BRPI0816415A2 - Indicador de carga - Google Patents
Indicador de cargaInfo
- Publication number
- BRPI0816415A2 BRPI0816415A2 BRPI0816415-0A2A BRPI0816415A BRPI0816415A2 BR PI0816415 A2 BRPI0816415 A2 BR PI0816415A2 BR PI0816415 A BRPI0816415 A BR PI0816415A BR PI0816415 A2 BRPI0816415 A2 BR PI0816415A2
- Authority
- BR
- Brazil
- Prior art keywords
- load
- load bearing
- cavity
- indicator
- bearing member
- Prior art date
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
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C23/00—Bearings for exclusively rotary movement adjustable for aligning or positioning
- F16C23/02—Sliding-contact bearings
- F16C23/04—Sliding-contact bearings self-adjusting
- F16C23/043—Sliding-contact bearings self-adjusting with spherical surfaces, e.g. spherical plain bearings
- F16C23/045—Sliding-contact bearings self-adjusting with spherical surfaces, e.g. spherical plain bearings for radial load mainly, e.g. radial spherical plain bearings
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/02—Undercarriages
-
- 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
-
- 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
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C11/00—Pivots; Pivotal connections
- F16C11/04—Pivotal connections
- F16C11/045—Pivotal connections with at least a pair of arms pivoting relatively to at least one other arm, all arms being mounted on one pin
-
- 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
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C17/00—Sliding-contact bearings for exclusively rotary movement
- F16C17/12—Sliding-contact bearings for exclusively rotary movement characterised by features not related to the direction of the load
- F16C17/24—Sliding-contact bearings for exclusively rotary movement characterised by features not related to the direction of the load with devices affected by abnormal or undesired positions, e.g. for preventing overheating, for safety
-
- 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
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C23/00—Bearings for exclusively rotary movement adjustable for aligning or positioning
- F16C23/02—Sliding-contact bearings
- F16C23/04—Sliding-contact bearings self-adjusting
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01L—MEASURING FORCE, STRESS, TORQUE, WORK, MECHANICAL POWER, MECHANICAL EFFICIENCY, OR FLUID PRESSURE
- G01L5/00—Apparatus for, or methods of, measuring force, work, mechanical power, or torque, specially adapted for specific purposes
- G01L5/0061—Force sensors associated with industrial machines or actuators
- G01L5/0071—Specific indicating arrangements, e.g. of overload
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01N—INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
- G01N19/00—Investigating materials by mechanical methods
- G01N19/08—Detecting presence of flaws or irregularities
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01N—INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
- G01N21/00—Investigating or analysing materials by the use of optical means, i.e. using sub-millimetre waves, infrared, visible or ultraviolet light
- G01N21/84—Systems specially adapted for particular applications
- G01N21/88—Investigating the presence of flaws or contamination
- G01N21/8803—Visual inspection
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01P—MEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION, OR SHOCK; INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT
- G01P15/00—Measuring acceleration; Measuring deceleration; Measuring shock, i.e. sudden change of acceleration
- G01P15/02—Measuring acceleration; Measuring deceleration; Measuring shock, i.e. sudden change of acceleration by making use of inertia forces using solid seismic masses
- G01P15/04—Measuring acceleration; Measuring deceleration; Measuring shock, i.e. sudden change of acceleration by making use of inertia forces using solid seismic masses for indicating maximum value
