ZA948876B - Pitch variation control device for the blades of a turbo-machine rotor and method of operating the device - Google Patents
Pitch variation control device for the blades of a turbo-machine rotor and method of operating the deviceInfo
- Publication number
- ZA948876B ZA948876B ZA948876A ZA948876A ZA948876B ZA 948876 B ZA948876 B ZA 948876B ZA 948876 A ZA948876 A ZA 948876A ZA 948876 A ZA948876 A ZA 948876A ZA 948876 B ZA948876 B ZA 948876B
- Authority
- ZA
- South Africa
- Prior art keywords
- turbo
- blades
- operating
- variation control
- control device
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C11/00—Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
- B64C11/30—Blade pitch-changing mechanisms
- B64C11/44—Blade pitch-changing mechanisms electric
-
- 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
-
- 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)
- Aviation & Aerospace Engineering (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR9313409A FR2712250B1 (fr) | 1993-11-10 | 1993-11-10 | Procédé et dispositif de commande de variation du pas des pales d'un rotor. |
Publications (1)
Publication Number | Publication Date |
---|---|
ZA948876B true ZA948876B (en) | 1995-07-31 |
Family
ID=9452718
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
ZA948876A ZA948876B (en) | 1993-11-10 | 1994-11-09 | Pitch variation control device for the blades of a turbo-machine rotor and method of operating the device |
Country Status (10)
Country | Link |
---|---|
US (1) | US5595474A (ru) |
EP (1) | EP0652154B1 (ru) |
JP (1) | JP3032440B2 (ru) |
CA (1) | CA2135469C (ru) |
DE (1) | DE69411672T2 (ru) |
FR (1) | FR2712250B1 (ru) |
RU (1) | RU2107194C1 (ru) |
UA (1) | UA26462C2 (ru) |
WO (1) | WO1995013215A1 (ru) |
ZA (1) | ZA948876B (ru) |
Families Citing this family (63)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE4446623A1 (de) * | 1994-12-24 | 1996-06-27 | Klein Schanzlin & Becker Ag | Propellerverstelleinrichtung mit Synchronelement |
RU2108268C1 (ru) * | 1996-10-17 | 1998-04-10 | Йелстаун Корпорейшн Н.В. | Система и способ управления воздушным винтом изменяемого шага с обратной связью |
US6379109B1 (en) | 2000-05-12 | 2002-04-30 | Roy F. Senior, Jr. | Method and apparatus for detecting and removing obstructions in mechanical aerators |
US6476534B1 (en) | 2000-08-08 | 2002-11-05 | General Dynamics Advanced Technology Systems, Inc. | Permanent magnet phase-control motor |
PL206076B1 (pl) * | 2000-11-14 | 2010-06-30 | Aloys Wobben | Siłownia wiatrowa |
WO2003035470A1 (en) * | 2001-10-22 | 2003-05-01 | Lamont John S | Aircraft |
FR2831225B1 (fr) | 2001-10-24 | 2004-01-02 | Snecma Moteurs | Dispositif electrohydraulique de changement de pas d'helice |
US6672835B1 (en) | 2003-05-19 | 2004-01-06 | Arthur C. Hughes | Method and apparatus for self-contained variable pitch and/or constant speed propeller including provisions for feathering and reverse pitch operation |
CA2459200A1 (en) | 2004-02-27 | 2005-08-27 | John S. Lamont | Aircraft |
US20050226727A1 (en) * | 2004-03-03 | 2005-10-13 | Dennis Brian D | Methods and systems for controlling the pitch of a propeller |
US7513320B2 (en) * | 2004-12-16 | 2009-04-07 | Tdy Industries, Inc. | Cemented carbide inserts for earth-boring bits |
US7901185B2 (en) * | 2007-02-21 | 2011-03-08 | United Technologies Corporation | Variable rotor blade for gas turbine engine |
US7939958B2 (en) * | 2007-06-01 | 2011-05-10 | Bill Todorof | Direct drive wind turbine and blade assembly |
FR2922265B1 (fr) * | 2007-10-12 | 2013-11-22 | Snecma | Turboreacteur incorporant un generateur de courant electrique. |
