PL413810A1 - Układ i sposób regulacji skoku śmigła - Google Patents
Układ i sposób regulacji skoku śmigłaInfo
- Publication number
- PL413810A1 PL413810A1 PL413810A PL41381015A PL413810A1 PL 413810 A1 PL413810 A1 PL 413810A1 PL 413810 A PL413810 A PL 413810A PL 41381015 A PL41381015 A PL 41381015A PL 413810 A1 PL413810 A1 PL 413810A1
- Authority
- PL
- Poland
- Prior art keywords
- otb
- pitch
- fluid communication
- flow channel
- pitch adjustment
- Prior art date
Links
- 238000000034 method Methods 0.000 title abstract 2
- 239000012530 fluid Substances 0.000 abstract 2
Classifications
-
- 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
- B64C11/38—Blade pitch-changing mechanisms fluid, e.g. hydraulic
-
- 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
- F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
- F02C9/48—Control of fuel supply conjointly with another control of the plant
- F02C9/56—Control of fuel supply conjointly with another control of the plant with power transmission control
- F02C9/58—Control of fuel supply conjointly with another control of the plant with power transmission control with control of a variable-pitch propeller
-
- 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
- B64C11/306—Blade pitch-changing mechanisms specially adapted for contrarotating propellers
-
- 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
- F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
- F02C3/04—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor
-
- 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
-
- 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
- F02C7/06—Arrangements of bearings; Lubricating
-
- 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
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D2027/005—Aircraft with an unducted turbofan comprising contra-rotating rotors, e.g. contra-rotating open rotors [CROR]
-
- 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
- F05D2220/32—Application in turbines in gas turbines
- F05D2220/323—Application in turbines in gas turbines for aircraft propulsion, e.g. jet 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
- F05D2240/00—Components
- F05D2240/35—Combustors or associated equipment
-
- 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)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Wind Motors (AREA)
Abstract
Ujawniono układy i sposoby regulacji kąta skoku śmigła i zespół wirnikowy, który selektywnie ogranicza kąt skoku w zależności od wybranego trybu pracy. Układ zawiera siłownik (45) mający przednią i tylną komorę, łożysko olejowe (OTB) oraz kołnierz z precyzyjnym zatrzymaniem. Kołnierz z precyzyjnym zatrzymaniem zawiera pierwszy kanał przepływowy w połączeniu płynu z OTB oraz z komorą przednią w trybie pracy naziemnej, oraz drugi kanał przepływowy w połączeniu płynu z OTB oraz z komorą przednią w trybie pracy podczas lotu.
Priority Applications (7)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
PL413810A PL226824B1 (pl) | 2015-09-07 | 2015-09-07 | Układ isposób regulacji skoku smigła |
US15/228,148 US10793255B2 (en) | 2015-09-07 | 2016-08-04 | System and method for controlling propeller pitch |
CA2940042A CA2940042A1 (en) | 2015-09-07 | 2016-08-25 | System and method for controlling propeller pitch |
JP2016166482A JP2017095081A (ja) | 2015-09-07 | 2016-08-29 | プロペラピッチを制御するためのシステム及び方法 |
EP16186944.1A EP3138771A1 (en) | 2015-09-07 | 2016-09-02 | System and method for controlling propeller pitch |
BR102016020541A BR102016020541A2 (pt) | 2015-09-07 | 2016-09-06 | sistema de controle de passo, motor de turbina a gás e método para controlar um ângulo de passo |
