PL3974313T3 - Aparatura i sposoby sterowania śmigłem samolotu - Google Patents
Aparatura i sposoby sterowania śmigłem samolotuInfo
- Publication number
- PL3974313T3 PL3974313T3 PL21203536.4T PL21203536T PL3974313T3 PL 3974313 T3 PL3974313 T3 PL 3974313T3 PL 21203536 T PL21203536 T PL 21203536T PL 3974313 T3 PL3974313 T3 PL 3974313T3
- Authority
- PL
- Poland
- Prior art keywords
- controlling
- methods
- aircraft propeller
- propeller
- aircraft
- Prior art date
Links
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
- B64C11/301—Blade pitch-changing mechanisms characterised by blade position indicating means
-
- 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
-
- 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
- B64C11/46—Arrangements of, or constructional features peculiar to, multiple propellers
- B64C11/50—Phase synchronisation between multiple propellers
-
- 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
- B64D45/00—Aircraft indicators or protectors not otherwise provided for
- B64D45/0005—Devices specially adapted to indicate the position of a movable element of the aircraft, e.g. landing gear
-
- 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
- B64D35/00—Transmitting power from power plants to propellers or rotors; Arrangements of transmissions
- B64D35/02—Transmitting power from power plants to propellers or rotors; Arrangements of transmissions specially adapted for specific power plants
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Measurement Of Length, Angles, Or The Like Using Electric Or Magnetic Means (AREA)
- Length Measuring Devices With Unspecified Measuring Means (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US15/239,784 US10486827B2 (en) | 2016-08-17 | 2016-08-17 | Apparatus and methods for aircraft propeller control |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| PL3974313T3 true PL3974313T3 (pl) | 2025-09-08 |
Family
ID=59649621
Family Applications (2)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| PL17186725T PL3284666T3 (pl) | 2016-08-17 | 2017-08-17 | Aparatura i sposób sterowania śmigłem samolotu |
| PL21203536.4T PL3974313T3 (pl) | 2016-08-17 | 2017-08-17 | Aparatura i sposoby sterowania śmigłem samolotu |
Family Applications Before (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| PL17186725T PL3284666T3 (pl) | 2016-08-17 | 2017-08-17 | Aparatura i sposób sterowania śmigłem samolotu |
Country Status (3)
| Country | Link |
|---|---|
| US (3) | US10486827B2 (pl) |
| EP (2) | EP3974313B1 (pl) |
| PL (2) | PL3284666T3 (pl) |
Families Citing this family (29)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US10486827B2 (en) * | 2016-08-17 | 2019-11-26 | Pratt & Whitney Canada Corp. | Apparatus and methods for aircraft propeller control |
| US10889367B2 (en) | 2017-04-24 | 2021-01-12 | Pratt & Whitney Canada Corp. | Feedback system for pitch-adjustable blades of aircraft bladed rotor |
| GB2563948A (en) * | 2017-06-30 | 2019-01-02 | Airbus Operations Ltd | Aircraft landing gear assembly |
| WO2019217635A1 (en) | 2018-05-09 | 2019-11-14 | Abb Schweiz Ag | Turbine speed detection and use |
| US10864979B2 (en) * | 2018-06-27 | 2020-12-15 | Pratt & Whitney Canada Corp. | System and method for propeller feedback ring position detection |