RU2523928C2 (ru) * | 2009-02-27 | 2014-07-27 | Снекма | Лопатки вентилятора с изменяемым углом установки |
FR2951696B1 (fr) * | 2009-10-22 | 2011-12-23 | Snecma | Systeme pour faire varier l'incidence des pales d'une helice de turbomachine pour aeronef, utilisant un moteur electrique sans balai |
FR2956854B1 (fr) * | 2010-03-01 | 2012-08-17 | Snecma | Dispositif de commande de l'orientation des pales de soufflante d'un turbopropulseur par contrepoids. |
FR2959481B1 (fr) * | 2010-04-30 | 2013-02-08 | Hispano Suiza Sa | Actionnement des pales d'une soufflante non carenee |
FR2961176B1 (fr) * | 2010-06-15 | 2012-08-03 | Hispano Suiza Sa | Alimentation electrique des equipements portes par le rotor d'un moteur d'aeronef |
DE102010039394A1 (de) * | 2010-08-17 | 2012-02-23 | Siemens Aktiengesellschaft | Verstellpropeller oder -repeller |
FR2964944B1 (fr) * | 2010-09-20 | 2013-05-24 | Snecma | Dispositif d'etancheite a soufflet pour la traversee de cloison par une biellette d'un systeme de commande de l'orientation des pales de soufflante d'un turbopropulseur |
RU2479753C2 (ru) * | 2011-07-07 | 2013-04-20 | Общество с ограниченной ответственностью "Газхолодтехника" | Способ автоматического управления частотой вращения рабочих колес вентиляторов |
US9470153B2 (en) * | 2011-10-05 | 2016-10-18 | United Technologies Corporation | Combined pump system for engine TMS AOC reduction and ECS loss elimination |
FR2983235B1 (fr) * | 2011-11-24 | 2018-04-13 | Safran Electrical & Power | Systeme mecanique tournant a actionnement sans contact |
ITTO20111113A1 (it) * | 2011-12-05 | 2013-06-06 | Wilic Sarl | Impianto eolico per la generazione di energia elettrica |
US20130280078A1 (en) * | 2012-04-23 | 2013-10-24 | Kollmorgen Corporation | Wind Turbine Blade Pitch Redundant Safety Arrangement |
FR2997245B1 (fr) * | 2012-10-24 | 2016-01-15 | Hispano Suiza Sa | Systeme electromecanique d'actionnement et/ou generation, comprenant une isolation electrique entre la source electrique et le consommateur |
WO2015053930A1 (en) * | 2013-10-11 | 2015-04-16 | Unison Industries, Llc | Method and apparatus for controlling a turboprop engine |
CN104863881B (zh) * | 2014-02-21 | 2018-10-23 | 南京中兴新软件有限责任公司 | 电子设备中风扇转速的控制方法及装置 |
US10436056B2 (en) | 2015-06-23 | 2019-10-08 | General Electric Company | Relative position measurement |
US10436151B2 (en) * | 2015-11-17 | 2019-10-08 | General Electric Company | Modular fan for a gas turbine engine |
US10830066B2 (en) * | 2016-01-05 | 2020-11-10 | Safran Aircraft Engines | Low-pitch variable-setting fan of a turbine engine |
US10288087B2 (en) * | 2016-03-24 | 2019-05-14 | United Technologies Corporation | Off-axis electric actuation for variable vanes |
US10294813B2 (en) | 2016-03-24 | 2019-05-21 | United Technologies Corporation | Geared unison ring for variable vane actuation |
US10329946B2 (en) * | 2016-03-24 | 2019-06-25 | United Technologies Corporation | Sliding gear actuation for variable vanes |
US10329947B2 (en) | 2016-03-24 | 2019-06-25 | United Technologies Corporation | 35Geared unison ring for multi-stage variable vane actuation |
US10190599B2 (en) | 2016-03-24 | 2019-01-29 | United Technologies Corporation | Drive shaft for remote variable vane actuation |
US10415596B2 (en) | 2016-03-24 | 2019-09-17 | United Technologies Corporation | Electric actuation for variable vanes |
US10443430B2 (en) * | 2016-03-24 | 2019-10-15 | United Technologies Corporation | Variable vane actuation with rotating ring and sliding links |
US10458271B2 (en) | 2016-03-24 | 2019-10-29 | United Technologies Corporation | Cable drive system for variable vane operation |
US10301962B2 (en) | 2016-03-24 | 2019-05-28 | United Technologies Corporation | Harmonic drive for shaft driving multiple stages of vanes via gears |