CN201610807256.2A CN106499522B (zh) | 2015-09-07 | 2016-09-07 | 用于控制螺旋桨桨距的系统及方法 |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
PL413810A PL226824B1 (pl) | 2015-09-07 | 2015-09-07 | Układ isposób regulacji skoku smigła |
Publications (2)
Publication Number | Publication Date |
---|---|
PL413810A1 true PL413810A1 (pl) | 2017-03-13 |
PL226824B1 PL226824B1 (pl) | 2017-09-29 |
Family
ID=56855333
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PL413810A PL226824B1 (pl) | 2015-09-07 | 2015-09-07 | Układ isposób regulacji skoku smigła |
Country Status (7)
Country | Link |
---|---|
US (1) | US10793255B2 (pl) |
EP (1) | EP3138771A1 (pl) |
JP (1) | JP2017095081A (pl) |
CN (1) | CN106499522B (pl) |
BR (1) | BR102016020541A2 (pl) |
CA (1) | CA2940042A1 (pl) |
PL (1) | PL226824B1 (pl) |
Families Citing this family (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
PL226824B1 (pl) | 2015-09-07 | 2017-09-29 | Gen Electric | Układ isposób regulacji skoku smigła |
EP3354562A1 (en) * | 2017-01-30 | 2018-08-01 | Ge Avio S.r.l. | Transfer bearing collapsing device |
FR3087857B1 (fr) * | 2018-10-30 | 2021-02-12 | Safran Aircraft Engines | Module de soufflante a pales a calage variable |
US11530027B2 (en) | 2019-12-02 | 2022-12-20 | Pratt & Whitney Canada Corp. | Propeller control unit with bypass drain line |
US11702943B2 (en) | 2021-02-01 | 2023-07-18 | Pratt & Whitney Canada Corp. | Propeller control unit validation |
US11982190B2 (en) | 2021-02-02 | 2024-05-14 | Pratt & Whitney Canada Corp. | Propeller control unit |
FR3120913B1 (fr) * | 2021-03-16 | 2023-02-24 | Safran Aircraft Engines | Module de soufflante equipe d’un dispositif de transfert d’huile |
FR3120915B1 (fr) * | 2021-03-16 | 2023-04-14 | Safran Aircraft Engines | Module de soufflante equipe d’un dispositif de transfert d’huile |
FR3120914A1 (fr) | 2021-03-16 | 2022-09-23 | Safran Aircraft Engines | Module de soufflante equipe d’un dispositif de transfert d’huile |
FR3120912B1 (fr) * | 2021-03-16 | 2023-02-24 | Safran Aircraft Engines | Module de soufflante equipe d’un dispositif de transfert d’huile |
FR3130877A1 (fr) | 2021-12-20 | 2023-06-23 | Safran Aircraft Engines | Dispostif de transfert de fluide avec moyens de connexion hydraulique et mecanique |
WO2023247906A1 (fr) * | 2022-06-22 | 2023-12-28 | Safran Aircraft Engines | Mecanisme de changement de pas avec verin entourant un palier de transfert de fluide |
FR3137062B1 (fr) * | 2022-06-22 | 2024-05-17 | Safran Aircraft Engines | Mecanisme de changement de pas avec dispositif de verrouillage de pas comprenant une vis a rouleaux satellites |
FR3141441A1 (fr) * | 2022-10-28 | 2024-05-03 | Safran Aircraft Engines | Mécanisme de changement de pas à cinématique inversée |
Family Cites Families (30)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB568530A (en) * | 1941-03-07 | 1945-04-10 | English Electric Co Ltd | Improved operating gear for adjustable propeller type blades in hydraulic turbines and pumps |
NL84649C (pl) * | 1953-10-26 | |||
US4523891A (en) | 1983-06-15 | 1985-06-18 | United Technologies Corporation | Propeller pitch change actuation system |
GB8723246D0 (en) * | 1987-10-03 | 1987-11-04 | Dowty Rotol Ltd | Bladed rotor assemblies |
US4936746A (en) | 1988-10-18 | 1990-06-26 | United Technologies Corporation | Counter-rotation pitch change system |
US4893989A (en) | 1989-03-07 | 1990-01-16 | United Technologies Corporation | Variable propeller system incorporating a forward transfer bearing |
US5174718A (en) * | 1991-08-12 | 1992-12-29 | United Technologies Corporation | Blade pitch change control system |
US5186608A (en) * | 1991-10-25 | 1993-02-16 | United Technologies Corporation | Hydraulic low pitch switch for propeller pitch change system |