| US10801360B2 (en) * | 2018-06-29 | 2020-10-13 | Pratt & Whitney Canada Corp. | Phonic wheel with output voltage tuning |
| US10745110B2 (en) | 2018-06-29 | 2020-08-18 | Pratt & Whitney Canada Corp. | Propeller blade synchrophasing using phonic wheel |
| US10822105B2 (en) | 2018-07-04 | 2020-11-03 | Pratt & Whitney Canada Corp. | Method and system for controlling a crossing threshold used in determining rotational speed of a propeller |
| US11046422B2 (en) * | 2018-07-16 | 2021-06-29 | Pratt & Whitney Canada Corp. | Propeller blade angle feedback arrangement and method |
| US11279465B2 (en) * | 2018-07-16 | 2022-03-22 | Pratt & Whitney Canada Corp. | Propeller blade angle feedback arrangement and method |
| US11136134B2 (en) * | 2018-12-21 | 2021-10-05 | Pratt & Whitney Canada Corp. | System and method for operating a gas turbine engine coupled to an aircraft propeller |
| US10829201B2 (en) * | 2019-03-20 | 2020-11-10 | Pratt & Whitney Canada Corp. | Blade angle position feedback system with extended markers |
| US11643187B2 (en) * | 2019-04-09 | 2023-05-09 | Pratt & Whitney Canada Corp. | Blade angle position feedback system with profiled marker terminations |
| US11554850B2 (en) * | 2019-04-25 | 2023-01-17 | Pratt & Whitney Canada Corp. | Blade angle position feedback system with offset sensors |
| CN110186370B (zh) * | 2019-04-30 | 2021-02-09 | 中国航发南方工业有限公司 | 桨叶角测量传感器动态测试设备及方法 |
| US11333020B2 (en) * | 2019-05-31 | 2022-05-17 | Pratt & Whitney Canada Corp. | Feedback device with non-axially aligned position markers |
| US11371825B2 (en) * | 2019-05-31 | 2022-06-28 | Pratt & Whitney Canada Corp. | Feedback device with differing magnetic permeability zones |
| US11046423B2 (en) * | 2019-07-18 | 2021-06-29 | Pratt & Whitney Canada Corp. | Blade angle position feedback system with magnetic shield |
| US11365691B2 (en) * | 2019-09-05 | 2022-06-21 | Pratt & Whitney Canada Corp. | Blade angle position feedback system with embedded markers |
| US11420772B2 (en) * | 2019-12-17 | 2022-08-23 | Pratt & Whitney Canada Corp. | System and method for determining an axial position of a feedback device |
| US11592455B2 (en) * | 2020-01-13 | 2023-02-28 | Woodward, Inc. | Adaptive voltage threshold for turbine engine |
| US11767769B2 (en) * | 2020-12-11 | 2023-09-26 | Pratt & Whitney Canada Corp. | Method and system for testing a sensor of a propeller blade angle position feedback system |
| US11702943B2 (en) * | 2021-02-01 | 2023-07-18 | Pratt & Whitney Canada Corp. | Propeller control unit validation |
| US11905840B2 (en) * | 2021-02-01 | 2024-02-20 | Pratt & Whitney Canada Corp. | System and method for detecting failure of a propeller feedback device |
| CN113358084B (zh) * | 2021-04-30 | 2022-11-29 | 武汉船用机械有限责任公司 | 螺距反馈信号的确定装置 |
| CN114485373B (zh) * | 2022-01-05 | 2024-09-20 | 武汉船用机械有限责任公司 | 调距桨反馈环的调整方法和调整结构 |
| US12077278B1 (en) | 2023-04-27 | 2024-09-03 | Pratt & Whitney Canada Corp. | Systems and methods for detecting erroneous propeller blade pitch measurements |
| EP4506244A1 (en) * | 2023-08-09 | 2025-02-12 | Ratier-Figeac SAS | Protection system |
| CN117685179B (zh) * | 2024-01-31 | 2024-04-19 | 安徽容知日新科技股份有限公司 | 风机变桨系统监测方法、监测设备及存储介质 |