US10443431B2 (en) * | 2016-03-24 | 2019-10-15 | United Technologies Corporation | Idler gear connection for multi-stage variable vane actuation |
BE1024492B1 (fr) * | 2016-08-12 | 2018-03-12 | Safran Aero Boosters S.A. | Aube a orientation variable de compresseur de turbomachine axiale |
US10801339B2 (en) | 2017-07-11 | 2020-10-13 | General Electric Company | Aircraft gas turbine engine variable fan blade mechanism |
CN111065577A (zh) * | 2017-08-23 | 2020-04-24 | 维曼机器人股份有限公司 | 驱动机构 |
CN107902075B (zh) * | 2017-11-09 | 2020-11-27 | 中国航发湖南动力机械研究所 | 静态变距螺旋桨 |
FR3075257B1 (fr) * | 2017-12-14 | 2021-02-19 | Safran Aircraft Engines | Dispositif de reglage du calage d'une helice |
EP3502438A1 (en) * | 2017-12-19 | 2019-06-26 | Siemens Aktiengesellschaft | Compressor control |
FR3087232B1 (fr) | 2018-10-12 | 2021-06-25 | Safran Aircraft Engines | Turbomachine comprenant un rotor portant des pales a calage variable |
US11345469B2 (en) * | 2018-11-19 | 2022-05-31 | Joby Aero, Inc. | Aerial vehicle using motor pulse-induced cyclic control |
US10934880B1 (en) | 2019-09-04 | 2021-03-02 | The Boeing Company | Electrical generation from turbine engines |
CN113007133A (zh) * | 2019-12-19 | 2021-06-22 | 北汽福田汽车股份有限公司 | 风扇及散热模块、车辆 |
US11362567B2 (en) | 2020-01-16 | 2022-06-14 | The Boeing Company | Electrical power generation from turbine engines |
AT523262B1 (de) * | 2020-01-29 | 2021-07-15 | Manuel Schleiffelder Mag | Vorrichtung zur Verstellung der Neigung von Rotorblättern eines Rotors |
EP3882133A1 (en) | 2020-03-16 | 2021-09-22 | Ratier-Figeac SAS | Blade pitch actuation mechanism |
FR3108670B1 (fr) | 2020-03-31 | 2022-04-01 | Safran Aircraft Engines | Module de soufflante pour un banc d’essai de turbomachine d’aeronef |
US11193426B2 (en) | 2020-04-16 | 2021-12-07 | The Boeing Company | Electrically geared turbofan |
US20210347465A1 (en) * | 2020-05-11 | 2021-11-11 | Hamilton Sundstrand Corporation | Wireless power transformation for rotating propellers |
PL435034A1 (pl) * | 2020-08-20 | 2022-02-21 | General Electric Company Polska Spółka Z Ograniczoną Odpowiedzialnością | Zespoły silnika napędowego zapewniające dostęp do elementów składowych w komorach pędnych |
WO2022116398A1 (zh) * | 2021-02-20 | 2022-06-09 | 西安亚能电气有限责任公司 | 用于电力系统中风机的监测组件、监测装置以及监测模型 |
CN113682462A (zh) * | 2021-09-18 | 2021-11-23 | 上海交通大学 | 推进装置及其可调进口预旋导叶电驱动涵道风扇推进系统 |
CN113955084B (zh) * | 2021-12-22 | 2022-03-25 | 四川承天翼航空科技有限公司 | 旋翼变距控制系统、方法、同步/不同步变距控制方法 |
CN115123519B (zh) * | 2022-08-30 | 2022-11-22 | 沃飞长空科技(成都)有限公司 | 一种可变距的旋翼装置及飞行器 |
Family Cites Families (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2370135A (en) * | 1941-09-25 | 1945-02-27 | Engineering & Res Corp | Variable pitch propeller |
FR890641A (fr) * | 1942-10-05 | 1944-02-14 | Système pour la transmission d'énergie électrique entre une partie fixe et une partie mobile, mécanismes et machines comportant application de ce système | |
US2612228A (en) * | 1945-07-03 | 1952-09-30 | Fairey Aviat Co Ltd | Electrically driven propeller pitch change system |
US2632516A (en) * | 1946-11-26 | 1953-03-24 | United Aircraft Corp | Automatic control for reversing propellers |
US3044558A (en) * | 1960-01-05 | 1962-07-17 | Curtiss Wright Corp | Propeller pitch control system |
US3900274A (en) * | 1974-06-25 | 1975-08-19 | Gen Electric | Remote controlled actuation system for the rotor of a gas turbine engine |
US4591313A (en) * | 1983-12-30 | 1986-05-27 | The Boeing Company | Propeller pitch control system and apparatus |
US5281094A (en) * | 1991-05-13 | 1994-01-25 | Alliedsignal Inc | Electromechanical apparatus for varying blade of variable-pitch 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 |
