MX338232B - Sistema de enfriamiento de tren de aterrizaje de aeronave. - Google Patents

Sistema de enfriamiento de tren de aterrizaje de aeronave.

Info

Publication number
MX338232B
MX338232B MX2013013684A MX2013013684A MX338232B MX 338232 B MX338232 B MX 338232B MX 2013013684 A MX2013013684 A MX 2013013684A MX 2013013684 A MX2013013684 A MX 2013013684A MX 338232 B MX338232 B MX 338232B
Authority
MX
Mexico
Prior art keywords
air
landing gear
cooling system
aircraft landing
gear brake
Prior art date
Application number
MX2013013684A
Other languages
English (en)
Other versions
MX2013013684A (es
Inventor
David W Kirkbride
Darrell S Jolliffe
Original Assignee
Boeing Co
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 Boeing Co filed Critical Boeing Co
Publication of MX2013013684A publication Critical patent/MX2013013684A/es
Publication of MX338232B publication Critical patent/MX338232B/es

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C25/00—Alighting gear
    • B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface 
    • B64C25/42—Arrangement or adaptation of brakes
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B60—VEHICLES IN GENERAL
    • B60R—VEHICLES, VEHICLE FITTINGS, OR VEHICLE PARTS, NOT OTHERWISE PROVIDED FOR
    • B60R99/00—Subject matter not provided for in other groups of this subclass
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B60—VEHICLES IN GENERAL
    • B60T—VEHICLE BRAKE CONTROL SYSTEMS OR PARTS THEREOF; BRAKE CONTROL SYSTEMS OR PARTS THEREOF, IN GENERAL; ARRANGEMENT OF BRAKING ELEMENTS ON VEHICLES IN GENERAL; PORTABLE DEVICES FOR PREVENTING UNWANTED MOVEMENT OF VEHICLES; VEHICLE MODIFICATIONS TO FACILITATE COOLING OF BRAKES
    • B60T5/00—Vehicle modifications to facilitate cooling of brakes
    • 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
    • F16D65/78—Features relating to cooling
    • F16D65/84—Features relating to cooling for disc brakes
    • F16D65/847—Features relating to cooling for disc brakes with open cooling system, e.g. cooled by air
    • 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T137/00—Fluid handling
    • Y10T137/0318—Processes
    • 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T137/00—Fluid handling
    • Y10T137/6851—With casing, support, protector or static constructional installations
    • Y10T137/6855—Vehicle

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Transportation (AREA)
  • Braking Arrangements (AREA)
  • Retarders (AREA)
  • General Details Of Gearings (AREA)

Abstract

De acuerdo con una modalidad, es descrito un aparato para el enfriamiento al menos de un freno de tren de aterrizaje de una aeronave en vuelo. El aparato incluye un montaje de manipulación de aire que es acoplado con la aeronave. El montaje de manipulación de aire incluye al menos un puerto de entrada de aire. El aparato también incluye un montaje de suministro de aire que se encuentra en comunicación de recepción de aire con el montaje de manipulación de aire. El montaje de suministro de aire incluye al menos una tobera que es configurada para dirigir el aire hacia un primer espacio adyacente a un primer lado del freno de tren de aterrizaje para crear un diferencial de presión de aire a través del freno de tren de aterrizaje.
MX2013013684A 2013-02-28 2013-11-22 Sistema de enfriamiento de tren de aterrizaje de aeronave. MX338232B (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US13/779,982 US9573567B2 (en) 2013-02-28 2013-02-28 Aircraft landing gear cooling system

Publications (2)

Publication Number Publication Date
MX2013013684A MX2013013684A (es) 2014-09-01
MX338232B true MX338232B (es) 2016-04-08

Family

ID=50030143

Family Applications (1)

Application Number Title Priority Date Filing Date
MX2013013684A MX338232B (es) 2013-02-28 2013-11-22 Sistema de enfriamiento de tren de aterrizaje de aeronave.

Country Status (6)

Country Link
US (1) US9573567B2 (es)
EP (1) EP2772428B1 (es)
JP (1) JP6527308B2 (es)
BR (1) BR102014004458B1 (es)
CA (1) CA2833892C (es)
MX (1) MX338232B (es)