Family Cites Families (41)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2221306A (en) | 1988-07-29 | 1990-01-31 | Dowty Rotol Ltd | Assembly for determining the longitudinal displacement of a rotating shaft |
| US4948337A (en) | 1989-05-01 | 1990-08-14 | United Technologies Corporation | Aircraft engine propulsor blade pitch sensing |
| DE69025738T2 (de) | 1989-12-30 | 1996-11-14 | Toyota Motor Co Ltd | Blattverstellsteuerung für Propeller mit veränderbarer Steigung |
| US5211539A (en) * | 1991-05-13 | 1993-05-18 | Allied-Signal Inc. | Apparatus for indicating the pitch of turbofan blades |
| JPH0524585A (ja) | 1991-07-25 | 1993-02-02 | Toyota Motor Corp | 可変ピツチプロペラのピツチ制御装置 |
| US5284418A (en) | 1991-07-29 | 1994-02-08 | Toyota Jidosha Kabushiki Kaisha | Electric pitch control apparatus for variable pitch propeller capable of controlling the pitch angle based instantaneous operational conditions of the propeller |
| US5174718A (en) * | 1991-08-12 | 1992-12-29 | United Technologies Corporation | Blade pitch change control system |
| FR2754310B1 (fr) | 1996-10-04 | 1998-11-13 | Renault Sport | Groupe motopropulseur pour avion et son procede de commande |
| US5997250A (en) | 1997-01-09 | 1999-12-07 | Catercopters, Llc | Method and apparatus for controlling pitch of an aircraft propeller |
| US5865599A (en) | 1997-03-11 | 1999-02-02 | United Technologies Corporation | System and process for direct blade angle measurement in propulsion systems |
| JPH11255199A (ja) | 1998-03-10 | 1999-09-21 | Toyota Motor Corp | 航空機の推力制御装置 |
| US6213713B1 (en) | 1998-12-31 | 2001-04-10 | United Technologies Corporation | Apparatus for indicating pitch angle of a propeller blade |
| US20040018914A1 (en) | 2002-07-29 | 2004-01-29 | Stolfus Joel D. | Linear position sensing employing two geartooth sensors, a helical gear and a spur gear |
| JP3991998B2 (ja) * | 2004-02-13 | 2007-10-17 | 日産自動車株式会社 | 可変動弁機構の学習装置 |
| DE102004037352B4 (de) * | 2004-07-30 | 2008-06-26 | Eads Deutschland Gmbh | Verfahren zur Überwachung einer zulässigen Konfidenz einer Messgröße eines dynamischen Systems |
| JP4786390B2 (ja) * | 2006-03-30 | 2011-10-05 | トヨタ自動車株式会社 | 可変バルブタイミング装置 |
| US7281482B1 (en) | 2006-09-25 | 2007-10-16 | The United States Of America Represented By The Secretary Of The Navy | Side thruster performance improvement with power optimization controller |
| JP4826802B2 (ja) * | 2007-03-19 | 2011-11-30 | 国産電機株式会社 | 内燃機関用点火装置 |
| US20090109039A1 (en) * | 2007-10-24 | 2009-04-30 | Krikor George Kellzi | Remote starter system with temperature compensated crank time |
| JP4569665B2 (ja) * | 2008-05-13 | 2010-10-27 | トヨタ自動車株式会社 | 内燃機関の制御システム |
| GB0816637D0 (en) | 2008-09-12 | 2008-10-22 | Rolls Royce Plc | Blade Pitch Control |
| US20100108806A1 (en) | 2008-10-08 | 2010-05-06 | Searete Llc, A Limited Liability Corporation Of The State Of Delaware | Hybrid propulsive engine including at least one independently rotatable propeller/fan |
| US8465257B1 (en) | 2008-10-31 | 2013-06-18 | Brp Us Inc. | Variable pitch propeller |
| GB2465575A (en) | 2008-11-21 | 2010-05-26 | Rolls Royce Plc | Displacement measurement / rotor blade pitch measurement arrangement |
