BR0100649B1 - junta esférica com translação e montagem para suportar um motor em um avião. - Google Patents

junta esférica com translação e montagem para suportar um motor em um avião.

Info

Publication number
BR0100649B1
BR0100649B1 BRPI0100649-5A BR0100649A BR0100649B1 BR 0100649 B1 BR0100649 B1 BR 0100649B1 BR 0100649 A BR0100649 A BR 0100649A BR 0100649 B1 BR0100649 B1 BR 0100649B1
Authority
BR
Brazil
Prior art keywords
airplane
translation
engine
mounting
support
Prior art date
Application number
BRPI0100649-5A
Other languages
English (en)
Portuguese (pt)
Other versions
BR0100649A (pt
Inventor
John Alan Manteiga
Christopher James Wilusz
Cornelius H Dykhuizen
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 filed Critical
Publication of BR0100649A publication Critical patent/BR0100649A/pt
Publication of BR0100649B1 publication Critical patent/BR0100649B1/pt

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C11/00Pivots; Pivotal connections
    • F16C11/04Pivotal connections
    • F16C11/06Ball-joints; Other joints having more than one degree of angular freedom, i.e. universal joints
    • F16C11/0614Ball-joints; Other joints having more than one degree of angular freedom, i.e. universal joints the female part of the joint being open on two sides
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/40Arrangements for mounting power plants in aircraft
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/40Arrangements for mounting power plants in aircraft
    • B64D27/404Suspension arrangements specially adapted for supporting vertical loads
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C2326/00Articles relating to transporting
    • F16C2326/43Aeroplanes; Helicopters

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Pivots And Pivotal Connections (AREA)
  • Transmission Devices (AREA)
BRPI0100649-5A 2000-02-29 2001-02-20 junta esférica com translação e montagem para suportar um motor em um avião. BR0100649B1 (pt)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US09/515,171 US6330995B1 (en) 2000-02-29 2000-02-29 Aircraft engine mount

Publications (2)

Publication Number Publication Date
BR0100649A BR0100649A (pt) 2001-10-09
BR0100649B1 true BR0100649B1 (pt) 2009-05-05

Family

ID=24050240

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI0100649-5A BR0100649B1 (pt) 2000-02-29 2001-02-20 junta esférica com translação e montagem para suportar um motor em um avião.

Country Status (5)

Country Link
US (1) US6330995B1 (https=)
EP (1) EP1129942B1 (https=)
JP (1) JP4591903B2 (https=)
BR (1) BR0100649B1 (https=)
DE (1) DE60104342T2 (https=)

