ES2179286T3 - Instalacion de discos de freno de carbono para unidad de frenado y aeronave, y procedimiento de ensamblaje de discos segun dicha instalacion. - Google Patents
Instalacion de discos de freno de carbono para unidad de frenado y aeronave, y procedimiento de ensamblaje de discos segun dicha instalacion.Info
- Publication number
- ES2179286T3 ES2179286T3 ES97402513T ES97402513T ES2179286T3 ES 2179286 T3 ES2179286 T3 ES 2179286T3 ES 97402513 T ES97402513 T ES 97402513T ES 97402513 T ES97402513 T ES 97402513T ES 2179286 T3 ES2179286 T3 ES 2179286T3
- Authority
- ES
- Spain
- Prior art keywords
- installation
- braking
- side stator
- stators
- rotors
- 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.)
- Expired - Lifetime
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
- F16D2055/0004—Parts or details of disc brakes
- F16D2055/0058—Fully lined, i.e. braking surface extending over the entire disc circumference
-
- 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
- F16D2055/0095—Plural rotors with different properties, e.g. to influence working conditions like wear or temperature
-
- 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
- F16D65/00—Parts or details
- F16D65/02—Braking members; Mounting thereof
- F16D65/12—Discs; Drums for disc brakes
- F16D65/125—Discs; Drums for disc brakes characterised by the material used for the disc body
- F16D65/126—Discs; Drums for disc brakes characterised by the material used for the disc body the material being of low mechanical strength, e.g. carbon, beryllium; Torque transmitting members therefor
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Braking Arrangements (AREA)
Abstract
LA INVENCION CONSISTE EN UN DISPOSITIVO DE DISCOS DE FRENO DE CARBONO PARA UNIDADES DE FRENADO DE AERONAVES, QUE COMPRENDE UNA ALTERNANCIA DE ESTATORES ACOPLADOS A UN TUBO DE TORSION Y DE ROTORES ACOPLADOS A LA RUEDA DE QUE SE TRATE. EL DISPOSITIVO SE ORGANIZA SEGUN DOS CONFIGURACIONES, QUE CORRESPONDEN A UN FUNCIONAMIENTO POR CADA DOS CARRERAS DE DESGASTE SUCESIVAS DE LOS PISTONES DE LA CORONA DE FRENADO. LA PRIMERA CONFIGURACION COMPRENDE UN GRUPO CENTRAL DE ROTORES Y ESTATORES (RI, SJ), DISPUESTO ENTRE UN ESTATOR LATERAL DELANTERO (SAV) Y UN ESTATOR LATERAL TRASERO (SAR); LA SEGUNDA CONFIGURACION COMPRENDE EL MISMO ESTATOR LATERAL DELANTERO (SAV) Y LOS MISMOS ROTORES Y ESTATORES (RI, SJ) DEL GRUPO CENTRAL, PERO DISPUESTOS ENTRE UN DISCO DE CALCE (C), CUYO GROSOR ES INFERIOR A LA CARRERA DE DESGASTE (D) DE LOS PISTONES, Y UN NUEVO ESTATOR LATERAL TRASERO (SAR), CUYO GROSOR ES SUPERIOR AL DEL ESTATOR LATERAL TRASERO ANTERIOR.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR9613338A FR2755094B1 (fr) | 1996-10-31 | 1996-10-31 | Agencement de disques de frein en carbone pour unite de freinage d'aeronef, et procede d'assemblage de disques selon un tel agencement |
Publications (1)
Publication Number | Publication Date |
---|---|
ES2179286T3 true ES2179286T3 (es) | 2003-01-16 |
Family
ID=9497242
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
ES97402513T Expired - Lifetime ES2179286T3 (es) | 1996-10-31 | 1997-10-23 | Instalacion de discos de freno de carbono para unidad de frenado y aeronave, y procedimiento de ensamblaje de discos segun dicha instalacion. |
Country Status (5)
Country | Link |
---|---|
US (1) | US5992577A (es) |
EP (1) | EP0840029B1 (es) |
DE (1) | DE69713987T2 (es) |
ES (1) | ES2179286T3 (es) |
FR (1) | FR2755094B1 (es) |
Families Citing this family (23)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6532637B1 (en) | 1997-06-06 | 2003-03-18 | Honeywell International Inc. | Method of converting an aircraft brake assembly and a convertible aircraft brake assembly |
US6119817A (en) * | 1997-06-06 | 2000-09-19 | Alliedsignal Inc. | Method of converting an aircraft brake assembly |
US5926932A (en) | 1997-06-06 | 1999-07-27 | Alliedsignal Inc. | Methods of converting aircraft brake assemblies |
FR2786239B1 (fr) * | 1998-11-25 | 2001-02-16 | Messier Bugatti | Dispositif de friction a disques a commande pneumatique pour transmission |
US7168528B1 (en) * | 1999-05-11 | 2007-01-30 | Goodrich Corporation | Three run disk brake stack and method of assembly |
CA2318688C (en) * | 1999-09-13 | 2008-11-18 | The B.F. Goodrich Company | Aircraft landing gear with integrated brake actuation system |
