BR112017002081A2 - elemento de superfície de controle para uma aeronave - Google Patents

elemento de superfície de controle para uma aeronave

Info

Publication number
BR112017002081A2
BR112017002081A2 BR112017002081A BR112017002081A BR112017002081A2 BR 112017002081 A2 BR112017002081 A2 BR 112017002081A2 BR 112017002081 A BR112017002081 A BR 112017002081A BR 112017002081 A BR112017002081 A BR 112017002081A BR 112017002081 A2 BR112017002081 A2 BR 112017002081A2
Authority
BR
Brazil
Prior art keywords
reinforcement
fiber composite
aircraft
composite element
control surface
Prior art date
Application number
BR112017002081A
Other languages
English (en)
Other versions
BR112017002081B1 (pt
Inventor
Meindlhumer Martin
Seis Michael
Original Assignee
Facc Ag
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 Facc Ag filed Critical Facc Ag
Publication of BR112017002081A2 publication Critical patent/BR112017002081A2/pt
Publication of BR112017002081B1 publication Critical patent/BR112017002081B1/pt

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/02—Mounting or supporting thereof
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/32—Air braking surfaces
    • B64C9/323—Air braking surfaces associated with wings
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/20—Integral or sandwich constructions
    • 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
    • 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
    • B64C9/18—Adjustable control surfaces or members, e.g. rudders forming slots at the rear of the wing by single flaps
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/32—Air braking surfaces
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • 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

Abstract

a presente invenção refere-se a um elemento de superfície de controle (4) para uma aeronave, particularmente freio aerodinâmico, com um elemento composto de fibra (3), que apresenta uma superfície (8) circundada por ar, com um dispositivo de apoio (5) para o apoio móvel do elemento composto de fibra (3) em um componente estrutural, e com uma estrutura de reforço (9) para reforço do elemento composto de fibra (3). a estrutura de reforço (9) apresenta pelo menos um elemento de reforço, formado de modo integral com o elemento composto de fibra (3), sendo que a estrutura de reforço (9) apresenta um elemento de reforço primário (10) configurado para recepção de cargas principais, que está conectado com pelo menos um elemento de reforço secundário (11; 11?, 11??) para recepção de cargas secundárias, sendo que o elemento composto de fibra (3) apresenta uma reentrância (15) para a formação integral do elemento de reforço primário (10).
BR112017002081-5A 2014-08-11 2015-08-11 Elemento de superfície de controle para uma aeronave BR112017002081B1 (pt)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
ATA50557/2014 2014-08-11
ATA50557/2014A AT516211A1 (de) 2014-08-11 2014-08-11 Steuerflächenelement
PCT/AT2015/050196 WO2016023056A1 (de) 2014-08-11 2015-08-11 Steuerflächenelement für ein flugzeug

Publications (2)

Publication Number Publication Date
BR112017002081A2 true BR112017002081A2 (pt) 2017-12-19
BR112017002081B1 BR112017002081B1 (pt) 2022-08-09

Family

ID=54014442

Family Applications (1)

Application Number Title Priority Date Filing Date
BR112017002081-5A BR112017002081B1 (pt) 2014-08-11 2015-08-11 Elemento de superfície de controle para uma aeronave

Country Status (11)

Country Link
US (1) US10518866B2 (pt)
EP (1) EP3180243B1 (pt)
CN (1) CN107000827B (pt)
AT (1) AT516211A1 (pt)
BR (1) BR112017002081B1 (pt)
CA (1) CA2956704C (pt)
ES (1) ES2730051T3 (pt)
HR (1) HRP20190866T1 (pt)
RU (1) RU2687535C1 (pt)
SG (1) SG11201700938QA (pt)
WO (1) WO2016023056A1 (pt)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP3009344B1 (en) 2014-10-16 2019-05-29 Airbus Operations GmbH Panel structure and associated method
US20180099736A1 (en) * 2016-10-12 2018-04-12 The Boeing Company Aircraft wings, aircraft, and related methods
EP3625122A1 (en) * 2017-05-18 2020-03-25 BAE Systems PLC Door assembly for a vehicle
EP3403917A1 (en) * 2017-05-18 2018-11-21 BAE SYSTEMS plc Door assembly for a vehicle
CN108248825B (zh) * 2018-03-02 2020-12-08 西北工业大学 一种飞行器翼面结构
FR3090577A1 (fr) * 2018-12-20 2020-06-26 Daher Aerospace Elément mobile de voilure
US11046420B2 (en) * 2019-10-23 2021-06-29 The Boeing Company Trailing edge flap having a waffle grid interior structure
FR3107254A1 (fr) * 2020-02-18 2021-08-20 Airbus Operations (S.A.S.) Procédé de fabrication d’une structure aérodynamique mobile d’aéronef et structure aérodynamique mobile d’aéronef ainsi obtenue
CA3122789A1 (en) 2020-07-29 2022-01-29 The Boeing Company Bead-stiffened movable surfaces
AT524687B1 (de) 2021-05-27 2022-08-15 Facc Ag Verfahren zum Verschweißen von Faser-Kunststoff-Verbund-(FKV)-Bauteilen und Stabilisierungsvorrichtung