Families Citing this family (104)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2799432A1 (fr) * 1999-10-07 2001-04-13 Snecma Suspension a securite integree pour groupes motopropulseurs d'aeronefs
GB2359052B (en) * 2000-02-09 2003-09-17 Rolls Royce Plc Engine arrangement
FR2828167B1 (fr) * 2001-07-31 2003-11-21 Airbus France Dispositif d'accrochage d'un moteur sur un aeronef
US6607165B1 (en) * 2002-06-28 2003-08-19 General Electric Company Aircraft engine mount with single thrust link
US6808333B2 (en) * 2002-10-30 2004-10-26 Cnh Canada, Ltd Pivot pin assembly
US6984104B2 (en) * 2002-12-16 2006-01-10 United Technologies Corporation Variable vane arm/unison ring attachment system
FR2855495B1 (fr) * 2003-05-27 2006-11-24 Snecma Moteurs Dispositif d'accrochage avant de moteur d'avion
FR2855494B1 (fr) * 2003-05-27 2006-09-22 Snecma Moteurs Dispositif d'accrocharge arriere de moteur d'avion
FR2862612B1 (fr) * 2003-11-25 2006-02-17 Airbus France Dispositif d'accrochage d'un moteur sous une voilure d'aeronef
US7260892B2 (en) * 2003-12-24 2007-08-28 General Electric Company Methods for optimizing turbine engine shell radial clearances
FR2865512B1 (fr) * 2004-01-23 2007-05-11 Airbus France Dispositif de jonction articulee
US6843449B1 (en) * 2004-02-09 2005-01-18 General Electric Company Fail-safe aircraft engine mounting system
US7163068B2 (en) * 2004-03-04 2007-01-16 Wayne Job Hitch assembly
FR2867155B1 (fr) * 2004-03-08 2007-06-29 Snecma Moteurs Suspension d'un moteur a la structure d'un avion
FR2868041B1 (fr) * 2004-03-25 2006-05-26 Snecma Moteurs Sa Suspension d'un moteur d'avion
FR2869874B1 (fr) * 2004-05-04 2006-06-23 Snecma Moteurs Sa Moteur d'avion avec des moyens de suspension a la structure d'un avion
FR2873986B1 (fr) * 2004-08-04 2007-12-21 Airbus France Sas Ensemble moteur pour aeronef
SE528948C2 (sv) * 2004-12-23 2007-03-20 Volvo Aero Corp Ringformad vridstyv statisk komponent för en flygplansmotor
FR2883839B1 (fr) * 2005-03-29 2007-06-29 Snecma Moteurs Sa Suspension arriere de turboreacteur
FR2887853B1 (fr) * 2005-06-29 2007-08-17 Airbus France Sas Attache moteur pour aeronef destinee a etre interposee entre un moteur et un mat d'accrochage
FR2891245B1 (fr) * 2005-09-26 2007-10-26 Airbus France Sas Procede de montage d'un moteur d'aeronef sur une structure rigide d'un mat d'accrochage du moteur
FR2891243B1 (fr) * 2005-09-26 2009-04-03 Airbus France Sas Mat d'accrochage de moteur pour aeronef
FR2891253B1 (fr) * 2005-09-28 2007-10-26 Airbus France Sas Attache arriere d'un moteur d'aeronef a deux manilles
FR2891250B1 (fr) * 2005-09-28 2007-10-26 Airbus France Sas Ensemble moteur pour aeronef comprenant un moteur ainsi qu'un mat d'accrochage d'un tel moteur
ES2336395B1 (es) * 2005-10-28 2011-02-14 Airbus Operations, S.L. Sistema de soporte de motor auxiliar.
FR2892706B1 (fr) * 2005-10-31 2009-04-24 Airbus France Sas Dispositif d'attache avant d'un turboreacteur a un mat de fixation d'un aeronef
FR2894934B1 (fr) * 2005-12-15 2009-11-13 Airbus France Attache arriere d'un moteur d'aeronef avec manille en attente et ressort pour un tel axe en attente
FR2917711B1 (fr) * 2007-06-25 2010-01-15 Snecma Suspension d'un turbomoteur a la structure d'un aeronef
FR2923459B1 (fr) * 2007-11-09 2010-05-21 Snecma Moyen de blocage en rotation d'un axe supportant un organe de suspension de turbomoteur
FR2923460B1 (fr) * 2007-11-12 2010-05-14 Snecma Montage d'un organe de suspension d'un turbomoteur
FR2924684B1 (fr) * 2007-12-07 2010-01-01 Snecma Suspension d'un turboreacteur a un aeronef
US8826641B2 (en) * 2008-01-28 2014-09-09 United Technologies Corporation Thermal management system integrated pylon
US9234481B2 (en) * 2008-01-25 2016-01-12 United Technologies Corporation Shared flow thermal management system
GB2459483B (en) 2008-04-24 2010-06-30 Rolls Royce Plc Engine mounting arrangement
US20140174056A1 (en) * 2008-06-02 2014-06-26 United Technologies Corporation Gas turbine engine with low stage count low pressure turbine
GB0810585D0 (en) 2008-06-11 2008-07-16 Rolls Royce Plc Engine mounting arrangement
GB0810589D0 (en) * 2008-06-11 2008-07-16 Rolls Royce Plc Engine mounting arrangement
FR2933070B1 (fr) * 2008-06-25 2010-08-20 Snecma Systeme propulsif d'aeronef
WO2010024736A1 (en) * 2008-08-29 2010-03-04 Volvo Aero Corporation A component and a gas turbine engine comprising the component
FR2952150B1 (fr) * 2009-11-02 2012-02-24 Airbus Operations Sas Bielle structurale comportant un mode filtrant des vibrations
US10137542B2 (en) 2010-01-14 2018-11-27 Senvion Gmbh Wind turbine rotor blade components and machine for making same
CN102762850B (zh) 2010-01-14 2015-04-08 耐普迪考股份有限公司 风力涡轮机转子叶片部件及其制造方法
KR101828921B1 (ko) * 2010-06-14 2018-02-13 로오드 코포레이션 헬리콥터 엔진 장착 시스템 및 방법
US8668444B2 (en) * 2010-09-28 2014-03-11 General Electric Company Attachment stud for a variable vane assembly of a turbine compressor
US8714916B2 (en) * 2010-09-28 2014-05-06 General Electric Company Variable vane assembly for a turbine compressor
FR2965549B1 (fr) * 2010-10-01 2013-07-05 Airbus Operations Sas Dispositif de reprise de poussee a bielles pour mat d'accrochage d'un moteur d'aeronef, integrant trois rotules alignees
FR2966125B1 (fr) * 2010-10-15 2013-04-26 Aircelle Sa Ensemble d'accrochage d'une suspension d'un ensemble propulsif d'aeronef
FR2975132B1 (fr) * 2011-05-09 2015-06-26 Snecma Bielles de suspension du canal de flux froid d'un turboreacteur a rotules excentriques
US20130074517A1 (en) * 2011-09-23 2013-03-28 United Technologies Corporation Gas turbine engine mount assembly
GB201118548D0 (en) * 2011-10-27 2011-12-07 Airbus Operations Ltd Plain journal bearing
US9410596B2 (en) 2011-11-04 2016-08-09 Honeywell International Inc. Mounting systems for structural members, fastening assemblies thereof, and vibration isolation systems including the same
FR2982331B1 (fr) * 2011-11-07 2013-11-29 Eurocopter France Mecanisme d'articulation en rotule entre une chape et une bielle, notamment pour un appareillage de commande equipant un giravion
US8672262B2 (en) * 2012-01-10 2014-03-18 Textron Innovations Inc. Mechanically optimized liquid inertia vibration eliminator and aircraft pylon system
US8678323B2 (en) 2012-02-28 2014-03-25 Honeywell International Inc. Launch lock assemblies including axial gap amplification devices and spacecraft isolation systems including the same
