BR0313311A - Sistema de controle para movimentar um reversor de empuxo - Google Patents

Sistema de controle para movimentar um reversor de empuxo

Info

Publication number
BR0313311A
BR0313311A BR0313311-7A BR0313311A BR0313311A BR 0313311 A BR0313311 A BR 0313311A BR 0313311 A BR0313311 A BR 0313311A BR 0313311 A BR0313311 A BR 0313311A
Authority
BR
Brazil
Prior art keywords
plates
thrust reverser
torque
moving
torsion spring
Prior art date
Application number
BR0313311-7A
Other languages
English (en)
Inventor
Donald J Christensen
Original Assignee
Honeywell Int Inc
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 Honeywell Int Inc filed Critical Honeywell Int Inc
Publication of BR0313311A publication Critical patent/BR0313311A/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
    • F16D55/02—Brakes with substantially-radial braking surfaces pressed together in axial direction, e.g. disc brakes with axially-movable discs or pads pressed against axially-located rotating members
    • F16D55/04—Brakes with substantially-radial braking surfaces pressed together in axial direction, e.g. disc brakes with axially-movable discs or pads pressed against axially-located rotating members by moving discs or pads away from one another against radial walls of drums or cylinders
    • 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
    • B64D33/00—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/04—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of exhaust outlets or jet pipes
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/54—Nozzles having means for reversing jet thrust
    • F02K1/64—Reversing fan flow
    • F02K1/70—Reversing fan flow using thrust reverser flaps or doors mounted on the fan housing
    • F02K1/72—Reversing fan flow using thrust reverser flaps or doors mounted on the fan housing the aft end of the fan housing being movable to uncover openings in the fan housing for the reversed flow
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/54—Nozzles having means for reversing jet thrust
    • F02K1/76—Control or regulation of thrust reversers
    • F02K1/763—Control or regulation of thrust reversers with actuating systems or actuating devices; Arrangement of actuators for thrust reversers
    • 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
    • F16D55/38—Brakes with a plurality of rotating discs all lying side by side mechanically actuated
    • 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
    • F16D59/00—Self-acting brakes, e.g. coming into operation at a predetermined speed
    • 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
    • F16D2121/14—Mechanical
    • 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
    • F16D2125/20—Mechanical mechanisms converting rotation to linear movement or vice versa
    • F16D2125/34—Mechanical mechanisms converting rotation to linear movement or vice versa acting in the direction of the axis of rotation
    • F16D2125/36—Helical cams, Ball-rotating ramps
    • F16D2125/38—Helical cams, Ball-rotating ramps with plural cam or ball-ramp mechanisms arranged concentrically with the brake rotor axis
    • 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
    • F16D2127/00—Auxiliary mechanisms
    • F16D2127/001—Auxiliary mechanisms for automatic or self-acting brake operation
    • F16D2127/005—Auxiliary mechanisms for automatic or self-acting brake operation force- or torque-responsive

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Braking Arrangements (AREA)

Abstract

"SISTEMA DE CONTROLE PARA MOVIMENTAR UM REVERSOR DE EMPUXO". Sistema reversor de empuxo que inclui uma montagem de freio ativado por torque passante (410) que limita o torque aplicado em partes do conjunto de componentes de acionamento do reversor de empuxo de uma aeronave. A montagem de freio (410) inclui duas chapas (602,604) que são acopladas juntas com uma mola de torção (608). Quando um torque predeterminado é aplicado à mola de torção (608), a mola de torção (608) desloca as chapas (602,604) uma da outra. As esferas (606) que estão posicionadas nos sulcos em came (618,628) em cada uma das chapas (602,604) induzem as chapas a transitarem em afastamento uma da outra e a contatarem as superfícies de freio (816,818) para de esse modo limitar o torque no conjunto de componentes de acionamento.
BR0313311-7A 2002-08-05 2003-08-05 Sistema de controle para movimentar um reversor de empuxo BR0313311A (pt)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US10/212,384 US6666307B1 (en) 2002-08-05 2002-08-05 Thrust reverser system with a pass-through torque activated brake
PCT/US2003/025277 WO2004013481A1 (en) 2002-08-05 2003-08-05 Thrust reverser system with a pass-through torque activated brake

