WO2009141484A3 - Métodos y sistemas para la reducción del fenómeno de acoplamiento estructural en el sistema de control de un mástil de reabastecimiento en vuelo - Google Patents

Métodos y sistemas para la reducción del fenómeno de acoplamiento estructural en el sistema de control de un mástil de reabastecimiento en vuelo Download PDF

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Publication number
WO2009141484A3
WO2009141484A3 PCT/ES2009/070176 ES2009070176W WO2009141484A3 WO 2009141484 A3 WO2009141484 A3 WO 2009141484A3 ES 2009070176 W ES2009070176 W ES 2009070176W WO 2009141484 A3 WO2009141484 A3 WO 2009141484A3
Authority
WO
WIPO (PCT)
Prior art keywords
systems
boom
controlling
flexible mode
reducing
Prior art date
Application number
PCT/ES2009/070176
Other languages
English (en)
French (fr)
Other versions
WO2009141484A2 (es
Inventor
Carlos ÁVILA APARICIO
Daniel PELÁEZ FERNÁNDEZ
Melchor Barrio Mendez
Original Assignee
Eads Construcciones Aeronauticas, S.A
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 Eads Construcciones Aeronauticas, S.A filed Critical Eads Construcciones Aeronauticas, S.A
Priority to EP09749968A priority Critical patent/EP2308755B1/en
Publication of WO2009141484A2 publication Critical patent/WO2009141484A2/es
Publication of WO2009141484A3 publication Critical patent/WO2009141484A3/es

Links

Classifications

    • 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
    • B64D39/00—Refuelling during flight

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Jib Cranes (AREA)

Abstract

Un método de control de un mástil (11) de reabastecimiento en vuelo para aumentar el amortiguamiento de su desplazamiento mediante un movimiento de unas superficies de control (16) relacionado con su velocidad angular que comprende los siguientes pasos: a) Se disponen al menos dos sensores (32, 33) en dos secciones del mástil (11) situadas en lados opuestos del valle (41 ) del modo flexible dominante (40) para cualquier longitud de su extensión telescópica (12) y se determinan en ellas los módulos (D1, D2) de las deformadas angulares del modo flexible dominante (40); b) Se obtienen las velocidades angulares (Q1, Q2) a partir de los datos proporcionados por dichos sensores (32, 33); c) Se obtiene la velocidad angular Q no afectada por la resonancia del modo flexible dominante (40) como una función de dichas velocidades angulares (Q1, Q2) y dichos módulos (D1, D2) que elimina la componente del movimiento elástico del modo flexible dominante (40). La invención también se refiere a un sistema de control y a un programa de ordenador para ejecutar dicho método.
PCT/ES2009/070176 2008-05-22 2009-05-21 Métodos y sistemas para la reducción del fenómeno de acoplamiento estructural en el sistema de control de un mástil de reabastecimiento en vuelo WO2009141484A2 (es)

Priority Applications (1)

Application Number Priority Date Filing Date Title
EP09749968A EP2308755B1 (en) 2008-05-22 2009-05-21 Methods and systems for reducing the structural coupling phenomenon in systems for controlling an air refuelling boom

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
ES200801498 2008-05-22
ESP200801498 2008-05-22

Publications (2)

Publication Number Publication Date
WO2009141484A2 WO2009141484A2 (es) 2009-11-26
WO2009141484A3 true WO2009141484A3 (es) 2010-03-25

Family

ID=41340613

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/ES2009/070176 WO2009141484A2 (es) 2008-05-22 2009-05-21 Métodos y sistemas para la reducción del fenómeno de acoplamiento estructural en el sistema de control de un mástil de reabastecimiento en vuelo

Country Status (3)

Country Link
US (1) US8332081B2 (es)
EP (1) EP2308755B1 (es)
WO (1) WO2009141484A2 (es)

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EP2528820B1 (en) * 2010-01-29 2016-01-13 The Boeing Company A hoist cable management system for a refueling boom
US9150310B1 (en) * 2010-09-10 2015-10-06 The Boeing Company Methods and systems for directing remote aerial refueling operations
GB2500669B (en) * 2012-03-29 2016-03-30 Icon Polymer Group Hose for conveying fluid
US9038954B2 (en) * 2012-07-23 2015-05-26 The Boeing Company Refueling boom disconnection system
DK3308643T3 (da) 2013-09-18 2021-10-25 Horsch Leeb Application Systems Gmbh Anordning til udbringning af flydende og/eller faste virksomme stoffer og fremgangsmåde til styring af en sådan anordning
DK3065530T3 (da) 2013-11-10 2022-06-13 Horsch Leeb Application Systems Gmbh Apparat til udbringning af flydende og/eller faste virkestoffer og fremgangsmåde til styring af et sådant apparat
DE102015102975A1 (de) 2015-03-02 2016-09-08 Horsch Leeb Application Systems Gmbh Vorrichtung zum Ausbringen von flüssigen und/oder festen Wirkstoffen und Verfahren zur Steuerung einer solchen Vorrichtung
US10703499B2 (en) 2018-05-21 2020-07-07 Textron Systems Corporation In-flight aircraft refueling by jettisoning and onboarding replaceable fuel tanks
CN115424496B (zh) * 2022-08-31 2023-09-26 北京蓝天航空科技股份有限公司 空中加油训练模拟系统

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Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3432468A1 (de) * 1984-09-04 1986-03-13 Messerschmitt Boelkow Blohm Betankungseinrichtung fuer flugzeuge waehrend des fluges
EP0780292A1 (en) * 1995-12-22 1997-06-25 The Boeing Company Actuated roll axis aerial refueling boom
EP1705116A2 (en) * 2005-03-24 2006-09-27 The Boeing Company Systems and methods for automatically and semiautomatically controlling aircraft refueling

Also Published As

Publication number Publication date
US8332081B2 (en) 2012-12-11
EP2308755B1 (en) 2013-03-27
EP2308755A2 (en) 2011-04-13
WO2009141484A2 (es) 2009-11-26
US20090292406A1 (en) 2009-11-26

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