BRPI0711118A2 - escora de interconexão para colocação entre flaps de pouso adjacentes de uma aeronave - Google Patents

escora de interconexão para colocação entre flaps de pouso adjacentes de uma aeronave Download PDF

Info

Publication number
BRPI0711118A2
BRPI0711118A2 BRPI0711118-5A BRPI0711118A BRPI0711118A2 BR PI0711118 A2 BRPI0711118 A2 BR PI0711118A2 BR PI0711118 A BRPI0711118 A BR PI0711118A BR PI0711118 A2 BRPI0711118 A2 BR PI0711118A2
Authority
BR
Brazil
Prior art keywords
strut
longitudinal direction
damping device
aircraft
placement
Prior art date
Application number
BRPI0711118-5A
Other languages
English (en)
Inventor
Susanne Versluis
Original Assignee
Airbus Gmbh
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 Airbus Gmbh filed Critical Airbus Gmbh
Publication of BRPI0711118A2 publication Critical patent/BRPI0711118A2/pt

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/14—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
    • B64C9/04—Adjustable control surfaces or members, e.g. rudders with compound dependent movements
    • 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
    • B64D45/00—Aircraft indicators or protectors not otherwise provided for
    • B64D45/0005—Devices specially adapted to indicate the position of a movable element of the aircraft, e.g. landing gear
    • 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
    • F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
    • F16F7/00—Vibration-dampers; Shock-absorbers
    • F16F7/12—Vibration-dampers; Shock-absorbers using plastic deformation of members
    • F16F7/125—Units with a telescopic-like action as one member moves into, or out of a second member
    • 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
    • F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
    • F16F9/00—Springs, vibration-dampers, shock-absorbers, or similarly-constructed movement-dampers using a fluid or the equivalent as damping medium
    • F16F9/32—Details
    • F16F9/58—Stroke limiting stops, e.g. arranged on the piston rod outside the cylinder
    • 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
    • B64D45/00—Aircraft indicators or protectors not otherwise provided for
    • B64D45/0005—Devices specially adapted to indicate the position of a movable element of the aircraft, e.g. landing gear
    • B64D2045/001—Devices specially adapted to indicate the position of a movable element of the aircraft, e.g. landing gear for indicating symmetry of flaps deflection
    • 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)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Vibration Dampers (AREA)
  • Vibration Prevention Devices (AREA)

Abstract

ESCORA DE INTERCONEXãO PARA COLOCAçãO ENTRE FLAPS DE POUSO ADJACENTES DE UMA AERONAVE. Uma escora de interconexão (10,10') é divulgada, a qual compreende dois elementos de escora arranjados de maneira coaxial (20, 21, 20', 21') que podem ser deslocados um em relação ao outro na direção longitudinal (L) da escora de interconexão (10,10'), dois batentes extremos que definem a capacidade de deslocamento recíproca dos dois elementos de escora (20, 21, 20', 21'), bem como dispositivo de amortecimento (30, 30', 32, 32') que quando um deslocamento permissível específico é excedido, amortece o movimento de deslocamento dos elementos de escora (20, 21, 20', 21') antes de alcançar os batentes extremos, e no qual o dispositivo de amortecimento (30, 30', 32, 32') consiste em um material que é plasticamete deformável na faixa de força que ocorre, o dispositivo de amortecimento (30, 30', 32, 32') sendo comprimido para amortecer o movimento de deslocamento na direção longitudinal (L) e ao mesmo tempo sendo submetido a um aumento de seção transversal transversalmente à direção longitudinal (L) por meio da compressão.
BRPI0711118-5A 2006-05-03 2007-04-27 escora de interconexão para colocação entre flaps de pouso adjacentes de uma aeronave BRPI0711118A2 (pt)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US79733106P 2006-05-03 2006-05-03
DE102006020554A DE102006020554B4 (de) 2006-05-03 2006-05-03 Verbindungsstrebe zur Anordnung zwischen benachbarten Landeklappen eines Flugzeuges
PCT/EP2007/054136 WO2007128708A1 (en) 2006-05-03 2007-04-27 Interconnecting strut for arranging between adjacent landing flaps of an aircraft

Publications (1)

Publication Number Publication Date
BRPI0711118A2 true BRPI0711118A2 (pt) 2011-08-30

Family

ID=38579784

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI0711118-5A BRPI0711118A2 (pt) 2006-05-03 2007-04-27 escora de interconexão para colocação entre flaps de pouso adjacentes de uma aeronave

Country Status (9)