US5897293A (en) * | 1996-11-22 | 1999-04-27 | United Technologies Corporation | Counterweighted propeller control system |
US6261062B1 (en) * | 2000-01-17 | 2001-07-17 | Brunswick Corporation | Actuation system for a controllable pitch propeller |
US6811376B2 (en) * | 2002-03-19 | 2004-11-02 | Hamilton Sundstrand | Actuation system for a controllable pitch propeller |
GB0614302D0 (en) | 2006-07-19 | 2006-08-30 | Rolls Royce Plc | An engine arrangement |
US8439640B2 (en) | 2008-07-15 | 2013-05-14 | Hamilton Sundstrand Corporation | Propeller blade pitch control system |
FR2937678B1 (fr) * | 2008-10-23 | 2013-11-22 | Snecma | Dispositif de commande de l'orientation des pales de soufflante d'un turbopropulseur |
FR2946011B1 (fr) * | 2009-05-29 | 2013-01-11 | Snecma | Dispositif a verin mobile pour la commande de l'orientation des pales de soufflante d'un turbopropulseur |
FR2946315B1 (fr) | 2009-06-04 | 2011-05-20 | Eurocopter France | Procede et systeme de commande et de regulation motrice pour helicoptere hybride |
FR2955085B1 (fr) * | 2010-01-08 | 2011-12-23 | Snecma | Systeme d'helices contrarotatives pour turbomachine d'aeronef |
US8566000B2 (en) | 2010-02-23 | 2013-10-22 | Williams International Co., L.L.C. | System and method for controlling a single-spool turboshaft engine |
KR20120014347A (ko) | 2010-08-09 | 2012-02-17 | 현대중공업 주식회사 | Cpp 추진 제어 시스템에서의 프로펠러 피치 제어 장치 및 방법 |
US8336290B2 (en) * | 2010-09-30 | 2012-12-25 | General Electric Company | Pitch change apparatus for counter-rotating propellers |
US8371105B2 (en) * | 2010-09-30 | 2013-02-12 | General Electric Company | Hydraulic system for fan pitch change actuation of counter-rotating propellers |
FR2973333B1 (fr) * | 2011-03-29 | 2014-08-01 | Snecma | Systeme pour changer le pas d'helices contrarotatives d'un turbomoteur |
GB2491811B (en) * | 2011-06-14 | 2013-10-09 | Rolls Royce Plc | Mounting system |
FR2978122B1 (fr) * | 2011-07-21 | 2013-08-30 | Snecma | Dispositif d'alimentation en fluide d'un verin hydraulique pour la commande de l'orientation des pales de soufflante d'un turbopropulseur a double helice |
FR2978953B1 (fr) | 2011-08-08 | 2013-09-20 | Snecma | Systeme de commande hydraulique de l'orientation de pales de soufflante |
FR2980770B1 (fr) * | 2011-10-03 | 2014-06-27 | Snecma | Turbomachine a helice(s) pour aeronef avec systeme pour changer le pas de l'helice. |
JP6059468B2 (ja) * | 2012-08-24 | 2017-01-11 | ジーイー・アビエイション・システムズ・リミテッドGe Aviation Systems Limited | オープンローター様式のためのピッチ変更機構 |
FR2998867B1 (fr) * | 2012-12-05 | 2016-12-23 | Snecma | Dispositif d'alimentation et de repartition de fluide |
US10384763B2 (en) * | 2013-10-07 | 2019-08-20 | Ge Aviation Systems Limited | Pitch control assembly |
PL226824B1 (pl) | 2015-09-07 | 2017-09-29 | Gen Electric | Układ isposób regulacji skoku smigła |
-
2015
- 2015-09-07 PL PL413810A patent/PL226824B1/pl unknown
-
2016
- 2016-08-04 US US15/228,148 patent/US10793255B2/en active Active
- 2016-08-25 CA CA2940042A patent/CA2940042A1/en not_active Abandoned
- 2016-08-29 JP JP2016166482A patent/JP2017095081A/ja active Pending
- 2016-09-02 EP EP16186944.1A patent/EP3138771A1/en not_active Withdrawn
- 2016-09-06 BR BR102016020541A patent/BR102016020541A2/pt not_active Application Discontinuation
- 2016-09-07 CN CN201610807256.2A patent/CN106499522B/zh active Active
Also Published As
Publication number | Publication date |
---|---|
CN106499522A (zh) | 2017-03-15 |
EP3138771A1 (en) | 2017-03-08 |
BR102016020541A2 (pt) | 2017-03-14 |
US20170066523A1 (en) | 2017-03-09 |
CN106499522B (zh) | 2018-06-08 |
CA2940042A1 (en) | 2017-03-07 |
US10793255B2 (en) | 2020-10-06 |
PL226824B1 (pl) | 2017-09-29 |
JP2017095081A (ja) | 2017-06-01 |
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