BE820543A - Moteur a turbo soufflante a pas variable - Google Patents
Moteur a turbo soufflante a pas variableInfo
- Publication number
- BE820543A BE820543A BE149074A BE149074A BE820543A BE 820543 A BE820543 A BE 820543A BE 149074 A BE149074 A BE 149074A BE 149074 A BE149074 A BE 149074A BE 820543 A BE820543 A BE 820543A
- Authority
- BE
- Belgium
- Prior art keywords
- variable step
- turbo motor
- step blower
- blower turbo
- motor
- Prior art date
Links
Classifications
-
- 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
- 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
- F05D2260/70—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
- F05D2260/76—Adjusting of angle of incidence or attack of rotating blades the adjusting mechanism using auxiliary power sources
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Control Of Turbines (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US402067A US3873235A (en) | 1973-10-01 | 1973-10-01 | Variable pitch turbofan engine |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| BE820543A true BE820543A (fr) | 1975-01-16 |
Family
ID=23590375
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| BE149074A BE820543A (fr) | 1973-10-01 | 1974-09-30 | Moteur a turbo soufflante a pas variable |
Country Status (8)
| Country | Link |
|---|---|
| US (1) | US3873235A (fr) |
| JP (1) | JPS5924259B2 (fr) |
| BE (1) | BE820543A (fr) |
| CA (1) | CA1015276A (fr) |
| DE (1) | DE2446527A1 (fr) |
| FR (1) | FR2246743A1 (fr) |
| GB (3) | GB1484685A (fr) |
| IT (1) | IT1022364B (fr) |
Families Citing this family (31)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3912418A (en) * | 1974-10-01 | 1975-10-14 | United Technologies Corp | Lubrication system for a rotor |
| FR2309744A1 (fr) * | 1975-04-30 | 1976-11-26 | Ratier Sa Forest | Dispositif de commande de variation du pas des pales d'un ventilateur |
| US3994128A (en) * | 1975-05-21 | 1976-11-30 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Dual output variable pitch turbofan actuation system |
| US4657484A (en) * | 1984-09-04 | 1987-04-14 | General Electric Company | Blade pitch varying means |
| JPS62192868U (fr) * | 1986-05-26 | 1987-12-08 | ||
| US4753572A (en) * | 1986-10-02 | 1988-06-28 | United Technologies Corporation | Propeller pitch change actuation system |
| US4750862A (en) * | 1986-11-28 | 1988-06-14 | United Technologies Corporation | Modular propeller blade pitch actuation system |
| US4718823A (en) * | 1987-02-24 | 1988-01-12 | United Technologies Corporation | Pitch changing mechanism for fan blades |
| US5211539A (en) * | 1991-05-13 | 1993-05-18 | Allied-Signal Inc. | Apparatus for indicating the pitch of turbofan blades |
| US5186608A (en) * | 1991-10-25 | 1993-02-16 | United Technologies Corporation | Hydraulic low pitch switch for propeller pitch change system |
| GB2465575A (en) * | 2008-11-21 | 2010-05-26 | Rolls Royce Plc | Displacement measurement / rotor blade pitch measurement arrangement |
| CA2784674C (fr) * | 2009-12-18 | 2018-03-20 | Flexxaire Inc. | Ventilateur a pas variable comportant un capteur de pas |
| GB201000054D0 (en) * | 2010-01-05 | 2010-02-17 | Rolls Royce Plc | Propeller assembly pitch change apparatus |
| US8021112B2 (en) * | 2010-06-29 | 2011-09-20 | General Electric Company | Methods and systems for monitoring operation of a wind turbine |
| GB201011349D0 (en) * | 2010-07-06 | 2010-08-18 | Rolls Royce Plc | Axial displacement and rotational speed monitoring |
| KR101060682B1 (ko) | 2011-05-31 | 2011-08-30 | 박정근 | 축류팬의 날개각 조절 검지장치 |
| FR2980770B1 (fr) * | 2011-10-03 | 2014-06-27 | Snecma | Turbomachine a helice(s) pour aeronef avec systeme pour changer le pas de l'helice. |
| FR3009015B1 (fr) * | 2013-07-24 | 2015-08-07 | Snecma | Dispositif de commande du calage des pales, et helice |
