BRPI0403306A - Conjunto de frenagem de aeronave - Google Patents

Conjunto de frenagem de aeronave

Info

Publication number
BRPI0403306A
BRPI0403306A BR0403306-0A BRPI0403306A BRPI0403306A BR PI0403306 A BRPI0403306 A BR PI0403306A BR PI0403306 A BRPI0403306 A BR PI0403306A BR PI0403306 A BRPI0403306 A BR PI0403306A
Authority
BR
Brazil
Prior art keywords
assembly
aircraft braking
braking set
wheel
shaft
Prior art date
Application number
BR0403306-0A
Other languages
English (en)
Inventor
Jean Narcy
Philippe Chico
Original Assignee
Messier Bugatti
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 Messier Bugatti filed Critical Messier Bugatti
Publication of BRPI0403306A publication Critical patent/BRPI0403306A/pt
Publication of BRPI0403306B1 publication Critical patent/BRPI0403306B1/pt

Links

Classifications

    • 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
    • F16D—COUPLINGS FOR TRANSMITTING ROTATION; CLUTCHES; BRAKES
    • F16D55/00—Brakes with substantially-radial braking surfaces pressed together in axial direction, e.g. disc brakes
    • F16D55/24—Brakes with substantially-radial braking surfaces pressed together in axial direction, e.g. disc brakes with a plurality of axially-movable discs, lamellae, or pads, pressed from one side towards an axially-located member
    • F16D55/26—Brakes with substantially-radial braking surfaces pressed together in axial direction, e.g. disc brakes with a plurality of axially-movable discs, lamellae, or pads, pressed from one side towards an axially-located member without self-tightening action
    • F16D55/36—Brakes with a plurality of rotating discs all lying side by side
    • 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
    • F16D—COUPLINGS FOR TRANSMITTING ROTATION; CLUTCHES; BRAKES
    • F16D55/00—Brakes with substantially-radial braking surfaces pressed together in axial direction, e.g. disc brakes
    • F16D2055/0075—Constructional features of axially engaged brakes
    • F16D2055/0091—Plural actuators arranged side by side on the same side of the rotor
    • 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
    • F16D—COUPLINGS FOR TRANSMITTING ROTATION; CLUTCHES; BRAKES
    • F16D2121/00—Type of actuator operation force
    • F16D2121/18—Electric or magnetic
    • F16D2121/24—Electric or magnetic using motors
    • 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
    • F16D—COUPLINGS FOR TRANSMITTING ROTATION; CLUTCHES; BRAKES
    • F16D2250/00—Manufacturing; Assembly
    • F16D2250/0084—Assembly or disassembly

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Braking Arrangements (AREA)

Abstract

"CONJUNTO DE FRENAGEM DE AERONAVE". A invenção refere-se a um conjunto de frenagem de aeronave que compreende uma pilha de discos (101) circundando um eixo de roda (11) coaxialmente, o dita pilha sendo constituída alternativamente de discos rotores (102) ligados em rotação com a roda (12), e discos estatores (103) ligados em rotação com um tubo de torção, e sendo pressionada entre uma peça traseira de retenção (106) e os impulsores (122) de uma pluralidade de acionadores eletromecânicos (120) dispostos circunferencialmente sobre uma coroa dianteira de suporte. De acordo com a invenção, o tubo de torção (111) e a coroa (112) suportando os acionadores eletromecânicos (120) constituem um conjunto monobloco (110) que é fixado ao eixo (11), e a peça traseira de retenção (106) é fixada de maneira desmontável sobre o dito conjunto monobloco (110) em uma extremidade deste último.
BRPI0403306-0A 2003-08-28 2004-08-18 conjunto de frenagem de aeronave. BRPI0403306B1 (pt)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0310246A FR2859259B1 (fr) 2003-08-28 2003-08-28 Ensemble de freinage d'aeronef

Publications (2)

Publication Number Publication Date
BRPI0403306A true BRPI0403306A (pt) 2005-05-31
BRPI0403306B1 BRPI0403306B1 (pt) 2013-02-05

Family

ID=34089866

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI0403306-0A BRPI0403306B1 (pt) 2003-08-28 2004-08-18 conjunto de frenagem de aeronave.