Publications (1)

Publication Number Publication Date
BR0313311A true BR0313311A (pt) 2005-06-21

Family

ID=29735439

Family Applications (1)

Application Number Title Priority Date Filing Date
BR0313311-7A BR0313311A (pt) 2002-08-05 2003-08-05 Sistema de controle para movimentar um reversor de empuxo

Country Status (7)

Country Link
US (2) US6666307B1 (pt)
EP (1) EP1527268A1 (pt)
JP (1) JP2005534857A (pt)
AU (1) AU2003259798A1 (pt)
BR (1) BR0313311A (pt)
CA (1) CA2494866A1 (pt)
WO (1) WO2004013481A1 (pt)

Families Citing this family (31)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2846377B1 (fr) * 2002-10-25 2006-06-30 Hispano Suiza Sa Inverseur de poussee electromecanique pour turboreacteur a controle permanent de position
DE10308758A1 (de) * 2003-02-28 2004-09-16 Dr.Ing.H.C. F. Porsche Ag Verfahren zur Steuerung von Front- und/oder Heckspoilern
US6786315B1 (en) * 2003-03-28 2004-09-07 Honeywell International, Inc. Thrust reverser system with sequential torque decoupler
DE102004023123A1 (de) * 2003-05-30 2004-12-16 Ringspann Gmbh Absturzsicherung
US7264203B2 (en) * 2003-10-02 2007-09-04 The Nordam Group, Inc. Spider actuated thrust reverser
US7093424B2 (en) * 2004-08-24 2006-08-22 Honeywell International, Inc. Thrust reverser system electro-mechanical brake manual release mechanism
US7513101B2 (en) 2005-10-28 2009-04-07 Honeywell International Inc. Synchronized motor thrust reverser actuation system
US7491127B2 (en) * 2006-04-27 2009-02-17 Honeywell International Inc. Spline with lubricant retention feature for use in torque limiter
US7946105B2 (en) * 2006-11-02 2011-05-24 Honeywell International Inc. Bi-directional locking ring assembly for aircraft thrust reverser manual drive unit
GB0705301D0 (en) * 2007-03-20 2007-04-25 Goodrich Actuation Systems Ltd Actuator arrangement
FR2920196B1 (fr) * 2007-08-20 2013-08-09 Aircelle Sa Inverseur de poussee avec systeme de freinage des actionneurs
FR2947870B1 (fr) * 2009-07-09 2011-07-08 Aircelle Sa Systeme d'actionnement pour element mobile de nacelle de moteur d'aeronef, tel qu'un capot d'inverseur de poussee
GB0917057D0 (en) * 2009-09-29 2009-11-11 Goodrich Actuation Systems Ltd Thrust reverser actuation
FR2954278B1 (fr) 2009-12-18 2012-01-20 Aircelle 7303 Structure support pour inverseur de poussee notamment a grilles
US8511441B2 (en) * 2010-04-01 2013-08-20 Hamilton Sundstrand Corporation Cone brake no-back
US9651126B2 (en) 2010-09-30 2017-05-16 Hamilton Sundstrand Corporation Cone brake load limiter method and apparatus
NL2006492C2 (nl) * 2011-03-30 2012-10-02 Ee Voertuig met een reminrichting.
US9038367B2 (en) 2011-09-16 2015-05-26 United Technologies Corporation Fan case thrust reverser
CN103122958B (zh) * 2011-11-21 2016-05-04 哈米尔顿森德斯特兰德公司 锥形制动器载荷限制器方法和设备
DE102012020820B4 (de) * 2012-10-23 2022-03-17 Liebherr-Aerospace Lindenberg Gmbh Differenzgeschwindigkeitsabhängige Bremse
US9616990B2 (en) 2014-07-18 2017-04-11 Hamilton Sundstrand Corporation Aircraft component rotary device
DE102014011336A1 (de) * 2014-07-30 2016-02-04 Liebherr-Aerospace Lindenberg Gmbh Rücklaufsperre mit radial wirkenden Bremselementen
US9527580B2 (en) 2014-09-24 2016-12-27 Hamilton Sundstrand Corporation Cone brake no-back assembly with gain reduction spring and method
FR3028295B1 (fr) * 2014-11-06 2020-01-17 Safran Electronics & Defense Systeme d'actionnement d'une structure mobile d'un inverseur de poussee d'un aeronef, inverseur de poussee et reacteur comprenant un tel systeme.
EP3193003A1 (en) * 2016-01-15 2017-07-19 Goodrich Actuation Systems Ltd. Thrust reverser actuation system architecture
CN108223624B (zh) * 2016-12-22 2020-08-07 比亚迪股份有限公司 电动式制动器以及具有它的车辆
EP3450785B1 (en) 2017-08-30 2020-05-20 Microtecnica S.r.l. No-back/torque limiter device with torque sensing elements
US10612491B2 (en) * 2017-09-25 2020-04-07 Rohr, Inc. Mounting device with pin actuator
DE102019113946A1 (de) * 2019-05-24 2020-11-26 Liebherr-Aerospace Lindenberg Gmbh Lastbegrenzungsvorrichtung mit lasthaltender Kupplung
WO2021207009A1 (en) * 2020-04-05 2021-10-14 Duplicent, Llc Expanding rotor brake
US11906006B2 (en) 2021-10-08 2024-02-20 Honeywell International Inc. Self-activated no-back device

