WO2010028943A3 - Steuersystem für einen flugzeugpropellerantrieb - Google Patents

Steuersystem für einen flugzeugpropellerantrieb Download PDF

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Publication number
WO2010028943A3
WO2010028943A3 PCT/EP2009/060953 EP2009060953W WO2010028943A3 WO 2010028943 A3 WO2010028943 A3 WO 2010028943A3 EP 2009060953 W EP2009060953 W EP 2009060953W WO 2010028943 A3 WO2010028943 A3 WO 2010028943A3
Authority
WO
WIPO (PCT)
Prior art keywords
propeller
speed
accelerator
controlling
control system
Prior art date
Application number
PCT/EP2009/060953
Other languages
English (en)
French (fr)
Other versions
WO2010028943A2 (de
Inventor
Erik Bollen
Bodo Metzdorf
Original Assignee
Thielert Aircraft Engines Gmbh Vertr. D. D. Insolvenzverwalter Dr. Bruno M. Kübler
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Thielert Aircraft Engines Gmbh Vertr. D. D. Insolvenzverwalter Dr. Bruno M. Kübler filed Critical Thielert Aircraft Engines Gmbh Vertr. D. D. Insolvenzverwalter Dr. Bruno M. Kübler
Priority to EP09782180A priority Critical patent/EP2331401A2/de
Priority to US13/062,842 priority patent/US20110190966A1/en
Priority to CA2736193A priority patent/CA2736193A1/en
Priority to CN2009801351854A priority patent/CN102149600A/zh
Publication of WO2010028943A2 publication Critical patent/WO2010028943A2/de
Publication of WO2010028943A3 publication Critical patent/WO2010028943A3/de

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
    • B64C11/305—Blade pitch-changing mechanisms characterised by being influenced by other control systems, e.g. fuel supply
    • 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
    • B64D31/00—Power plant control systems; Arrangement of power plant control systems in aircraft
    • B64D31/02—Initiating means
    • B64D31/04—Initiating means actuated personally
    • 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
    • B64D31/00—Power plant control systems; Arrangement of power plant control systems in aircraft
    • B64D31/02—Initiating means
    • B64D31/06—Initiating means actuated automatically
    • 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
    • B64D31/00—Power plant control systems; Arrangement of power plant control systems in aircraft
    • B64D31/14—Transmitting means between initiating means and power plants

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Automation & Control Theory (AREA)
  • Electrical Control Of Air Or Fuel Supplied To Internal-Combustion Engine (AREA)
  • Combined Controls Of Internal Combustion Engines (AREA)
  • Control Of Vehicle Engines Or Engines For Specific Uses (AREA)

Abstract

Eine Steuerung für einen Flugzeugpropellerantrieb zur Leistungsregelung des Dieselmotors (2) mittels eines Gashebels (7) und eines Steuermoduls (8) und zur Drehzahlregelung des mit dem Dieselmotor (2) über einen Antriebsstrang (3) verbundenen und über ein Propellerblattstellventil (6) steuerbaren Flugzeugpropellers (4) umfasst einen voll digitalen Triebwerksregler (8) mit einem in diesen integrierten geschlossenen, mit dem Gashebel zur Leistungsregelung und mit dem Propellerblattstellventil zur Regelung der Propellerdrehzahl verbundenen Regelkreis, der den auf der Gashebelstellung beruhenden Sollwert und den gemessenen Istwert der Motordrehzahl vergleicht und auf der Basis der ermittelten Differenzdrehzahl das Propellerblattstellventil (6) steuert und die Propellerdrehzahl automatisch an die über die Gashebelstellung vorgegebene Motorleistung anpasst. Durch die Einhebelbedienung wird der Pilot entlastet. Der Bauteilaufwand für die redundant ausgeführte Steuerung wird verringert.
PCT/EP2009/060953 2008-09-09 2009-08-25 Steuersystem für einen flugzeugpropellerantrieb WO2010028943A2 (de)

Priority Applications (4)

Application Number Priority Date Filing Date Title
EP09782180A EP2331401A2 (de) 2008-09-09 2009-08-25 Steuersystem für einen flugzeugpropellerantrieb
US13/062,842 US20110190966A1 (en) 2008-09-09 2009-08-25 Control System For An Aircraft Propeller Drive
CA2736193A CA2736193A1 (en) 2008-09-09 2009-08-25 Control system for an aircraft propeller drive
CN2009801351854A CN102149600A (zh) 2008-09-09 2009-08-25 飞机螺旋桨驱动器的控制系统

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE102008041925.7 2008-09-09
DE102008041925A DE102008041925A1 (de) 2008-09-09 2008-09-09 Steuersystem für einen Flugzeugpropellerantrieb

