FR2287601A1 - Dispositif de changement du pas pour un ventilateur de poussee carene - Google Patents
Dispositif de changement du pas pour un ventilateur de poussee careneInfo
- Publication number
- FR2287601A1 FR2287601A1 FR7530013A FR7530013A FR2287601A1 FR 2287601 A1 FR2287601 A1 FR 2287601A1 FR 7530013 A FR7530013 A FR 7530013A FR 7530013 A FR7530013 A FR 7530013A FR 2287601 A1 FR2287601 A1 FR 2287601A1
- Authority
- FR
- France
- Prior art keywords
- fairing
- change device
- pitch change
- thrust fan
- thrust
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
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
- F04D29/00—Details, component parts, or accessories
- F04D29/26—Rotors specially for elastic fluids
- F04D29/32—Rotors specially for elastic fluids for axial flow pumps
- F04D29/321—Rotors specially for elastic fluids for axial flow pumps for axial flow compressors
- F04D29/322—Blade mountings
- F04D29/323—Blade mountings adjustable
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D7/00—Rotors with blades adjustable in operation; Control thereof
-
- 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
- F02C7/36—Power transmission arrangements between the different shafts of the gas turbine plant, or between the gas-turbine plant and the power user
-
- 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
- F02K3/06—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 with front fan
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2220/00—Application
- F05D2220/30—Application in turbines
- F05D2220/36—Application in turbines specially adapted for the fan of turbofan engines
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2260/00—Function
- F05D2260/40—Transmission of power
- F05D2260/403—Transmission of power through the shape of the drive components
- F05D2260/4031—Transmission of power through the shape of the drive components as in toothed gearing
- F05D2260/40311—Transmission of power through the shape of the drive components as in toothed gearing of the epicyclical, planetary or differential type
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2260/00—Function
- F05D2260/50—Kinematic linkage, i.e. transmission of position
- F05D2260/56—Kinematic linkage, i.e. transmission of position using cams or eccentrics
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2260/00—Function
- F05D2260/70—Adjusting of angle of incidence or attack of rotating blades
- F05D2260/74—Adjusting of angle of incidence or attack of rotating blades by turning around an axis perpendicular the rotor centre line
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2260/00—Function
- F05D2260/70—Adjusting of angle of incidence or attack of rotating blades
- F05D2260/79—Bearing, support or actuation arrangements therefor
-
- 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)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US05/513,323 US4021142A (en) | 1974-10-09 | 1974-10-09 | Pitch-change apparatus for a ducted thrust fan |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2287601A1 true FR2287601A1 (fr) | 1976-05-07 |
FR2287601B1 FR2287601B1 (fr) | 1980-11-14 |
Family
ID=24042774
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR7530013A Granted FR2287601A1 (fr) | 1974-10-09 | 1975-10-01 | Dispositif de changement du pas pour un ventilateur de poussee carene |
Country Status (4)
Country | Link |
---|---|
US (1) | US4021142A (fr) |
JP (1) | JPS5164604A (fr) |
FR (1) | FR2287601A1 (fr) |
GB (1) | GB1521545A (fr) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN114435585A (zh) * | 2022-01-28 | 2022-05-06 | 清华大学 | 可变桨距风扇及其变距方法 |
Families Citing this family (19)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4717610A (en) * | 1987-02-02 | 1988-01-05 | United Technologies Corporation | Composite disk for supporting fan blades |
US5282719A (en) * | 1991-05-13 | 1994-02-01 | Alliedsignal Inc. | Quad mode fan pitch actuation system for a gas turbine engine |