| FR2943620B1 (fr) | 2009-03-27 | 2012-08-17 | Eurocopter France | Procede et dispositif pour optimiser le point de fonctionnement d'helices propulsives disposees de part et d'autre du fuselage d'un giravion |
| JP5437687B2 (ja) * | 2009-04-14 | 2014-03-12 | ナブテスコ株式会社 | アクチュエータ監視回路、制御装置、およびアクチュエータユニット |
| US9272778B2 (en) | 2009-06-04 | 2016-03-01 | Airbus Helicopters | Device for assisting in piloting hybrid helicopter, hybrid helicopter provided with such device, and method implemented by such device |
| FR2946322B1 (fr) | 2009-06-04 | 2011-06-17 | Eurocopter France | Dispositif d'aide au pilotage d'un helicoptere hybride, helicoptere hybride muni d'un tel dispositif et procede mis en oeuvre par ledit dispositif |
| US8689538B2 (en) | 2009-09-09 | 2014-04-08 | The Boeing Company | Ultra-efficient propulsor with an augmentor fan circumscribing a turbofan |
| JP5758659B2 (ja) * | 2011-03-17 | 2015-08-05 | トヨタ自動車株式会社 | エンジン試験装置及びエンジン試験方法 |
| GB201221095D0 (en) * | 2012-11-23 | 2013-01-09 | Rolls Royce Plc | Monitoring and control system |
| JP6126432B2 (ja) * | 2013-03-29 | 2017-05-10 | 本田技研工業株式会社 | 燃料噴射制御装置 |
| US9821901B2 (en) | 2013-11-21 | 2017-11-21 | Pratt & Whitney Canada Corp. | System and method for electronic propeller blade angle position feedback |
| US20170283046A1 (en) * | 2014-10-01 | 2017-10-05 | Sikorsky Aircraft Corporation | Sealed hub and shaft fairing for rotary wing aircraft |
| PL226824B1 (pl) * | 2015-09-07 | 2017-09-29 | Gen Electric | Układ isposób regulacji skoku smigła |
| GB2548085B (en) * | 2016-02-29 | 2019-12-25 | Ge Aviation Systems Llc | A system and method for coordinating a propeller with an electronic engine control |
| US10486827B2 (en) * | 2016-08-17 | 2019-11-26 | Pratt & Whitney Canada Corp. | Apparatus and methods for aircraft propeller control |
| EP3296513B1 (en) * | 2016-09-16 | 2020-08-19 | Ratier-Figeac SAS | Propeller health monitoring |
| EP3401661B1 (en) * | 2017-05-10 | 2023-11-08 | Ratier-Figeac SAS | Propeller health monitoring |
| FR3075353B1 (fr) * | 2017-12-14 | 2020-05-29 | Safran Aircraft Engines | Mesure non intrusive du calage d'une pale |
| US11046422B2 (en) * | 2018-07-16 | 2021-06-29 | Pratt & Whitney Canada Corp. | Propeller blade angle feedback arrangement and method |
-
2016
- 2016-08-17 US US15/239,784 patent/US10486827B2/en active Active
-
2017
- 2017-08-17 EP EP21203536.4A patent/EP3974313B1/en active Active
- 2017-08-17 PL PL17186725T patent/PL3284666T3/pl unknown
- 2017-08-17 EP EP17186725.2A patent/EP3284666B1/en active Active
- 2017-08-17 PL PL21203536.4T patent/PL3974313T3/pl unknown
-
2019
- 2019-10-25 US US16/664,122 patent/US11292607B2/en active Active
-
2022
- 2022-02-28 US US17/682,349 patent/US12365443B2/en active Active
Also Published As
| Publication number | Publication date |
|---|---|
| US20180050816A1 (en) | 2018-02-22 |
| EP3284666A1 (en) | 2018-02-21 |
| EP3284666B1 (en) | 2021-10-20 |
| US10486827B2 (en) | 2019-11-26 |
| US20220177155A1 (en) | 2022-06-09 |
| EP3974313A1 (en) | 2022-03-30 |
| PL3284666T3 (pl) | 2022-03-07 |
| CA2976500A1 (en) | 2018-02-17 |
| EP3974313B1 (en) | 2025-05-14 |
| US11292607B2 (en) | 2022-04-05 |
| US20200172263A1 (en) | 2020-06-04 |
| US12365443B2 (en) | 2025-07-22 |
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