CA3042316A1 - Aile d'aeronef comprenant un volet mobile de bord de fuite entraine par un moteur electrique lineaire - Google Patents

Aile d'aeronef comprenant un volet mobile de bord de fuite entraine par un moteur electrique lineaire Download PDF

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Publication number
CA3042316A1
CA3042316A1 CA3042316A CA3042316A CA3042316A1 CA 3042316 A1 CA3042316 A1 CA 3042316A1 CA 3042316 A CA3042316 A CA 3042316A CA 3042316 A CA3042316 A CA 3042316A CA 3042316 A1 CA3042316 A1 CA 3042316A1
Authority
CA
Canada
Prior art keywords
wing
flap
trailing edge
carriage
edge flap
Prior art date
Legal status (The legal status 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 status listed.)
Pending
Application number
CA3042316A
Other languages
English (en)
Inventor
Hugues LANGER
Steve SCIARRABONE
Stephane Debaisieux
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Sonaca SA
Original Assignee
Sonaca SA
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 Sonaca SA filed Critical Sonaca SA
Publication of CA3042316A1 publication Critical patent/CA3042316A1/fr
Pending legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/14—Adjustable control surfaces or members, e.g. rudders forming slots
    • B64C9/16—Adjustable control surfaces or members, e.g. rudders forming slots at the rear of the wing
    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02K—DYNAMO-ELECTRIC MACHINES
    • H02K41/00—Propulsion systems in which a rigid body is moved along a path due to dynamo-electric interaction between the body and a magnetic field travelling along the path
    • H02K41/02—Linear motors; Sectional motors
    • H02K41/03—Synchronous motors; Motors moving step by step; Reluctance motors
    • H02K41/031—Synchronous motors; Motors moving step by step; Reluctance motors of the permanent magnet type
    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02K—DYNAMO-ELECTRIC MACHINES
    • H02K7/00—Arrangements for handling mechanical energy structurally associated with dynamo-electric machines, e.g. structural association with mechanical driving motors or auxiliary dynamo-electric machines
    • H02K7/14—Structural association with mechanical loads, e.g. with hand-held machine tools or fans
    • 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
    • Y02T50/40—Weight reduction

Landscapes

  • Engineering & Computer Science (AREA)
  • Power Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Electromagnetism (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Transmission Devices (AREA)
  • Linear Motors (AREA)

Abstract

L'invention concerne une aile d'aéronef comprenant un volet mobile de bord de fuite (16), l'aile comprenant un dispositif (50) de mise en mouvement de ce volet, le dispositif étant équipé : - d'une poutre (51) portant un rail de guidage; - d'un chariot (52a) monté mobile sur le rail (20); - d'une liaison articulée (40a) entre le chariot (52a) et une ferrure (30) solidaire du volet; - d'un organe de basculement (29) du volet mobile; - d'une liaison articulée (40b) entre la ferrure (30) et l'organe de basculement (29); et - d'une liaison articulée (40c) entre l'organe de basculement (29) et la poutre (51). Selon l'invention, le dispositif (50) comprend un moteur électrique linéaire (22) comportant un ensemble primaire (52) équipé du chariot (52a) qui intègre des bobines (55), et un ensemble secondaire (54) comportant une voie magnétique agencée sur le rail (20).
CA3042316A 2016-11-04 2017-11-02 Aile d'aeronef comprenant un volet mobile de bord de fuite entraine par un moteur electrique lineaire Pending CA3042316A1 (fr)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
BE2016/5823A BE1024276B1 (fr) 2016-11-04 2016-11-04 Aile d’aeronef comprenant un volet mobile de bord de fuite entraine par un moteur electrique lineaire
BE2016/5823 2016-11-04
PCT/EP2017/078003 WO2018083145A1 (fr) 2016-11-04 2017-11-02 Aile d'aeronef comprenant un volet mobile de bord de fuite entraine par un moteur electrique lineaire

Publications (1)

Publication Number Publication Date
CA3042316A1 true CA3042316A1 (fr) 2018-05-11

Family

ID=57326131

Family Applications (1)

Application Number Title Priority Date Filing Date
CA3042316A Pending CA3042316A1 (fr) 2016-11-04 2017-11-02 Aile d'aeronef comprenant un volet mobile de bord de fuite entraine par un moteur electrique lineaire

Country Status (3)

Country Link
BE (1) BE1024276B1 (fr)
CA (1) CA3042316A1 (fr)
WO (1) WO2018083145A1 (fr)

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4542869A (en) * 1983-06-23 1985-09-24 Mcdonnell Douglas Corporation Flap mechanism
US5686907A (en) 1995-05-15 1997-11-11 The Boeing Company Skew and loss detection system for individual high lift devices
DE102004006940B4 (de) * 2004-02-12 2009-02-26 Airbus Deutschland Gmbh Landeklappenführung für Luftfahrzeuge
DE102006036464B4 (de) * 2006-08-04 2009-08-20 Airbus Deutschland Gmbh Hochauftriebssystem für ein Flugzeug
US9281735B2 (en) * 2012-01-05 2016-03-08 Rensselaer Polytechnic Institute Flux-switching linear permanent magnet machine with yokeless translator
JP2016078584A (ja) * 2014-10-15 2016-05-16 三菱航空機株式会社 航空機
CN205610454U (zh) * 2016-04-28 2016-09-28 深圳线马科技有限公司 有铁芯永磁同步直线电机

Also Published As

Publication number Publication date
BE1024276B1 (fr) 2018-01-11
WO2018083145A1 (fr) 2018-05-11
BR112019008662A2 (pt) 2019-07-09

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Effective date: 20221012

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