Family Cites Families (47)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US22852A (en) * 1859-02-08 Improvement in photography on wood
US2015688A (en) 1933-10-19 1935-10-01 Steel Wheel Corp Drive mechanism
US2441052A (en) * 1946-01-21 1948-05-04 Elmer E Wilmer Coupling that compensates for axial displacement of shafts connected thereby
US2660281A (en) 1949-02-25 1953-11-24 Bendix Aviat Corp Slip clutch for screw actuators
US2819589A (en) 1954-04-01 1958-01-14 Gen Motors Corp Fluid pressure actuator and synchronizing means therefor
US2783861A (en) * 1954-11-29 1957-03-05 Cleveland Pneumatic Tool Co Drive-released brake
US3367456A (en) * 1965-12-30 1968-02-06 Gen Motors Corp Torque sensitive brake
US3536169A (en) * 1969-01-10 1970-10-27 Carter H Arnold Load brake for unidirectional or bidirectional use
US3596740A (en) 1970-01-27 1971-08-03 Trw Inc Torque limiter
US3653226A (en) 1970-06-11 1972-04-04 Hobson Ltd H M Bi-directional torque limiters
US3640092A (en) * 1970-07-10 1972-02-08 Hobson Ltd H M Torque limiter
FR2181177A5 (pt) 1972-04-20 1973-11-30 Dba
CH537539A (de) * 1972-07-26 1973-05-31 Inventio Ag Lastabhängige Bremsvorrichtung für Fördereinrichtungen
GB1451327A (en) * 1973-02-23 1976-09-29 Girling Ltd Brake actuator mechanisms provided with automatic slack adjusters
US4030578A (en) 1976-05-03 1977-06-21 The Boeing Company Torque limiter
US4117909A (en) * 1976-06-21 1978-10-03 Massachusetts Institute Of Technology Wheel torque feedback controlled front brake
JPS5849742B2 (ja) * 1979-02-14 1983-11-07 日本発条株式会社 摩擦制振装置
US4531617A (en) * 1980-04-10 1985-07-30 D. Wickham And Company Limited Overspeed safety braking device
US4442928A (en) 1981-10-02 1984-04-17 The Bendix Corporation Actuator
US4459121A (en) 1982-03-12 1984-07-10 The Garrett Corporation Torque limiting clutch
DE3222674C2 (de) 1982-06-16 1984-04-05 MTU Motoren- und Turbinen-Union München GmbH, 8000 München Einrichtung zum Verstellen von Schubumkehrern
US4489801A (en) * 1982-09-09 1984-12-25 Yamaha Motor Corporation, U.S.A. Braking assembly for a snowmobile
US4458582A (en) 1982-10-18 1984-07-10 Sundstrand Corporation Automatic rigging arrangement for actuation systems
US4579039A (en) 1983-12-12 1986-04-01 Sundstrand Corporation Power drive unit
US4545470A (en) 1983-12-14 1985-10-08 Sundstrand Corporation Narrow tolerance range slip clutch
JPS60252084A (ja) * 1984-05-26 1985-12-12 本田技研工業株式会社 車輪角減速度センサの支持・駆動装置
US4693349A (en) 1986-07-25 1987-09-15 Sundstrand Corporation Torque limiting apparatus
JPS63110060A (ja) * 1986-10-24 1988-05-14 Honda Motor Co Ltd 車両用アンチロツク制御装置の車輪角加速度センサ