US5183387A (en) * | 1992-01-03 | 1993-02-02 | Allied-Signal, Inc. | Fault-tolerant apparatus for controlling blade pitch |
FR2709618B1 (fr) * | 1993-07-28 | 1995-09-29 | Hispano Suiza Sa | Dispositif de transmission de signaux électriques de puissance à un ensemble tournant. |
US5451141A (en) * | 1993-12-23 | 1995-09-19 | United Technologies Corporation | Propeller pitch change machanism with inductive brake and motor |
-
1993
- 1993-11-10 FR FR9313409A patent/FR2712250B1/fr not_active Expired - Fee Related
-
1994
- 1994-11-09 WO PCT/FR1994/001308 patent/WO1995013215A1/fr unknown
- 1994-11-09 ZA ZA948876A patent/ZA948876B/xx unknown
- 1994-11-09 CA CA002135469A patent/CA2135469C/fr not_active Expired - Fee Related
- 1994-11-09 RU RU95121938A patent/RU2107194C1/ru not_active IP Right Cessation
- 1994-11-09 EP EP94402530A patent/EP0652154B1/fr not_active Expired - Lifetime
- 1994-11-09 DE DE69411672T patent/DE69411672T2/de not_active Expired - Fee Related
- 1994-11-09 UA UA95073144A patent/UA26462C2/uk unknown
- 1994-11-10 JP JP6303020A patent/JP3032440B2/ja not_active Expired - Fee Related
-
1996
- 1996-04-04 US US08/627,394 patent/US5595474A/en not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
UA26462C2 (uk) | 1999-08-30 |
WO1995013215A1 (fr) | 1995-05-18 |
CA2135469C (fr) | 2003-04-22 |
JPH07197852A (ja) | 1995-08-01 |
CA2135469A1 (fr) | 1995-05-11 |
JP3032440B2 (ja) | 2000-04-17 |
EP0652154B1 (fr) | 1998-07-15 |
DE69411672D1 (de) | 1998-08-20 |
FR2712250A1 (fr) | 1995-05-19 |
EP0652154A1 (fr) | 1995-05-10 |
FR2712250B1 (fr) | 1995-12-29 |
RU2107194C1 (ru) | 1998-03-20 |
DE69411672T2 (de) | 1998-12-24 |
US5595474A (en) | 1997-01-21 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
ZA948876B (en) | Pitch variation control device for the blades of a turbo-machine rotor and method of operating the device | |
AU4597396A (en) | Rotor device and control for wind turbine | |
PT1394929E (pt) | Processo para operação de uma central de energia eólica, bem como a própria central de energia eólica | |
GB2282856B (en) | Method and apparatus for reducing stress on the tips of turbine or compressor blades | |
DE3664421D1 (en) | Method for repairing a steam turbine or generator rotor | |
GB2261032B (en) | Rotor blade for a gas turbine | |
ZA891570B (en) | Wind turbine shutdown system | |
GB9401470D0 (en) | Retaining and sealng arrangement for the blades of a rotor disc | |
PL312501A1 (en) | Control system for showing oscillations of a number of blades on a rotating rotor wheel | |
GB8907283D0 (en) | Gas turbine clearance control | |
AU4521789A (en) | Turbine blade clearance controller | |
AU624530B2 (en) | A turbine nozzle, and a method of varying the power of same | |
GB2276575B (en) | A method and apparatus for producing an integrally bladed rotor | |
GB2310897B (en) | Method and apparatus for reducing stress on the tips of turbine or compressor blades | |
GB2264283B (en) | Overspeed governor of a stairlift and method of operating the stairlift | |
GB2324835B (en) | Method of manufacturing a turbine blade | |
GB9005866D0 (en) | Control system and method for controlling a gas turbine engine | |
GB9401049D0 (en) | A method of repairing turbine blades | |
GB9401057D0 (en) | A method of repairing turbine blades | |
GB8906929D0 (en) | Method of repairing turbine blades | |
GB9417425D0 (en) | Apparatus for machining turbine blades | |
GB9501304D0 (en) | A method of repairing turbine blades | |
GB9501293D0 (en) | A method of repairing turbine blades | |
GB9601556D0 (en) | A method of repairing turbine blades | |
GB9601555D0 (en) | A method of repairing turbine blades |