- G01P15/06—Measuring acceleration; Measuring deceleration; Measuring shock, i.e. sudden change of acceleration by making use of inertia forces using solid seismic masses for indicating maximum value using members subjected to a permanent deformation
-
- G—PHYSICS
- G08—SIGNALLING
- G08B—SIGNALLING OR CALLING SYSTEMS; ORDER TELEGRAPHS; ALARM SYSTEMS
- G08B23/00—Alarms responsive to unspecified undesired or abnormal conditions
-
- 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
- B64D2045/008—Devices for detecting or indicating hard landing
-
- 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
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C2326/00—Articles relating to transporting
- F16C2326/43—Aeroplanes; Helicopters
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB0718296A GB2452938B (en) | 2007-09-19 | 2007-09-19 | Load indicator |
PCT/GB2008/003187 WO2009037475A1 (en) | 2007-09-19 | 2008-09-19 | Load indicator |
Publications (1)
Publication Number | Publication Date |
---|---|
BRPI0816415A2 true BRPI0816415A2 (pt) | 2015-03-03 |
Family
ID=38670176
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BRPI0816415-0A2A BRPI0816415A2 (pt) | 2007-09-19 | 2008-09-19 | Indicador de carga |
Country Status (11)
Country | Link |
---|---|
US (1) | US8539843B2 (pt) |
EP (1) | EP2190744B1 (pt) |
JP (1) | JP4873391B2 (pt) |
CN (1) | CN101808902B (pt) |
AT (1) | ATE554003T1 (pt) |
BR (1) | BRPI0816415A2 (pt) |
CA (1) | CA2699705C (pt) |
ES (1) | ES2386570T3 (pt) |
GB (1) | GB2452938B (pt) |
RU (1) | RU2478921C2 (pt) |
WO (1) | WO2009037475A1 (pt) |
Families Citing this family (28)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB0723506D0 (en) * | 2007-12-03 | 2008-01-09 | Airbus Uk Ltd | Apparatus for indicating loading in a structure having exceeded a predetermined threshold |
EP2368797B1 (en) * | 2010-03-05 | 2015-10-28 | Goodrich Corporation | System for indicating an airplane hard landing |
GB2478579A (en) | 2010-03-11 | 2011-09-14 | Messier Dowty Ltd | Aircraft landing gear stop pad |
GB2485803B (en) * | 2010-11-24 | 2013-02-06 | Messier Dowty Ltd | Mechanical position indicator |
US9103849B2 (en) * | 2011-06-10 | 2015-08-11 | Shockwatch, Inc. | Impact indicator |
FR3000723B1 (fr) * | 2013-01-10 | 2015-01-16 | Messier Bugatti Dowty | Organe fusible destine a reunir deux chapes pour former une articulation |
US9499257B2 (en) * | 2013-06-17 | 2016-11-22 | Goodrich Corporation | Weight reducing landing gear features |
CN103983463B (zh) * | 2014-04-17 | 2016-08-24 | 中国航空工业集团公司沈阳飞机设计研究所 | 一种飞机机体与起落架联合加载的验证试验方法 |
CN107108039B (zh) * | 2015-01-07 | 2019-08-30 | 洛德公司 | 飞行器发动机安装架 |
EP3159260B1 (en) * | 2015-10-23 | 2019-11-27 | Safran Landing Systems UK Limited | Aircraft landing gear assembly including a health and usage monitoring system (hums) and method |
US10272991B2 (en) * | 2016-06-23 | 2019-04-30 | Goodrich Corporation | Metallic composite joint |
EP3336485B1 (en) | 2016-12-15 | 2020-09-23 | Safran Landing Systems UK Limited | Aircraft assembly including deflection sensor |
JP6728089B2 (ja) * | 2017-02-27 | 2020-07-22 | 三菱重工業株式会社 | 位置決定装置、それを備えた位置決定システム、及び位置決定方法並びに位置決定プログラム |
EP3379222B1 (en) | 2017-03-22 | 2020-12-30 | Methode Electronics Malta Ltd. | Magnetoelastic based sensor assembly |
US11221262B2 (en) | 2018-02-27 | 2022-01-11 | Methode Electronics, Inc. | Towing systems and methods using magnetic field sensing |
US11084342B2 (en) | 2018-02-27 | 2021-08-10 | Methode Electronics, Inc. | Towing systems and methods using magnetic field sensing |
US11014417B2 (en) | 2018-02-27 | 2021-05-25 | Methode Electronics, Inc. | Towing systems and methods using magnetic field sensing |
US11135882B2 (en) | 2018-02-27 | 2021-10-05 | Methode Electronics, Inc. | Towing systems and methods using magnetic field sensing |
EP3758959A4 (en) | 2018-02-27 | 2022-03-09 | Methode Electronics, Inc. | TOWING SYSTEMS AND METHODS USING MAGNETIC SENSING |