Publications (2)

Publication Number Publication Date
WO2010028943A2 WO2010028943A2 (de) 2010-03-18
WO2010028943A3 true WO2010028943A3 (de) 2010-07-01

Family

ID=41693582

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/EP2009/060953 WO2010028943A2 (de) 2008-09-09 2009-08-25 Steuersystem für einen flugzeugpropellerantrieb

Country Status (6)

Country Link
US (1) US20110190966A1 (de)
EP (1) EP2331401A2 (de)
CN (1) CN102149600A (de)
CA (1) CA2736193A1 (de)
DE (1) DE102008041925A1 (de)
WO (1) WO2010028943A2 (de)

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2984275B1 (fr) * 2011-12-19 2014-09-05 Airbus Operations Sas Systeme de commande de l'energie d'un vehicule a interface unique
CN102923299B (zh) * 2012-10-31 2015-03-25 中国航天空气动力技术研究院 恒速螺旋桨变矩pid控制系统
CN105620767A (zh) * 2014-10-28 2016-06-01 中国航空工业集团公司西安飞机设计研究所 一种利用油门杆综合控制发动机和螺旋桨的方法
WO2018017733A1 (en) * 2016-07-20 2018-01-25 Deltahawk Engines, Inc. Single input engine controller and system
DE102016222652A1 (de) * 2016-11-17 2018-05-17 Robert Bosch Gmbh Verfahren und Vorrichtung zur Überwachung einer Abweichung einer ersten Drehzahl einer ersten Antriebseinheit für ein Luftfahrzeug von einer zweiten Drehzahl einer mindestens zweiten Antriebseinheit für ein Luftfahrzeug
CN106704009B (zh) * 2016-12-13 2019-10-11 安徽航瑞航空动力装备有限公司 一种活塞式航空发动机负荷协调控制方法
CN108298095A (zh) * 2017-12-15 2018-07-20 石家庄飞机工业有限责任公司 一种小型通用飞机用航煤活塞发动机动力装置
EP3543112B1 (de) * 2018-03-23 2020-10-21 Ge Avio S.r.l. System und verfahren zur kombinierten propellerdrehzahl- und propellerneigungswinkelregelung für ein turbopropellertriebwerk
CN109470486A (zh) * 2018-12-26 2019-03-15 东北农业大学 一种无人机油动发动机拉力测试试验装置及方法
US11964750B2 (en) * 2019-03-07 2024-04-23 General Electric Company Propeller speed overshoot preventing logic
CN114379770B (zh) * 2022-01-21 2024-05-14 夏青元 一种无人机电动恒速变距螺旋桨转速及桨距自动控制器
CN117075527B (zh) * 2023-10-17 2023-12-26 成都天域航通科技有限公司 一种大型固定翼货运无人机飞行控制系统

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6340289B1 (en) * 1998-04-03 2002-01-22 Aurora Flight Sciences Corporation Single lever power controller for manned and unmanned aircraft
US20040031267A1 (en) * 2002-08-16 2004-02-19 Toyota Jidosha Kabushiki Kaisha Control system for a turbo-charged diesel aircraft engine

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5029091A (en) * 1989-04-11 1991-07-02 United Technologies Corporation Ground mode control of aircraft propeller speed and pitch
US5517819A (en) * 1994-12-19 1996-05-21 General Electric Company Engine full authority digital engine control automatic mach hold
JP3990155B2 (ja) * 2000-01-14 2007-10-10 シーメンス アクチエンゲゼルシヤフト 船舶推進駆動システム
WO2002016739A2 (en) * 2000-08-21 2002-02-28 Bombardier-Rotax Gmbh & Co. Kg. Turbocharger control system and propeller control system by stepper motor
WO2004065768A2 (en) * 2003-01-22 2004-08-05 Karem Abraham E Fail-operational internal combustion engine
JP2006283621A (ja) * 2005-03-31 2006-10-19 Honda Motor Co Ltd 航空エンジンの電子制御装置

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6340289B1 (en) * 1998-04-03 2002-01-22 Aurora Flight Sciences Corporation Single lever power controller for manned and unmanned aircraft
US20040031267A1 (en) * 2002-08-16 2004-02-19 Toyota Jidosha Kabushiki Kaisha Control system for a turbo-charged diesel aircraft engine

Also Published As

Publication number Publication date
DE102008041925A1 (de) 2010-03-25
CA2736193A1 (en) 2010-03-18
WO2010028943A2 (de) 2010-03-18
CN102149600A (zh) 2011-08-10
US20110190966A1 (en) 2011-08-04
EP2331401A2 (de) 2011-06-15

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