FR2992942B1 - METHOD OF USING AND MAINTAINING A LANDING BRAKE COMPRISING A BRAKE ACTUATOR DISC STACK, AIRCRAFT BRAKE AND WHEEL BRAKE ASSEMBLY COMPRISING SUCH ACTUATOR - Google Patents

METHOD OF USING AND MAINTAINING A LANDING BRAKE COMPRISING A BRAKE ACTUATOR DISC STACK, AIRCRAFT BRAKE AND WHEEL BRAKE ASSEMBLY COMPRISING SUCH ACTUATOR

Info

Publication number
FR2992942B1
FR2992942B1 FR1256592A FR1256592A FR2992942B1 FR 2992942 B1 FR2992942 B1 FR 2992942B1 FR 1256592 A FR1256592 A FR 1256592A FR 1256592 A FR1256592 A FR 1256592A FR 2992942 B1 FR2992942 B1 FR 2992942B1
Authority
FR
France
Prior art keywords
brake
actuator
maintaining
landing
aircraft
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
Application number
FR1256592A
Other languages
French (fr)
Other versions
FR2992942A1 (en
Inventor
Emmanuel Colin
Dominique Onfroy
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Safran Landing Systems SAS
Original Assignee
Messier Bugatti Dowty SA
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 Dowty SA filed Critical Messier Bugatti Dowty SA
Priority to FR1256592A priority Critical patent/FR2992942B1/en
Publication of FR2992942A1 publication Critical patent/FR2992942A1/en
Application granted granted Critical
Publication of FR2992942B1 publication Critical patent/FR2992942B1/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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
    • F16D65/00—Parts or details
    • F16D65/0043—Brake maintenance and assembly, tools therefor
    • 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
    • B64C25/44—Actuating mechanisms
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
    • B64F5/00—Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
    • B64F5/60—Testing or inspecting aircraft components or systems
    • 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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D45/00—Aircraft indicators or protectors not otherwise provided for
    • B64D2045/0085—Devices for aircraft health monitoring, e.g. monitoring flutter or vibration
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D45/00—Aircraft indicators or protectors not otherwise provided for
    • 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
    • F16D2125/00—Components of actuators
    • F16D2125/18—Mechanical mechanisms
    • F16D2125/58—Mechanical mechanisms transmitting linear movement
FR1256592A 2012-07-09 2012-07-09 METHOD OF USING AND MAINTAINING A LANDING BRAKE COMPRISING A BRAKE ACTUATOR DISC STACK, AIRCRAFT BRAKE AND WHEEL BRAKE ASSEMBLY COMPRISING SUCH ACTUATOR Active FR2992942B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR1256592A FR2992942B1 (en) 2012-07-09 2012-07-09 METHOD OF USING AND MAINTAINING A LANDING BRAKE COMPRISING A BRAKE ACTUATOR DISC STACK, AIRCRAFT BRAKE AND WHEEL BRAKE ASSEMBLY COMPRISING SUCH ACTUATOR

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1256592A FR2992942B1 (en) 2012-07-09 2012-07-09 METHOD OF USING AND MAINTAINING A LANDING BRAKE COMPRISING A BRAKE ACTUATOR DISC STACK, AIRCRAFT BRAKE AND WHEEL BRAKE ASSEMBLY COMPRISING SUCH ACTUATOR

Publications (2)

Publication Number Publication Date
FR2992942A1 FR2992942A1 (en) 2014-01-10
FR2992942B1 true FR2992942B1 (en) 2015-03-06

Family

ID=46963885

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1256592A Active FR2992942B1 (en) 2012-07-09 2012-07-09 METHOD OF USING AND MAINTAINING A LANDING BRAKE COMPRISING A BRAKE ACTUATOR DISC STACK, AIRCRAFT BRAKE AND WHEEL BRAKE ASSEMBLY COMPRISING SUCH ACTUATOR

Country Status (1)

Country Link
FR (1) FR2992942B1 (en)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20160304191A1 (en) * 2015-04-16 2016-10-20 Goodrich Corporation Increased brake radius to improve rto performance
GB2559329A (en) * 2017-01-26 2018-08-08 Airbus Operations Ltd Fault detection based on brake torque and temperature
FR3070370B1 (en) * 2017-08-28 2019-09-06 Safran Landing Systems AIR TERMINAL AIR TERMINAL WITH REPORTED AXLE, AND ASSOCIATED ASSEMBLY METHODS

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6003640A (en) * 1997-05-09 1999-12-21 The B.F. Goodrich Company Electronic braking system with brake wear measurement and running clearance adjustment
US7104366B2 (en) * 2002-12-11 2006-09-12 Honeywell International Method of increasing friction material utilization for carbon brakes
US9815438B2 (en) * 2010-02-12 2017-11-14 Honeywell International Inc. Aircraft electric brake actuator assembly with line replaceable actuator brake

Also Published As

Publication number Publication date
FR2992942A1 (en) 2014-01-10

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