US11491832B2 (en) | 2018-02-27 | 2022-11-08 | Methode Electronics, Inc. | Towing systems and methods using magnetic field sensing |
US11130563B2 (en) * | 2018-11-07 | 2021-09-28 | The Boeing Company | Monolithic outboard gear beam support fitting |
CA3060756A1 (en) * | 2018-11-07 | 2020-05-07 | Bombardier Inc. | Hard landing indicator for an aircraft landing gear |
CN109979037A (zh) * | 2019-03-19 | 2019-07-05 | 四川函钛科技有限公司 | Qar参数综合可视化分析方法及系统 |
US11124293B2 (en) * | 2019-04-23 | 2021-09-21 | Goodrich Corporation | Integral bracket manifold for landing gear assemblies |
KR102325331B1 (ko) | 2019-12-20 | 2021-11-10 | 한화토탈 주식회사 | 터트-부탄올로부터 이소부틸렌의 제조방법 |
CN112429253B (zh) * | 2020-12-14 | 2022-10-11 | 江西洪都航空工业集团有限责任公司 | 一种加速度重着陆指示器 |
CN113062934B (zh) * | 2021-04-23 | 2022-05-27 | 中铁工程装备集团有限公司 | 一种盾构机主驱动减速机过载保护器及盾构机 |
FR3136264A1 (fr) * | 2022-06-03 | 2023-12-08 | Safran Landing Systems | Dispositif de blocage d’une broche d’arrêt |
Family Cites Families (27)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2960289A (en) * | 1958-07-07 | 1960-11-15 | Cleveland Pneumatic Ind Inc | Aircraft landing gear |
GB1027395A (en) * | 1962-02-16 | 1966-04-27 | Nat Res Dev | Controlled fluid lubricated bearings |
US3237590A (en) * | 1963-09-13 | 1966-03-01 | Bendix Corp | Strain gauge means |
SU467246A1 (ru) | 1973-02-14 | 1975-04-15 | Краснодарский Филиал Вниимонтаж Спецстрой Всесоюзного Научно-Исследовательского Института По Монтажным И Специальным Строительным Работам | Устройство дл контрол усилий зат жки резьбовых соединений |
US3845919A (en) * | 1974-01-07 | 1974-11-05 | Boeing Co | Landing gear truck pitch damping |
US3948141A (en) * | 1974-08-20 | 1976-04-06 | Katsumi Shinjo | Load indicating washer |
JPS5746842A (en) * | 1980-08-15 | 1982-03-17 | Teijin Ltd | High frequency welding method |
US4392623A (en) * | 1980-12-22 | 1983-07-12 | The Boeing Company | Fused connection adapted to fail under different overloads acting in different directions |
FR2511103A1 (fr) * | 1981-08-10 | 1983-02-11 | Aerospatiale | Composants munis d'un dispositif d'absorption d'energie par deformation plastique et/ou de limitation d'effort, et trains d'atterrissage d'aerodynes equipes de tels composants |
US4373862A (en) * | 1981-10-26 | 1983-02-15 | United Technologies Corporation | Rotor blade shaft integrity monitoring system |
US4447388A (en) * | 1981-11-30 | 1984-05-08 | The United States Of America As Represented By The United States Department Of Energy | Bolt failure detection |
DE3343495A1 (de) * | 1983-12-01 | 1985-07-18 | Paul 7936 Allmendingen Friese | Dehnbruch-anzeiger |
JPS60209137A (ja) * | 1984-04-03 | 1985-10-21 | Topy Ind Ltd | 疲労損傷予知法 |
US4698623A (en) * | 1984-11-07 | 1987-10-06 | Smith Richard G | Overload detection apparatus |
JPS6261898A (ja) * | 1985-09-10 | 1987-03-18 | ニユ−モ・コ−ポレ−シヨン | 着陸装置 |
US4869444A (en) * | 1986-09-30 | 1989-09-26 | The Boeing Company | Adjustable two-stage aircraft landing gear system |
GB8815826D0 (en) * | 1988-07-04 | 1988-08-10 | Westland Helicopters | Method & apparatus for detecting cracks |
SU1658186A1 (ru) * | 1989-03-20 | 1991-06-23 | Киевский Политехнический Институт Им.50-Летия Великой Октябрьской Социалистической Революции | Индикатор виброперегрузок |
JP3037370B2 (ja) * | 1990-07-11 | 2000-04-24 | 東芝エンジニアリング株式会社 | ピン形ロードセル |
JPH11512366A (ja) | 1995-09-14 | 1999-10-26 | シコルスキー エアクラフト コーポレイション | 衝撃荷重の大きさを示す手段を含むエネルギー吸収着陸装置/テールパイプ滑走機 |
GB9828475D0 (en) * | 1998-12-24 | 1999-02-17 | British Aerospace | Load measurement |
AUPR001800A0 (en) | 2000-09-08 | 2000-10-05 | Structural Monitoring Systems Ltd | Method and apparatus for monitoring the integrity of structures |
GB0428378D0 (en) * | 2004-12-24 | 2005-02-02 | Airbus Uk Ltd | Apparatus and method for measuring loads sustained by a bearing pin |
US7193530B2 (en) * | 2005-03-29 | 2007-03-20 | Nance C Kirk | Aircraft landing gear automated inspection and life limitation escalation system and method |