US20130232768A1 (en) 2012-03-12 2013-09-12 United Technologies Corporation Turbine engine case mount and dismount
US9217337B2 (en) 2012-05-10 2015-12-22 United Technologies Corporation Adjustable engine mount
US9194296B2 (en) 2012-05-18 2015-11-24 Pratt & Whitney Canada Corp. Inner bypass duct wall attachment
US9227734B2 (en) * 2012-08-31 2016-01-05 United Technologies Corporation Secondary load path for gas turbine engine
US8985509B2 (en) 2012-08-31 2015-03-24 United Technologies Corporation Assembly for mounting a turbine engine to a pylon
US9475594B2 (en) 2012-09-25 2016-10-25 Honeywell International Inc. Launch lock assemblies with reduced preload and spacecraft isolation systems including the same
FR3000467A1 (fr) * 2012-12-28 2014-07-04 Airbus Operations Sas Manille a trois points a capacite de filtrage de vibrations et attache moteur d'aeronef equipee d'une telle manille
US9365278B2 (en) * 2013-01-21 2016-06-14 The Boeing Company Variation compensating assembly
FR3001714B1 (fr) * 2013-02-05 2016-08-26 Astrium Sas Dispositif de support et de maintien de reservoirs cryogeniques
CN103112595B (zh) * 2013-02-06 2016-01-27 中国商用飞机有限责任公司 推进系统一体化的吊挂结构
CN103101628B (zh) * 2013-02-06 2015-05-27 中国商用飞机有限责任公司 一种与飞机吊挂一体化的前安装节
WO2014189588A2 (en) * 2013-03-15 2014-11-27 United Technologies Corporation Engine mount waiting fail safe lug joint with reduced dynamic amplification factor
GB201306674D0 (en) * 2013-04-12 2013-05-29 Rolls Royce Plc Rigid Raft for a Gas Turbine Engine
US10144524B2 (en) 2013-06-14 2018-12-04 Rohr, Inc. Assembly for mounting a turbine engine to a pylon
CN105392700B (zh) 2013-07-26 2018-12-18 Mra系统有限责任公司 飞行器发动机吊架
GB201315968D0 (en) * 2013-09-09 2013-10-23 Rolls Royce Plc Aircraft engine mount
FR3014972B1 (fr) * 2013-12-12 2016-04-22 Airbus Operations Sas Assemblage comprenant un axe d'articulation supporte par une chape et immobilise en translation par un dispositif de blocage integrant un double systeme d'anti-rotation
US11072412B2 (en) * 2014-05-28 2021-07-27 The Boeing Company Mounting member with anti-rotation bushings
US9783312B2 (en) 2014-07-10 2017-10-10 Honeywell International Inc. Method and apparatus for reducing high transient mount load in aircraft engine mounting systems
CN110182373B (zh) * 2015-01-07 2023-01-10 洛德公司 用于飞行器发动机安装架的轴承组件
US10092106B2 (en) 2015-07-14 2018-10-09 La-Z-Boy Incorporated Recliner and legrest mechanism for a furniture member
FR3041996B1 (fr) * 2015-10-05 2017-10-27 Snecma Systeme de suspension de deux modules d'un ensemble propulsif
US9828117B2 (en) * 2016-02-04 2017-11-28 United Launch Alliance, L.L.C. Tensioning apparatus and system for clamping joints
US10100779B2 (en) * 2016-04-09 2018-10-16 United Technologies Corporation Enhanced durability drive link for high load misalignment
US9986832B2 (en) * 2016-06-06 2018-06-05 La-Z-Boy Incorporated Furniture member with wall-proximity mechanism
US9986835B2 (en) 2016-09-22 2018-06-05 La-Z-Boy Incorporated Furniture member having cam tilt mechanism
FR3059364B1 (fr) * 2016-11-30 2018-11-23 Safran Aircraft Engines Systeme de suspension d'un premier element annulaire dans un deuxieme element annulaire de turbomachine et turbomachine correspondante
FR3059645B1 (fr) * 2016-12-02 2018-12-07 Safran Aircraft Engines Dispositif de suspension pour turbomachine
US10544793B2 (en) 2017-01-25 2020-01-28 General Electric Company Thermal isolation structure for rotating turbine frame
US10568428B2 (en) 2017-04-07 2020-02-25 La-Z-Boy Incorporated Furniture member having flexible seatback
US10537178B2 (en) 2017-04-07 2020-01-21 La-Z-Boy Incorporated Furniture member having flexible seatback
FR3075175B1 (fr) * 2017-12-20 2019-12-13 Safran Aircraft Engines Dispositif de suspension
US10524575B2 (en) 2018-04-16 2020-01-07 La-Z-Boy Incorporated Furniture member with foldable pawl and ratchet assembly
US10820708B2 (en) 2018-05-18 2020-11-03 La-Z-Boy Incorporated Furniture member with wall-proximity mechanism and locking trigger
US10524574B2 (en) 2018-05-18 2020-01-07 La-Z-Boy Incorporated Furniture member with powered wall-proximity mechanism
GB2577540A (en) * 2018-09-28 2020-04-01 Airbus Operations Ltd Joint for connecting aircraft structures
FR3091520A1 (fr) * 2019-01-09 2020-07-10 Airbus Operations (S.A.S.) Attache-moteur d’aéronef comprenant au moins un système d’immobilisation en translation d’un pion de cisaillement comportant une plaque d’obturation, procédé de montage de ladite attache-moteur et aéronef comprenant ladite attache-moteur
FR3093142A1 (fr) * 2019-02-22 2020-08-28 Airbus Operations Ensemble de pièces assemblées par un arbre traversant pouvant être monté en cas d’alignement approximatif entre les pièces
US11820510B2 (en) * 2019-03-26 2023-11-21 Yaborã Industria Aeronautica S.A. Quickly adjustable fail-safe link bar assemblies especially useful for connecting structural components of an aircraft
WO2020227658A1 (en) 2019-05-09 2020-11-12 La-Z-Boy Incorporated Reclining chaise
FR3096028B1 (fr) * 2019-05-14 2021-05-21 Airbus Operations Sas Attache moteur arriere pour un moteur d’aeronef
US11273923B2 (en) * 2019-07-12 2022-03-15 Spirit Aerosystems, Inc. Fail-safe engine support system
WO2021101818A1 (en) * 2019-11-19 2021-05-27 Moog Inc. Motion simulator fault tolerant load carrying pivot connection
WO2021126186A1 (en) * 2019-12-18 2021-06-24 Lord Corporation Ultra-high temperature elastomeric alignment & isolation devices
US11197549B1 (en) 2020-09-28 2021-12-14 La-Z-Boy Incorporated Wall-proximity furniture member having sync mechanism
US11428160B2 (en) 2020-12-31 2022-08-30 General Electric Company Gas turbine engine with interdigitated turbine and gear assembly
US12478185B2 (en) 2022-03-18 2025-11-25 La-Z-Boy Incorporated Reclining chaise mechanism
US12588765B2 (en) 2023-05-04 2026-03-31 La-Z-Boy Incorporated Rocking furniture member with power synchronous mechanism
FR3150505A1 (fr) * 2023-06-28 2025-01-03 Airbus Operations Système d’attache moteur avant pour un moteur d’aéronef qui comporte une structure compacte
FR3160675B1 (fr) * 2024-03-28 2026-04-03 Airbus Operations Sas Système d’attache moteur d’aéronef comprenant une manille à deux points équipée d’au moins une butée, aéronef comportant au moins un tel système d’attache moteur

