008-07-18 | 2011-12-20 | Hamilton Sundstrand Corporation | Auxiliary power unit inlet door actuation mechanism |
WO2010077241A1 (en) | 2008-12-30 | 2010-07-08 | Sikorsky Aircraft Corporation | Engine air particle separator |
US20120070271A1 (en) | 2010-09-21 | 2012-03-22 | Urban Justin R | Gas turbine engine with bleed duct for minimum reduction of bleed flow and minimum rejection of hail during hail ingestion events |
US8935926B2 (en) | 2010-10-28 | 2015-01-20 | United Technologies Corporation | Centrifugal compressor with bleed flow splitter for a gas turbine engine |
US8945254B2 (en) | 2011-12-21 | 2015-02-03 | General Electric Company | Gas turbine engine particle separator |
US9067679B2 (en) * | 2011-12-30 | 2015-06-30 | Aerospace Filtration Systems, Inc. | Heated screen for air intake of aircraft engines |
US8452516B1 (en) | 2012-01-31 | 2013-05-28 | United Technologies Corporation | Variable vane scheduling based on flight conditions for inclement weather |
USD722879S1 (en) | 2012-06-14 | 2015-02-24 | S.C. Johnson & Son, Inc. | Bottle |
USD736089S1 (en) | 2012-06-14 | 2015-08-11 | S.C. Johnson & Son, Inc. | Bottle |
USD736637S1 (en) | 2012-06-14 | 2015-08-18 | S.C. Johnson & Son, Inc. | Bottle |
US9518513B2 (en) | 2012-10-12 | 2016-12-13 | General Electric Company | Gas turbine engine two degree of freedom variable bleed valve for ice extraction |
US9982598B2 (en) | 2012-10-22 | 2018-05-29 | General Electric Company | Gas turbine engine variable bleed valve for ice extraction |
US9644537B2 (en) * | 2013-03-14 | 2017-05-09 | United Technologies Corporation | Free stream intake with particle separator for reverse core engine |
FR3009022B1 (fr) * | 2013-07-23 | 2018-03-16 | Safran Aircraft Engines | Moyeu de carter intermediaire pour turboreacteur d'aeronef comprenant des portes a geometrie profilee |
US9394827B2 (en) | 2013-08-07 | 2016-07-19 | Honeywell International Inc. | Inlet particle separator system with flow passage through hub and/or shroud |
EP2957503B1 (en) * | 2014-06-19 | 2016-08-17 | AIRBUS HELICOPTERS DEUTSCHLAND GmbH | Aircraft with two engines having by-pass air inlet openings and bleed air outlets as well as engine for an aircraft |
US9951690B2 (en) | 2014-08-19 | 2018-04-24 | Pratt & Whitney Canada Corp. | Low noise aeroengine inlet system |
US10221764B2 (en) | 2014-08-19 | 2019-03-05 | Pratt & Whitney Canada Corp. | Variable geometry inlet system |
US9957889B2 (en) | 2014-08-19 | 2018-05-01 | Pratt & Whitney Canada Corp. | Low noise aeroengine inlet system |
US10054050B2 (en) * | 2014-08-19 | 2018-08-21 | Pratt & Whitney Canada Corp. | Low noise aeroengine inlet system |
DE102014217829A1 (de) * | 2014-09-05 | 2016-03-10 | Rolls-Royce Deutschland Ltd & Co Kg | Verfahren zur Entnahme von Zapfluft und Flugzeugtriebwerk mit mindestens einer Vorrichtung zur Entnahme von Zapfluft |
FR3028289B1 (fr) * | 2014-11-06 | 2019-12-27 | Airbus Operations (S.A.S.) | Turbomachine d'aeronef comprenant un boitier d'admission d'air a profil aerodynamique variable |
GB201421773D0 (en) * | 2014-12-08 | 2015-01-21 | Rolls Royce Deutschland | Air intake arrangement |
US9719352B2 (en) | 2014-12-17 | 2017-08-01 | Honeywell International Inc. | Compartment based inlet particle separator system |
US10100734B2 (en) * | 2015-02-24 | 2018-10-16 | Honeywell International Inc. | Multi-channel particle separator |
US10138904B2 (en) | 2016-01-06 | 2018-11-27 | Honeywell International Inc. | Inlet particle separator system with high curvature hub |
USD845135S1 (en) | 2017-02-24 | 2019-04-09 | S. C. Johnson & Son, Inc. | Bottle neck with cap |
US11111024B2 (en) | 2018-01-12 | 2021-09-07 | Honeywell International Inc. | Foldable RAM air inlet filter |
US11525398B2 (en) * | 2019-04-02 | 2022-12-13 | The Boeing Company | Engine inlet with deployable particle separator |
US12043400B2 (en) * | 2022-03-29 | 2024-07-23 | Toyota Motor Engineering & Manufacturing North America, Inc. | Cooling system for aircraft components including ram chute body and relatively rotatable air conduit |
EP4292941A1 (en) * | 2022-06-15 | 2023-12-20 | Zero Emissions Aerospace Limited | Aircraft fuel cell air supply anti contamination system |
US12018615B2 (en) | 2022-10-31 | 2024-06-25 | Pratt & Whitney Canada Corp. | Systems and methods for controlling an air flow rate for a propulsion system air intake |
Family Cites Families (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
NL100160C (sv) * | 1955-03-11 | |||
GB571281A (en) * | 1942-05-01 | 1945-08-17 | United Aircraft Corp | Improvements in or relating to air ducts |
US2381705A (en) * | 1942-06-11 | 1945-08-07 | Vokes Cecil Gordon | Filter |
US2623610A (en) * | 1949-10-25 | 1952-12-30 | Gen Electric | Air inlet screen for gas turbines |
US2970431A (en) * | 1959-01-02 | 1961-02-07 | Curtiss Wright Corp | Rotating inlet for jet engines |
US3329377A (en) * | 1965-10-11 | 1967-07-04 | United Aircraft Canada | Protection for aircraft engines against snow, ice and airborne particles |
US3338049A (en) * | 1966-02-01 | 1967-08-29 | Gen Electric | Gas turbine engine including separator for removing extraneous matter |
US3952972A (en) * | 1974-12-24 | 1976-04-27 | United Aircraft Of Canada Limited | Inertial separator |
-
1979
- 1979-03-15 US US06/021,422 patent/US4250703A/en not_active Expired - Lifetime
-
1980
- 1980-04-16 CA CA000349981A patent/CA1120733A/en not_active Expired
- 1980-04-17 SE SE8002886A patent/SE421232B/sv unknown
- 1980-04-21 DE DE3015651A patent/DE3015651C2/de not_active Expired
- 1980-04-21 GB GB8013020A patent/GB2074655B/en not_active Expired
- 1980-04-30 FR FR8009771A patent/FR2481746A1/fr not_active Withdrawn
Also Published As
Publication number | Publication date |
---|---|
SE421232B (sv) | 1981-12-07 |
DE3015651C2 (de) | 1983-03-03 |
CA1120733A (en) | 1982-03-30 |
DE3015651A1 (de) | 1981-10-29 |
GB2074655A (en) | 1981-11-04 |
US4250703A (en) | 1981-02-17 |
FR2481746A1 (fr) | 1981-11-06 |
GB2074655B (en) | 1983-06-29 |
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