US6340075B1 (en) * | 1999-11-24 | 2002-01-22 | The B. F. Goodrich Company | Three run disk brake stack and method of assembly |
US7369973B2 (en) | 2000-06-29 | 2008-05-06 | Object Reservoir, Inc. | Method and system for representing reservoir systems |
US7104366B2 (en) * | 2002-12-11 | 2006-09-12 | Honeywell International | Method of increasing friction material utilization for carbon brakes |
FR2859259B1 (fr) | 2003-08-28 | 2006-02-03 | Messier Bugatti | Ensemble de freinage d'aeronef |
US7766130B2 (en) * | 2004-11-19 | 2010-08-03 | Honeywell International Inc. | Wear pin assemblies for carbon-carbon composite brake systems |
US7556128B2 (en) * | 2005-10-31 | 2009-07-07 | Warner Electric Technology Llc | Dual actuator friction brake assembly |
US7900751B2 (en) * | 2006-02-01 | 2011-03-08 | Honeywell International Inc. | Method and brake disc assembly to utilize worn refurbished brake material |
GB0702500D0 (en) | 2007-02-09 | 2007-03-21 | Dunlop Aerospace Ltd | Braking |
EP2215375B1 (de) * | 2007-10-10 | 2016-11-16 | BorgWarner Inc. | Verfahren zur montage einer reibschlüssig arbeitenden einrichtung, reibschlüssig arbeitende einrichtung mit einem reiblamellensatz und reiblamellensatz für eine solche reibschlüssig arbeitende einrichtung |
FR3013412B1 (fr) * | 2013-11-21 | 2015-12-25 | Messier Bugatti Dowty | Procede de renovation et d’utilisation de disques de frein de type stator arriere a plots, disque assemble et pile de disques correspondante. |
US10473171B2 (en) | 2017-05-15 | 2019-11-12 | Goodrich Corporation | Extended torque tube |
US10228030B2 (en) * | 2017-05-15 | 2019-03-12 | Goodrich Corporation | Multi-disk brake assembly with travel limit pin |
US10274034B2 (en) | 2017-07-12 | 2019-04-30 | Goodrich Corporation | Wear liner with integrated torque button |
US10941823B2 (en) | 2017-11-27 | 2021-03-09 | Goodrich Corporation | Segmented wear liner |
US10724591B2 (en) | 2017-11-27 | 2020-07-28 | Goodrich Corporation | Brake assembly with disks of variable thickness and methods for disk reuse |
FR3085453B1 (fr) | 2018-08-29 | 2020-11-20 | Safran Landing Systems | Disque arriere d’une pile de disques en carbone de frein d’aeronef equipe de plots, et frein faisant application |
US11834159B2 (en) * | 2021-10-18 | 2023-12-05 | Goodrich Corporation | Torque button bushing |
Family Cites Families (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR1523402A (fr) * | 1967-03-22 | 1968-05-03 | Hispano Suiza Lallemant Soc | Perfectionnements apportés aux freins à disques multiples, notamment pour roues d'aviation |
US4742895A (en) * | 1984-07-02 | 1988-05-10 | The B. F. Goodrich Company | Disk brake assembly |
US4613017A (en) | 1984-07-02 | 1986-09-23 | The B. F. Goodrich Company | Disk brake and method of assembly |
GB8813518D0 (en) * | 1988-06-08 | 1988-07-13 | Dunlop Ltd | Improvements in multi-disc brakes |
CA2004091A1 (fr) * | 1988-11-29 | 1990-05-29 | Jean Guichard | Freins a disques multiples en carbone |
US5509507A (en) * | 1989-06-01 | 1996-04-23 | Dunlop Limited A British Company | Multi-disc brakes |
US4982818A (en) * | 1989-10-17 | 1991-01-08 | Allied-Signal Inc. | Cyclic brake disc overhaul technique and structure |
US5099960A (en) * | 1990-07-27 | 1992-03-31 | Aircraft Braking Systems Corp. | Composite brake disk and method of extending the braking service life thereof |
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 |
US5551534A (en) * | 1995-06-05 | 1996-09-03 | Aircraft Braking Systems Corp. | Pressure balanced brake stack |
US5862890A (en) * | 1996-01-16 | 1999-01-26 | Mcdonnell Douglas Corporation | Restrained aircraft brake apparatus |
-
1996
- 1996-10-31 FR FR9613338A patent/FR2755094B1/fr not_active Expired - Lifetime
-
1997
- 1997-10-23 ES ES97402513T patent/ES2179286T3/es not_active Expired - Lifetime
- 1997-10-23 DE DE69713987T patent/DE69713987T2/de not_active Expired - Lifetime
- 1997-10-23 EP EP97402513A patent/EP0840029B1/fr not_active Expired - Lifetime
- 1997-10-29 US US08/959,987 patent/US5992577A/en not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
DE69713987T2 (de) | 2003-03-27 |
US5992577A (en) | 1999-11-30 |
EP0840029B1 (fr) | 2002-07-17 |
EP0840029A1 (fr) | 1998-05-06 |
FR2755094B1 (fr) | 1998-11-27 |
DE69713987D1 (de) | 2002-08-22 |
FR2755094A1 (fr) | 1998-04-30 |
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