Family Cites Families (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3374545D1 (en) * 1983-12-08 1987-12-23 Boeing Co Aft engine mount
JPH0311210Y2 (https=) * 1986-09-24 1991-03-19
FR2635751B1 (fr) * 1988-09-01 1991-01-04 Snecma Dispositif de fixation d'une biellette de suspension d'un turboreacteur
US5275357A (en) 1992-01-16 1994-01-04 General Electric Company Aircraft engine mount
US5320307A (en) * 1992-03-25 1994-06-14 General Electric Company Aircraft engine thrust mount
US5351930A (en) * 1992-08-11 1994-10-04 Lord Corporation Mounting for engines and the like
US5277382A (en) 1992-10-13 1994-01-11 General Electric Company Aircraft engine forward mount
US5303880A (en) 1992-10-28 1994-04-19 General Electric Company Aircraft engine pin mount
US5443229A (en) * 1993-12-13 1995-08-22 General Electric Company Aircraft gas turbine engine sideways mount
US5649417A (en) * 1995-03-24 1997-07-22 The Boeing Company Fail-safe engine mount system
US5860623A (en) * 1995-05-03 1999-01-19 The Boeing Company Three link failsafe engine mount
US5620154A (en) * 1995-05-03 1997-04-15 The Boeing Company Three link failsafe engine mount
US5725181A (en) * 1996-05-01 1998-03-10 The Boeing Company Aircraft engine thrust mount
US5921500A (en) * 1997-10-08 1999-07-13 General Electric Company Integrated failsafe engine mount
US5927644A (en) 1997-10-08 1999-07-27 General Electric Company Double failsafe engine mount