US5205712A (en) * | 1991-05-13 | 1993-04-27 | Allied-Signal Inc. | Variable pitch fan gas turbine engine |
US7901185B2 (en) * | 2007-02-21 | 2011-03-08 | United Technologies Corporation | Variable rotor blade for gas turbine engine |
US8336289B2 (en) | 2007-08-30 | 2012-12-25 | United Technologies Corporation | Gas turbine engine systems and related methods involving multiple gas turbine cores |
US8590286B2 (en) * | 2007-12-05 | 2013-11-26 | United Technologies Corp. | Gas turbine engine systems involving tip fans |
US8402742B2 (en) | 2007-12-05 | 2013-03-26 | United Technologies Corporation | Gas turbine engine systems involving tip fans |
CN102066768A (zh) * | 2008-05-13 | 2011-05-18 | 旋转合成技术有限责任公司 | 风扇叶片保持和可变桨距系统 |
CA2751805A1 (fr) * | 2009-02-27 | 2010-09-02 | Snecma | Aubes de soufflante a calage cyclique |
FR2945512B1 (fr) * | 2009-05-15 | 2012-08-24 | Snecma | Helice non carenee a pales a calage variable pour une turbomachine |
DE102013012844B3 (de) * | 2013-08-02 | 2014-11-20 | Voith Patent Gmbh | Turbine für ein Strömungskraftwerk |
US9835037B2 (en) * | 2015-06-22 | 2017-12-05 | General Electric Company | Ducted thrust producing system with asynchronous fan blade pitching |
US10107130B2 (en) * | 2016-03-24 | 2018-10-23 | United Technologies Corporation | Concentric shafts for remote independent variable vane actuation |
US11421627B2 (en) * | 2017-02-22 | 2022-08-23 | General Electric Company | Aircraft and direct drive engine under wing installation |
US10934866B2 (en) | 2017-06-20 | 2021-03-02 | Rolls-Royce North American Technologies Inc. | Variable pitch change control method |
US10801339B2 (en) * | 2017-07-11 | 2020-10-13 | General Electric Company | Aircraft gas turbine engine variable fan blade mechanism |
GB201807774D0 (en) * | 2018-05-14 | 2018-06-27 | Rolls Royce Plc | Hybrid aircraft propulsion system |
US11428160B2 (en) | 2020-12-31 | 2022-08-30 | General Electric Company | Gas turbine engine with interdigitated turbine and gear assembly |
FR3125505B1 (fr) * | 2021-07-22 | 2023-07-21 | Safran Aircraft Engines | Systeme de changement de pas des pales d’une helice d’une turbomachine |
Family Cites Families (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1582166A (en) * | 1922-08-21 | 1926-04-27 | Cederquist Nils Herman | Variable-pitch propeller |
FR798405A (fr) * | 1934-12-06 | 1936-05-16 | Aeroplani Caproni | Perfectionnements aux hélices à pas variable |
GB456407A (en) * | 1935-03-23 | 1936-11-09 | Istvan Dobos | Improvements in or relating to screw propellers |
GB753237A (en) * | 1953-11-13 | 1956-07-18 | English Electric Co Ltd | Improvements in and relating to the control of feathering runner vanes of hydraulic turbines and pumps |
DE1012869B (de) * | 1956-05-11 | 1957-07-25 | Arno Fischer | Verstellantrieb fuer die Schaufeln von Stroemungsmaschinen |
DE1626028C3 (de) * | 1966-04-12 | 1974-04-04 | Dowty Rotol Ltd., Gloucester (Grossbritannien) | Mantelstrom-Gasturbinen-Triebwerk |
GB1371371A (en) * | 1971-04-27 | 1974-10-23 | Defence Secretary Of States Fo | Variable pitch fans or propellers particularly for gas turbine engines |
US3801219A (en) * | 1971-05-05 | 1974-04-02 | Jerome A Gross | Controllable pitch maripropeller |
-
1974
- 1974-10-09 US US05/513,323 patent/US4021142A/en not_active Expired - Lifetime
-
1975
- 1975-10-01 FR FR7530013A patent/FR2287601A1/fr active Granted
- 1975-10-07 JP JP50121201A patent/JPS5164604A/ja active Pending
- 1975-10-08 GB GB41224/75A patent/GB1521545A/en not_active Expired
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN114435585A (zh) * | 2022-01-28 | 2022-05-06 | 清华大学 | 可变桨距风扇及其变距方法 |
Also Published As
Publication number | Publication date |
---|---|
US4021142A (en) | 1977-05-03 |
GB1521545A (en) | 1978-08-16 |
JPS5164604A (fr) | 1976-06-04 |
FR2287601B1 (fr) | 1980-11-14 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
ST | Notification of lapse |