GB2452939B (en) * | 2007-09-19 | 2011-09-07 | Messier Dowty Ltd | Overload detection |
GB2453554B (en) * | 2007-10-09 | 2012-03-14 | Messier Dowty Ltd | Load detection in an aircraft landing gear |
GB0723506D0 (en) * | 2007-12-03 | 2008-01-09 | Airbus Uk Ltd | Apparatus for indicating loading in a structure having exceeded a predetermined threshold |
-
2007
- 2007-09-19 GB GB0718296A patent/GB2452938B/en not_active Expired - Fee Related
-
2008
- 2008-09-19 CA CA2699705A patent/CA2699705C/en active Active
- 2008-09-19 US US12/678,970 patent/US8539843B2/en active Active
- 2008-09-19 AT AT08806342T patent/ATE554003T1/de active
- 2008-09-19 ES ES08806342T patent/ES2386570T3/es active Active
- 2008-09-19 RU RU2010115338/11A patent/RU2478921C2/ru not_active IP Right Cessation
- 2008-09-19 CN CN2008801077906A patent/CN101808902B/zh active Active
- 2008-09-19 WO PCT/GB2008/003187 patent/WO2009037475A1/en active Application Filing
- 2008-09-19 BR BRPI0816415-0A2A patent/BRPI0816415A2/pt not_active IP Right Cessation
- 2008-09-19 EP EP08806342A patent/EP2190744B1/en active Active
- 2008-09-19 JP JP2010525431A patent/JP4873391B2/ja not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
US20100257946A1 (en) | 2010-10-14 |
EP2190744A1 (en) | 2010-06-02 |
CA2699705A1 (en) | 2009-03-26 |
ATE554003T1 (de) | 2012-05-15 |
JP4873391B2 (ja) | 2012-02-08 |
CN101808902B (zh) | 2013-04-24 |
RU2010115338A (ru) | 2011-10-27 |
EP2190744B1 (en) | 2012-04-18 |
US8539843B2 (en) | 2013-09-24 |
WO2009037475A1 (en) | 2009-03-26 |
ES2386570T3 (es) | 2012-08-23 |
CA2699705C (en) | 2014-11-18 |
JP2010539509A (ja) | 2010-12-16 |
GB2452938B (en) | 2011-08-10 |
RU2478921C2 (ru) | 2013-04-10 |
GB0718296D0 (en) | 2007-10-31 |
GB2452938A (en) | 2009-03-25 |
CN101808902A (zh) | 2010-08-18 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
BRPI0816415A2 (pt) | Indicador de carga | |
Rupp et al. | Practice guidelines for central venous access: a report by the American Society of Anesthesiologists Task Force on Central Venous Access | |
BR112012014006A2 (pt) | conjunto de trava para um membro de desgaste da escavadeira | |
BRPI0816659A2 (pt) | Garrafa acumuladora compensada com pressão | |
TW200718843A (en) | Space structure | |
EP2165024A4 (en) | STRUCTURAL SUSTAINABLE GAS SAFETY | |
WO2013070794A3 (en) | Analyte monitoring device and methods | |
BR112012033287B8 (pt) | sistema, conjunto de transdutor, e, método | |
ATE548050T1 (de) | Diagnoseverfahren | |
BR112014026273A2 (pt) | meio de união para acoplamento de dois elementos de construção; união de dois elementos de construção; e elemento de construção para utilização com uma união | |
DK2024089T3 (da) | Kuvette | |
AU2012300631A8 (en) | A load-indicating device | |
BRPI0606686A2 (pt) | elemento de amortecimento para revestimento de moinho | |
ATE496234T1 (de) | Bauteil mit innen- und aussenverzahnung | |
EP2345532A3 (en) | Oblong configuration for bonded patch | |
BR112015013968A2 (pt) | quadro de eletrônica para uso com segmentos de conduto acoplados | |
AU2012307532B2 (en) | Drain for a floor-level shower | |
WO2011153324A3 (en) | Lift arm assembly | |
MX357873B (es) | Ensamble de acoplamiento. | |
WO2014189588A3 (en) | Engine mount waiting fail safe lug joint with reduced dynamic amplification factor | |
ATE446235T1 (de) | Zahnstangenlenkung mit unterschiedlichen wandstärken | |
EA201492025A1 (ru) | Взвешивающий блок | |
EP2819209A3 (en) | Battery casing and battery assembly | |
DK1977934T3 (da) | Buffer til beskyttelse af et förste element, når det stöder imod et andet element | |
WO2009095110A3 (de) | Sensor mit gehäuse, sensormodul und einlegeteil |
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 6A E 7A 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: EM VIRTUDE DO ARQUIVAMENTO PUBLICADO NA RPI 2343 DE 01-12-2015 E CONSIDERANDO AUSENCIA DE MANIFESTACAO DENTRO DOS PRAZOS LEGAIS, INFORMO QUE CABE SER MANTIDO O ARQUIVAMENTO DO PEDIDO DE PATENTE, CONFORME O DISPOSTO NO ARTIGO 12, DA RESOLUCAO 113/2013. |