ES2721508T3 - Dispositivo de sellado y mecanismo de superficie de control de vuelo y aeronave asociados - Google Patents
Dispositivo de sellado y mecanismo de superficie de control de vuelo y aeronave asociados Download PDFInfo
- Publication number
- ES2721508T3 ES2721508T3 ES17162428T ES17162428T ES2721508T3 ES 2721508 T3 ES2721508 T3 ES 2721508T3 ES 17162428 T ES17162428 T ES 17162428T ES 17162428 T ES17162428 T ES 17162428T ES 2721508 T3 ES2721508 T3 ES 2721508T3
- Authority
- ES
- Spain
- Prior art keywords
- control surface
- seal
- movable
- fixed part
- sealing device
- 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.)
- Active
Links
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C9/00—Adjustable control surfaces or members, e.g. rudders
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/26—Attaching the wing or tail units or stabilising surfaces
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C5/00—Stabilising surfaces
- B64C5/02—Tailplanes
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C7/00—Structures or fairings not otherwise provided for
-
- 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
- B64C9/08—Adjustable control surfaces or members, e.g. rudders bodily displaceable
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16J—PISTONS; CYLINDERS; SEALINGS
- F16J15/00—Sealings
- F16J15/16—Sealings between relatively-moving surfaces
- F16J15/18—Sealings between relatively-moving surfaces with stuffing-boxes for elastic or plastic packings
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- 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
- Y02T50/30—Wing lift efficiency
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Sealing Devices (AREA)
Abstract
Un dispositivo de sellado (100, 100') y una superficie de control móvil (40) para un mecanismo de superficie de control de vuelo (10) de una aeronave (1), el mecanismo de superficie de control de vuelo (10) que comprende una parte fija (20) y la superficie de control móvil (40), la superficie de control móvil (40) siendo acoplable a la parte fija (20) de manera móvil con relación a la parte fija (20), en donde el dispositivo de sellado (100, 100') comprende un sello fijo (120) acoplable a la parte fija (20) y un sello móvil (140, 140') unido a la superficie de control móvil (40) para moverse con el movimiento de la superficie de control móvil (40), el sello móvil (140, 140') y el sello fijo (120) cooperan entre sí para proporcionar un sello aerodinámico para el mecanismo de superficie de control de vuelo (10), en donde la superficie de control móvil (40) se dispone detrás de la parte fija (20) en la dirección de vuelo (FD) de la aeronave, el sello fijo (120) es acoplable a un borde de salida (24) de la parte fija (20), y el sello móvil (140, 140') está unido a un borde de ataque (42) de la superficie de control móvil (40), y caracterizado porque existe un corte (45) en el borde de ataque (42) de la superficie de control móvil (40), y el sello móvil (140, 140') se dispone en el corte (45) para cubrir el corte (45).
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201610169346.3A CN107226194B (zh) | 2016-03-23 | 2016-03-23 | 密封装置以及相关联的飞行控制面机构和飞行器 |
Publications (1)
Publication Number | Publication Date |
---|---|
ES2721508T3 true ES2721508T3 (es) | 2019-08-01 |
Family
ID=58401506
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
ES17162428T Active ES2721508T3 (es) | 2016-03-23 | 2017-03-22 | Dispositivo de sellado y mecanismo de superficie de control de vuelo y aeronave asociados |
Country Status (4)
Country | Link |
---|---|
US (1) | US10683080B2 (es) |
EP (1) | EP3222515B1 (es) |
CN (1) | CN107226194B (es) |
ES (1) | ES2721508T3 (es) |
Families Citing this family (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP3318783A1 (en) * | 2016-11-02 | 2018-05-09 | Airbus Operations GmbH | Fairing for an aircraft |
FR3063125B1 (fr) * | 2017-02-22 | 2019-03-29 | Airbus Operations | Joint d'etancheite souple pour un aeronef |
US10969015B2 (en) * | 2017-10-19 | 2021-04-06 | The Boeing Company | Seal system for variable geometry gaps in aircraft systems |
GB201721568D0 (en) * | 2017-12-21 | 2018-02-07 | Airbus Operations Ltd | A seal plate for an aerodynamic surface |
CN108725753B (zh) * | 2018-05-11 | 2021-06-04 | 西北工业大学 | 用于飞机活动翼面的曲面式变厚度密封板的设计方法 |
FR3106569B1 (fr) * | 2020-01-23 | 2022-02-11 | Airbus Operations Sas | Assemblage pour aéronef comprenant un système d’étanchéité à l’air amélioré entre un carénage ventral et une aile |
Family Cites Families (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2458896A (en) * | 1942-08-10 | 1949-01-11 | Curtiss Wright Corp | Differential balance for airfoils |
US2461745A (en) * | 1944-12-28 | 1949-02-15 | United Aircraft Corp | Hinge structure for aircraft surfaces |
DE4235266C1 (de) * | 1992-10-20 | 1993-10-21 | Bodenseewerk Geraetetech | Verbindungsanordnung zum Verbinden eines einen Suchkopf abdeckenden Domes mit der Struktur eines Flugkörpers |
US5388788A (en) * | 1993-12-16 | 1995-02-14 | The Boeing Company | Hinge fairings for control surfaces |
FR2718707B1 (fr) * | 1994-04-18 | 1996-07-12 | Aerospatiale | Dispositif de protection d'une charnière de gouverne, notamment pour aéronef. |
US7051982B1 (en) | 1998-03-27 | 2006-05-30 | Bae Systems Plc | Fairing arrangements for aircraft |
US7611099B2 (en) * | 2005-09-07 | 2009-11-03 | The Boeing Company | Seal assemblies for use with drooped spoilers and other control surfaces on aircraft |
DE102006027707A1 (de) * | 2006-06-14 | 2007-12-20 | Airbus Deutschland Gmbh | Heckstruktur für ein Luft- oder Raumfahrzeug |
FR2903662B1 (fr) * | 2006-07-12 | 2009-06-12 | Airbus France Sas | Cone arriere d'un avion. |
GB0908370D0 (en) * | 2009-05-15 | 2009-06-24 | Airbus Uk Ltd | A hinge sealing element and an assembly including said element |
GB0911012D0 (en) * | 2009-06-25 | 2009-08-12 | Airbus Operations Ltd | Cross-bleed dam |
CN102009742A (zh) * | 2010-07-01 | 2011-04-13 | 北京航空航天大学 | 基于舵面吹/吸气的主动流动控制设备 |
FR2992629B1 (fr) * | 2012-06-27 | 2014-09-12 | Airbus Operations Sas | Dispositif de liaison mecanique d'une gouverne a un element structural fixe d'aeronef et element de voilure d'aeronef equipe de ce dispositif |
-
2016
- 2016-03-23 CN CN201610169346.3A patent/CN107226194B/zh active Active
-
2017
- 2017-03-22 US US15/466,743 patent/US10683080B2/en active Active
- 2017-03-22 EP EP17162428.1A patent/EP3222515B1/en active Active
- 2017-03-22 ES ES17162428T patent/ES2721508T3/es active Active
Also Published As
Publication number | Publication date |
---|---|
US20170274977A1 (en) | 2017-09-28 |
EP3222515A1 (en) | 2017-09-27 |
US10683080B2 (en) | 2020-06-16 |
CN107226194A (zh) | 2017-10-03 |
EP3222515B1 (en) | 2019-01-23 |
CN107226194B (zh) | 2022-04-05 |
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