Families Citing this family (23)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9404806B2 (en) 2013-03-14 2016-08-02 The Boeing Company Methods and apparatus to monitor components of an aircraft landing system
US20140345991A1 (en) * 2013-05-21 2014-11-27 Hamilton Sundstrand Corporation Active aircraft brake cooling system
US9242739B2 (en) * 2013-11-22 2016-01-26 The Boeing Company Methods to monitor components of an aircraft landing system
JP6549849B2 (ja) * 2015-01-26 2019-07-24 三菱航空機株式会社 航空機の主脚ベイの排熱構造
PE20161553Z (es) * 2016-11-09 2017-01-07 Cheesman Kurt Franz Meinel Sistema autonomo de enfriamiento de frenos para aeronaves
US20180134375A1 (en) * 2016-11-15 2018-05-17 The Boeing Company Temperature Actuated Panel
GB2563661B (en) * 2017-06-23 2020-08-05 Ogab Ltd Brake duct system and method
US10935093B2 (en) 2018-03-29 2021-03-02 Honeywell International Inc. Active brake cooling using nitrogen enriched air
US10829210B2 (en) 2018-06-27 2020-11-10 The Boeing Company Braking system for a dual landing gear aircraft
GB2576937A (en) * 2018-09-07 2020-03-11 Airbus Operations Ltd Controlling aircraft wheel brakes
FR3087239B1 (fr) * 2018-10-10 2023-03-31 Safran Electrical & Power Systeme et procede de refroidissement des freins d'un train d'atterrissage d'un aeronef
US11518501B2 (en) * 2019-01-28 2022-12-06 Goodrich Corporation System and method for reducing oxidation of friction disks
US11125294B2 (en) 2019-03-22 2021-09-21 Goodrich Corporation Systems and methods for reducing oxidation of friction disks
JP2021017215A (ja) * 2019-07-24 2021-02-15 三菱航空機株式会社 航空機の主脚ベイの冷却構造および航空機
CN110332260B (zh) * 2019-08-12 2021-09-24 湖北康晨安宝矿业设备有限责任公司 一种前桥行驻一体制动器
US11407397B2 (en) 2019-10-09 2022-08-09 Goodrich Corporation Brake temperature and turnaround time estimation systems and methods
US11441628B2 (en) * 2020-01-29 2022-09-13 The Boeing Company Aircraft brake cooling systems and methods
US11466742B2 (en) * 2020-01-30 2022-10-11 The Boeing Company Active cooling system for landing gear brakes
CA3077918C (en) * 2020-04-08 2021-05-25 Ivan Ralston Inboard brake system
DE102020111517A1 (de) * 2020-04-28 2021-10-28 Dr. Ing. H.C. F. Porsche Aktiengesellschaft Radträgeranordnung einer Vorderachse bzw. Hinterachse eines Kraftfahrzeuges
US11919647B2 (en) * 2020-05-15 2024-03-05 The Boeing Company Thermal control systems for aircraft landing gear wheel wells and related methods
US11884250B2 (en) 2020-10-30 2024-01-30 Honeywell International Inc. Brake cooling assembly
GB2601790A (en) 2020-12-10 2022-06-15 Airbus Operations Ltd Aircraft brake temperature control system

Family Cites Families (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2580001A (en) * 1948-09-23 1951-12-25 Dunlop Rubber Co Air-cooling apparatus for vehicle wheels
GB943472A (en) * 1959-07-02 1963-12-04 Dunlop Rubber Co Cooling means for wheel and brake assembly
US3251437A (en) * 1964-04-13 1966-05-17 Bendix Corp Air cooled disk brake
JPS4829321B1 (es) * 1967-07-31 1973-09-10
FR1582602A (es) * 1968-08-07 1969-10-03
GB1371336A (en) * 1970-11-25 1974-10-23 Dunlop Holdings Ltd Air cooled wheel assembly
JPS6013264Y2 (ja) * 1979-09-19 1985-04-26 株式会社日立製作所 車輪室の側面カバ−
EP0078793A1 (en) 1981-05-13 1983-05-18 MERLE, Julius Wheel brake cooling apparatus for aircraft
DE3321750A1 (de) * 1983-06-16 1984-12-20 Dr.Ing.H.C. F. Porsche Ag, 7000 Stuttgart Kuehleinrichtung fuer scheibenbremsen insb. von kraftfahrzeugen
JP2518745Y2 (ja) * 1992-02-26 1996-11-27 日本プラスト株式会社 自動車のブレーキ冷却装置
JPH0811798A (ja) * 1994-07-01 1996-01-16 Mitsubishi Heavy Ind Ltd 宇宙往還機の脚装置冷却装置
FR2749559B1 (fr) * 1996-06-10 1998-12-18 Patte Jacques Dispositif pour amener les roues d'un avion a la vitesse-sol avant l'atterrissage, puis pour refroidir des disques de freins apres l'atterrissage
US6315091B1 (en) * 1999-12-17 2001-11-13 Daimlerchrysler Corporation Brake cooling system
US6857510B2 (en) * 2002-04-04 2005-02-22 Axletech International Ip Holdings, Llc Forced air cooling system for vehicle driveline components
US7963376B2 (en) * 2007-04-17 2011-06-21 Joseph Gelb System for cooling a disc brake rotor and collecting brake pad waste
FR2941438B1 (fr) * 2009-01-26 2011-03-04 Technofan Ensemble de roue ventile.
RU2601794C2 (ru) * 2012-02-23 2016-11-10 Л-3 Коммьюникейшнз Магнет-Мотор Гмбх Блок привода для шасси летательного аппарата с интегрированным охлаждением

Also Published As

Publication number Publication date
EP2772428A1 (en) 2014-09-03
MX2013013684A (es) 2014-09-01
CA2833892C (en) 2016-06-21
BR102014004458B1 (pt) 2021-12-14
BR102014004458A2 (pt) 2015-10-20
JP2014169070A (ja) 2014-09-18
EP2772428B1 (en) 2018-05-02
JP6527308B2 (ja) 2019-06-05
CA2833892A1 (en) 2014-08-28
US9573567B2 (en) 2017-02-21
US20140239121A1 (en) 2014-08-28

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