Also Published As

Publication number Publication date
JP4591903B2 (ja) 2010-12-01
BR0100649A (pt) 2001-10-09
JP2001336520A (ja) 2001-12-07
DE60104342T2 (de) 2005-08-11
DE60104342D1 (de) 2004-08-26
US6330995B1 (en) 2001-12-18
EP1129942A3 (en) 2001-12-12
EP1129942A2 (en) 2001-09-05
EP1129942B1 (en) 2004-07-21

Similar Documents

Publication Publication Date Title
BR0100649B1 (pt) junta esférica com translação e montagem para suportar um motor em um avião.
BR0007612B1 (pt) conjunto de palheta para um motor e mancal de luva.
BR0102647B1 (pt) sistema de montagem para a montagem de um motor em uma aeronave.
BR0203556B1 (pt) aeronave com carenagem ventral e junta para esta.
DE60006769D1 (de) Flugtriebwerksaufhängung mit integrierter Sicherheitsvorrichtung
PT1084334E (pt) Processo de funcionamento e dispositivo de motor com injeccao de ar comprimido adicional.
ITMO990280A0 (it) Motore termico alternativo dotato di equilibratura e precompressione
DE60108920D1 (de) Gedämpfte Schubbefestigung eines Triebwerkes
DE10195927T1 (de) Verallgemeinerte Textlokalisation in Bildern
BR0106243B1 (pt) junta cavilhada para conexão de primeiro e segundo componentes.
DE60117740D1 (de) Kraftfahrzeugvorbau mit Kühler und Kühlerbefestigungstruktur
DE60143914D1 (de) Tastkopf mit Lageranordnung
ES2160526B1 (es) Disposicion dotada de una primera junta homocinetica fija y un arbol de conexion.
DE602004002128D1 (de) Kardangelenk mit Reibungs- und Befestigungslagerbüchse
DE50206381D1 (de) Axiallager
GB0122096D0 (en) Thrust bearing assembly with preload spring
DE60011382D1 (de) Brennkraftmaschine mit Bremsanlage
DE60201976D1 (de) Flugzeugtriebwerk mit luft- und wassergekühlten gegenüberliegenden zylindern
DE60123661D1 (de) Selbstemulgierende lipidmatrix (selm)
DE59902532D1 (de) Gummigelagertes kugelgelenk mit spannungsoptimierter lagergeometrie
GB0102028D0 (en) An engine and bearings therefor
BR0302537B1 (pt) motor com injeção de combustìvel e ar.
DE60015963D1 (de) Ermüdungserleichterung an der struktur eines luftfahrzeuges
DE69900474D1 (de) Brennstoffpulsationsdämpfer mit vakuumgesteuerter vorspannung
BR0204639B1 (pt) colheitadeira dotada de suporte de duto e estrutura de transição.

Legal Events

Date Code Title Description
B06A Patent application procedure suspended [chapter 6.1 patent gazette]
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 20/02/2001, OBSERVADAS AS CONDICOES LEGAIS.

B21F Lapse acc. art. 78, item iv - on non-payment of the annual fees in time

Free format text: REFERENTE A 16A ANUIDADE.

B24J Lapse because of non-payment of annual fees (definitively: art 78 iv lpi, resolution 113/2013 art. 12)