Country Link
US (1) US8469165B2 (pt)
EP (1) EP2013511A1 (pt)
JP (1) JP2009535262A (pt)
CN (1) CN101432546B (pt)
BR (1) BRPI0711118A2 (pt)
CA (1) CA2646203A1 (pt)
DE (1) DE102006020554B4 (pt)
RU (1) RU2439392C2 (pt)
WO (1) WO2007128708A1 (pt)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103676751B (zh) * 2012-09-07 2016-05-18 苏州宝时得电动工具有限公司 自动工作设备
US10059463B2 (en) * 2014-11-26 2018-08-28 Hamilton Sundstrand Corporation Sensor system for a wing panel assembly and method of monitoring a wing panel assembly
CN107161325B (zh) * 2017-07-31 2018-09-11 中国商用飞机有限责任公司 内外襟翼交联装置
CN113374799B (zh) * 2021-07-02 2022-03-25 中国航发湖南动力机械研究所 带阻尼减震的传扭结构和航空发动机

Family Cites Families (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2642845A (en) * 1950-12-20 1953-06-23 Westinghouse Air Brake Co Piston cushioning apparatus
US2783039A (en) * 1954-07-30 1957-02-26 John O Wilson Trailer hitch shock absorber
US3605553A (en) * 1969-05-05 1971-09-20 Pier Luigi Panigati Pressure fluid operated cylinder
JPS5122578B2 (pt) 1971-11-17 1976-07-10
US4336868A (en) * 1978-05-10 1982-06-29 Textron, Inc. Composite fibrous tube energy absorber
SU846886A1 (ru) 1979-11-28 1981-07-15 Ростовское Высшее Военное Командное Учи-Лище Им. Главного Маршала Артиллериинеделина M.И. Пластинчатый амортизатор одноразовогодЕйСТВи
EP0119197B1 (en) * 1982-09-20 1988-11-02 Ford Motor Company Limited A rebound stop member for a telescopic hydraulic shock absorber
USRE33696E (en) * 1984-12-12 1991-09-24 The Paton Corporation Composite spring
SU1326815A1 (ru) 1984-12-25 1987-07-30 Предприятие П/Я В-8209 Пластический амортизатор
DE3505839A1 (de) * 1985-02-20 1986-08-21 Messerschmitt-Bölkow-Blohm GmbH, 2800 Bremen Ausfallsicherung fuer klappensysteme an flugzeugtragfluegeln
DE3522449A1 (de) * 1985-06-22 1987-01-02 Messerschmitt Boelkow Blohm Daempfungselement
DE3546236A1 (de) * 1985-12-28 1987-07-02 Bauer Fritz & Soehne Ohg Gasfeder mit endlagendaempfung
FR2608242B1 (fr) * 1986-12-12 1989-03-31 Aerospatiale Amortisseur-verin, contre-fiche le comportant, et train d'atterrissage equipe d'une telle contre-fiche
RU1768818C (ru) 1988-10-06 1992-10-15 Мариупольский металлургический институт Амортизатор
DE3930137A1 (de) 1989-09-09 1991-03-21 Bayer Ag Stossdaempfer in form eines schockabsorbers
SU1710887A1 (ru) 1989-12-14 1992-02-07 Краснодарское высшее военное командно-инженерное училище ракетных войск Пластический амортизатор
EP0850170B1 (en) * 1995-09-14 1999-03-17 Sikorsky Aircraft Corporation Energy absorbing landing gear/tail skid including means for indicating the magnitude of impact loads
CA2432613C (en) * 2000-12-18 2009-12-22 Toray Industries, Inc. Impact energy absorption device
EP1233206B1 (en) * 2001-02-14 2008-07-30 Oiles Corporation Damper and automobile seat having the damper
US7441637B2 (en) * 2004-08-06 2008-10-28 Kayaba Industry Co., Ltd. Hydraulic shock absorber
JP4528258B2 (ja) * 2005-12-22 2010-08-18 シャープ株式会社 画像形成装置

Also Published As

Publication number Publication date
EP2013511A1 (en) 2009-01-14
DE102006020554A1 (de) 2007-11-15
JP2009535262A (ja) 2009-10-01
WO2007128708A1 (en) 2007-11-15
CN101432546A (zh) 2009-05-13
CA2646203A1 (en) 2007-11-15
DE102006020554B4 (de) 2011-06-16
RU2008142965A (ru) 2010-06-10
CN101432546B (zh) 2012-03-21
US20090152064A1 (en) 2009-06-18
RU2439392C2 (ru) 2012-01-10
US8469165B2 (en) 2013-06-25

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Legal Events

Date Code Title Description
B25D Requested change of name of applicant approved

Owner name: AIRBUS OPERATIONS GMBH (DE)

Free format text: NOME ALTERADO DE: AIRBUS DEUTSCHLAND GMBH

B08F Application fees: application dismissed [chapter 8.6 patent gazette]

Free format text: REFERENTE A 7A ANUIDADE.

B08K Patent lapsed as no evidence of payment of the annual fee has been furnished to inpi [chapter 8.11 patent gazette]

Free format text: REFERENTE AO DESPACHO 8.6 PUBLICADO NA RPI 2260 DE 29/04/2014.