US4860865A (en) * 1987-09-10 1989-08-29 The Montalvo Corporation Quick release, high torque, friction brakes and clutches
US4898265A (en) * 1988-01-27 1990-02-06 Sundstrand Corporation Torque limiter
US4850458A (en) * 1988-11-16 1989-07-25 Boeing Company Bidirectional rotary brake
US5090529A (en) * 1990-05-16 1992-02-25 Ivg Australia Pty. Limited Brake mechanism
GB9106515D0 (en) 1991-03-27 1991-05-22 Lucas Ind Plc Device for operation of a gas turbine engine thrust reverser system
US5545109A (en) * 1991-05-11 1996-08-13 Hayakawa; Toshio Torque limiter
US5299676A (en) * 1991-08-15 1994-04-05 Ivg Australia Pty. Limited Rotation check mechanism
EP0536954B1 (en) 1991-10-10 1996-01-24 Lucas Industries Public Limited Company A lock for a thrust reverser mechanism, a thrust reverser mechanism, and a thrust reverser
US5609020A (en) 1995-05-15 1997-03-11 The Boeing Company Thrust reverser synchronization shaft lock
US5769362A (en) 1996-05-01 1998-06-23 Safe Flight Instrument Corporation Aircraft control mechanism for a speed brake
FR2760047B1 (fr) * 1997-02-27 1999-05-07 Hispano Suiza Sa Inverseur de poussee de turboreacteur a portes associees a un dispositif de synchronisation de commande
FI103032B1 (fi) 1997-10-08 1999-04-15 Kci Kone Cranes Int Oy Kuormajarru
US5944148A (en) 1998-08-31 1999-08-31 The Boeing Company No-back brake
WO2001027486A1 (fr) * 1999-10-14 2001-04-19 Koyo Seiko Co., Ltd. Dispositif d'embrayage
US6715589B2 (en) * 2001-02-09 2004-04-06 Meritor Heavy Vehicle Systems, Llc Self-servoing disc brake rotor
GB0122321D0 (en) * 2001-09-15 2001-11-07 Lucas Industries Ltd Helicopter rotor blade locking pin braking asembly
US6598386B2 (en) * 2001-10-16 2003-07-29 Honeywell International, Inc. Jet engine thrust reverser system having torque limited synchronization
JP3828782B2 (ja) * 2001-11-08 2006-10-04 本田技研工業株式会社 トルクカム機構
JP3703444B2 (ja) * 2002-06-06 2005-10-05 川崎重工業株式会社 車輌用摩擦クラッチ

Also Published As

Publication number Publication date
CA2494866A1 (en) 2004-02-12
AU2003259798A1 (en) 2004-02-23
US6814191B2 (en) 2004-11-09
EP1527268A1 (en) 2005-05-04
US6666307B1 (en) 2003-12-23
JP2005534857A (ja) 2005-11-17
US20040035653A1 (en) 2004-02-26
WO2004013481A1 (en) 2004-02-12

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Legal Events

Date Code Title Description
B08F Application dismissed because of non-payment of annual fees [chapter 8.6 patent gazette]

Free format text: REFERENTE AS 7A E 8A ANUIDADES.

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 2157 DE 08/05/2012.