Family Cites Families (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5224670A (en) * 1991-09-13 1993-07-06 Grumman Aerospace Corporation Composite focused load control surface
JP2000043796A (ja) * 1998-07-30 2000-02-15 Japan Aircraft Development Corp 複合材の翼形構造およびその成形方法
US6270039B1 (en) * 1999-10-12 2001-08-07 Patria Finavicomp Oy Hinge for movable control surfaces in an aircraft and a connecting piece to be used with such a hinge
DE10013409C1 (de) 2000-03-17 2000-11-23 Daimler Chrysler Ag Verfahren und Vorrichtung zur Herstellung von faserverstärkten Bauteilen mittels eines Injektionsverfahrens
AT409482B (de) * 2001-01-26 2002-08-26 Fischer Adv Components Gmbh Einrichtung zum verbinden beweglicher teile mit strukturbauteilen von flugzeugen od. dgl.
ATE284346T1 (de) 2001-01-26 2004-12-15 Fischer Adv Components Gmbh Einrichtung zum verbinden beweglicher teile mit strukturbauteilen von flugzeugen od. dgl.
RU2184682C1 (ru) * 2001-01-31 2002-07-10 Акционерное общество открытого типа "ОКБ Сухого" Тормозной щиток летательного аппарата
CN106507753B (zh) * 2004-04-13 2010-08-04 成都飞机工业（集团）有限责任公司 轻型战斗机机翼
FI118122B (fi) * 2004-10-08 2007-07-13 Patria Aerostructures Oy Ilma-aluksen kääntyvä paneeli ja komposiittirakenteinen tukikappale
FI119726B (fi) 2006-09-26 2009-02-27 Patria Aerostructures Oy Ilma-aluksen kaarielementti, siipi, ohjainpinta sekä vakaaja
AT511113B1 (de) 2011-03-04 2013-09-15 Facc Ag Verfahren zur herstellung eines faserverbundbauteils und werkzeuganordnung hierfür
US20130011605A1 (en) * 2011-07-05 2013-01-10 Israel Aerospace Industries Ltd. Manufacture of articles formed of composite materials
CN203318675U (zh) * 2013-03-18 2013-12-04 空客(北京)工程技术中心有限公司 混合夹层结构、板式构件和飞机飞行控制部件
GB201315341D0 (en) * 2013-08-29 2013-10-09 Airbus Operations Ltd An aircraft structure and method of manufacture

Also Published As

Publication number Publication date
ES2730051T3 (es) 2019-11-07
EP3180243B1 (de) 2019-03-13
BR112017002081B1 (pt) 2022-08-09
RU2687535C1 (ru) 2019-05-14
CA2956704C (en) 2023-04-04
AT516211A1 (de) 2016-03-15
CA2956704A1 (en) 2016-02-18
HRP20190866T1 (hr) 2019-08-09
SG11201700938QA (en) 2017-03-30
US20170233061A1 (en) 2017-08-17
WO2016023056A1 (de) 2016-02-18
CN107000827A (zh) 2017-08-01
EP3180243A1 (de) 2017-06-21
US10518866B2 (en) 2019-12-31
CN107000827B (zh) 2020-09-08

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Legal Events

Date Code Title Description
B06U Preliminary requirement: requests with searches performed by other patent offices: procedure suspended [chapter 6.21 patent gazette]
B09A Decision: intention to grant [chapter 9.1 patent gazette]
B16A Patent or certificate of addition of invention granted [chapter 16.1 patent gazette]

Free format text: PRAZO DE VALIDADE: 20 (VINTE) ANOS CONTADOS A PARTIR DE 11/08/2015, OBSERVADAS AS CONDICOES LEGAIS