| DE102013014033B4 (de) * | 2013-08-26 | 2015-12-24 | Hägele GmbH | Hydraulische Stellvorrichtung |
| US9835041B2 (en) | 2014-10-31 | 2017-12-05 | Hamilton Sundstrand Corporation | Vane position sensor installation within a turbine case |
| US10458338B2 (en) * | 2015-10-19 | 2019-10-29 | General Electric Company | Aeroderivative jet engine accessory starter relocation to main shaft—directly connected to HPC shaft |
| PL414889A1 (pl) * | 2015-11-23 | 2017-06-05 | General Electric Company | Okapotowanie sprężające dla wylotu silnika odrzutowego |
| FR3046409B1 (fr) * | 2016-01-05 | 2018-02-09 | Safran Aircraft Engines | Systeme de commande de l'orientation des pales de soufflante d'une turbomachine a pion de blocage de mise en drapeau |
| FR3055354B1 (fr) * | 2016-08-26 | 2019-08-23 | Safran Aircraft Engines | Turbomachine comprenant des moyens d'etancheite et procede de montage de la turbomachine correspondant |
| CN108032993B (zh) * | 2017-12-15 | 2024-04-09 | 惠阳航空螺旋桨有限责任公司 | 一种小距锁止动装置 |
| CN111547252B (zh) * | 2020-04-21 | 2021-12-24 | 中国航发湖南动力机械研究所 | 尾桨桨距操纵轴装置及其制备方法 |
| FR3118942B1 (fr) * | 2021-01-18 | 2022-12-09 | Safran Aircraft Engines | Soufflante a calage variable |
| CN113048118B (zh) * | 2021-03-24 | 2022-02-18 | 大连理工大学 | 一种用于迎角调节的液压支撑装置 |
| FR3141718B1 (fr) * | 2022-11-08 | 2024-11-01 | Safran Aircraft Engines | Turbomachine d’aeronef a detection de deplacement axial d’une soufflante |
| FR3149352A1 (fr) | 2023-06-05 | 2024-12-06 | Franck GROLLEAU | Dispositif d’inversion de poussée pour moteur d’aéronef de forte puissance ultra-frugaux |
| FR3155207B1 (fr) * | 2023-11-14 | 2025-10-17 | Safran Aircraft Engines | Actionneur hydraulique lineaire pour une turbomachine d’aeronef |
Family Cites Families (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2472693A (en) * | 1949-06-07 | Pitch indicator for variable | ||
| US2670805A (en) * | 1947-03-20 | 1954-03-02 | Harry J Nichols | Controllable reversible pitch propeller |
| US2993543A (en) * | 1957-07-30 | 1961-07-25 | United Aircraft Corp | Multiple-area hydraulic motor |
| US3439745A (en) * | 1966-03-30 | 1969-04-22 | United Aircraft Corp | Combined propeller pitch lock and low pitch stop system |
| DE1628240A1 (de) * | 1966-04-12 | 1971-07-08 | Dowty Rotol Ltd | Vorrichtung zur Schaufelverstellung bei Geblaesen |
| GB1275064A (en) * | 1968-11-14 | 1972-05-24 | Lucas Industries Ltd | Servo-mechanism |
| US3757640A (en) * | 1971-12-01 | 1973-09-11 | Avco Corp | Simplified follower servomechanism |
-
1973
- 1973-10-01 US US402067A patent/US3873235A/en not_active Expired - Lifetime
-
1974
- 1974-09-03 CA CA208,299A patent/CA1015276A/en not_active Expired
- 1974-09-26 IT IT27768/74A patent/IT1022364B/it active
- 1974-09-27 FR FR7432725A patent/FR2246743A1/fr not_active Withdrawn
- 1974-09-28 DE DE19742446527 patent/DE2446527A1/de not_active Withdrawn
- 1974-09-30 BE BE149074A patent/BE820543A/fr not_active IP Right Cessation
- 1974-10-01 GB GB45519/76A patent/GB1484685A/en not_active Expired
- 1974-10-01 GB GB42540/74A patent/GB1484683A/en not_active Expired
- 1974-10-01 GB GB45518/76A patent/GB1484684A/en not_active Expired
- 1974-10-01 JP JP49112385A patent/JPS5924259B2/ja not_active Expired
Also Published As
| Publication number | Publication date |
|---|---|
| JPS5924259B2 (ja) | 1984-06-08 |
| IT1022364B (it) | 1978-03-20 |
| GB1484685A (en) | 1977-09-01 |
| GB1484684A (en) | 1977-09-01 |
| JPS5077718A (fr) | 1975-06-25 |
| FR2246743A1 (fr) | 1975-05-02 |
| CA1015276A (en) | 1977-08-09 |
| GB1484683A (en) | 1977-09-01 |
| US3873235A (en) | 1975-03-25 |
| DE2446527A1 (de) | 1975-04-10 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| RE | Patent lapsed |
Owner name: GENERAL ELECTRIC CY Effective date: 19840930 |