Country Status (8)

Country Link
US (1) US20050056499A1 (pt)
EP (1) EP1510719B1 (pt)
AT (1) ATE392565T1 (pt)
BR (1) BRPI0403306B1 (pt)
CA (1) CA2478879C (pt)
DE (1) DE602004013093T2 (pt)
ES (1) ES2304155T3 (pt)
FR (1) FR2859259B1 (pt)

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2862280B1 (fr) * 2003-11-14 2006-03-03 Messier Bugatti Atterrisseur, frein pour roue d'aeronef, ensemble de roue freinee d'aeronef, et procede de maintenance d'un tel atterrisseur
US7228945B2 (en) * 2005-03-16 2007-06-12 Hr Textron, Inc. Techniques for employing electric brakes to control movement of rotatable components
FR2917064B1 (fr) 2007-06-05 2010-05-14 Messier Bugatti Frein adapte a un essieu conique
GB201001176D0 (en) * 2010-01-26 2010-03-10 Airbus Operations Ltd Aircraft braking actuator
GB201001175D0 (en) * 2010-01-26 2010-03-10 Airbus Operations Ltd Aircraft steering actuator
FR2970698B1 (fr) * 2011-01-21 2013-10-04 Messier Dowty Sa Dispositif de freinage et d'entrainement en rotation d'une roue d'aeronef
FR3026717B1 (fr) * 2014-10-03 2016-11-25 Messier Bugatti Dowty Atterrisseur d'aeronef.
FR3037563B1 (fr) * 2015-06-16 2018-10-12 Safran Landing Systems Procede de maintenance d'un frein d'aeronef
US9995353B2 (en) * 2015-12-21 2018-06-12 Goodrich Corporation Modified actuator design to improve load distribution and damping
US10309468B2 (en) * 2017-10-20 2019-06-04 Goodrich Corporation Torque plate barrel having blended barrel support pedestal
CN107878737A (zh) * 2017-12-01 2018-04-06 北京北摩高科摩擦材料股份有限公司 一种飞机刹车机轮
GB2583706A (en) 2019-04-23 2020-11-11 Airbus Operations Ltd Aircraft braking system

Family Cites Families (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2934174A (en) * 1957-07-09 1960-04-26 Sarl Rech S Etudes Production Multi-disc brake
FR1523402A (fr) * 1967-03-22 1968-05-03 Hispano Suiza Lallemant Soc Perfectionnements apportés aux freins à disques multiples, notamment pour roues d'aviation
GB1220351A (en) * 1967-05-18 1971-01-27 Dunlop Co Ltd Improvements in disc brakes
JPS5230464Y1 (pt) * 1969-04-07 1977-07-12
GB1443709A (en) * 1972-12-19 1976-07-21 Dunlop Ltd Disc brakes
GB1446312A (en) * 1972-12-21 1976-08-18 Dunlop Ltd Disc brakes
US3977631A (en) * 1975-06-04 1976-08-31 The Boeing Company Aircraft wheel drive apparatus and method
US4742895A (en) 1984-07-02 1988-05-10 The B. F. Goodrich Company Disk brake assembly
US5509507A (en) 1989-06-01 1996-04-23 Dunlop Limited A British Company Multi-disc brakes
FR2668440B1 (fr) * 1990-10-30 1992-12-24 Alsthom Gec Systeme de freinage pour vehicule ferroviaire.
US5321876A (en) * 1992-12-10 1994-06-21 Allied-Signal Inc. Method of converting aircraft brake assemblies
US5494138A (en) 1994-10-14 1996-02-27 Alliedsignal, Inc. Aircraft brake torque transfer assembly
US5558186A (en) 1995-05-24 1996-09-24 The Bfgoodrich Company Friction disk with renewable wear faces
US5862890A (en) 1996-01-16 1999-01-26 Mcdonnell Douglas Corporation Restrained aircraft brake apparatus
US5944147A (en) * 1996-06-28 1999-08-31 Alliedsignal Inc. Integrated aircraft wheel, brake and axle
FR2755094B1 (fr) 1996-10-31 1998-11-27 Messier Bugatti Agencement de disques de frein en carbone pour unite de freinage d'aeronef, et procede d'assemblage de disques selon un tel agencement
US6003640A (en) * 1997-05-09 1999-12-21 The B.F. Goodrich Company Electronic braking system with brake wear measurement and running clearance adjustment
US6095293A (en) 1998-02-13 2000-08-01 The B. F. Goodrich Company Aircraft brake and method with electromechanical actuator modules
DE60025230T2 (de) 1999-09-13 2006-09-07 Goodrich Corp. Elektrisches bremsbetätigungsmodul für flugzeuge
CA2318688C (en) 1999-09-13 2008-11-18 The B.F. Goodrich Company Aircraft landing gear with integrated brake actuation system

Also Published As

Publication number Publication date
CA2478879C (fr) 2008-10-07
FR2859259B1 (fr) 2006-02-03
DE602004013093D1 (de) 2008-05-29
ATE392565T1 (de) 2008-05-15
CA2478879A1 (fr) 2005-02-28
EP1510719B1 (fr) 2008-04-16
ES2304155T3 (es) 2008-09-16
DE602004013093T2 (de) 2009-07-02
US20050056499A1 (en) 2005-03-17
EP1510719A1 (fr) 2005-03-02
FR2859259A1 (fr) 2005-03-04
BRPI0403306B1 (pt) 2013-02-05

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Legal Events

Date Code Title Description
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 18/08/2004, OBSERVADAS AS CONDICOES LEGAIS.

B25D Requested change of name of applicant approved
B25G Requested change of headquarter approved