BR112016010876A2 - - Google Patents
Info
- Publication number
- BR112016010876A2 BR112016010876A2 BR112016010876A BR112016010876A BR112016010876A2 BR 112016010876 A2 BR112016010876 A2 BR 112016010876A2 BR 112016010876 A BR112016010876 A BR 112016010876A BR 112016010876 A BR112016010876 A BR 112016010876A BR 112016010876 A2 BR112016010876 A2 BR 112016010876A2
- Authority
- BR
- Brazil
Links
Classifications
-
- G—PHYSICS
- G06—COMPUTING OR CALCULATING; COUNTING
- G06F—ELECTRIC DIGITAL DATA PROCESSING
- G06F11/00—Error detection; Error correction; Monitoring
- G06F11/30—Monitoring
- G06F11/34—Recording or statistical evaluation of computer activity, e.g. of down time, of input/output operation ; Recording or statistical evaluation of user activity, e.g. usability assessment
- G06F11/3409—Recording or statistical evaluation of computer activity, e.g. of down time, of input/output operation ; Recording or statistical evaluation of user activity, e.g. usability assessment for performance assessment
- G06F11/3433—Recording or statistical evaluation of computer activity, e.g. of down time, of input/output operation ; Recording or statistical evaluation of user activity, e.g. usability assessment for performance assessment for load management
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- 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
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/02—Aircraft characterised by the type or position of power plants
- B64D27/10—Aircraft characterised by the type or position of power plants of gas-turbine type
-
- 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
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/40—Arrangements for mounting power plants in aircraft
-
- 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
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/40—Arrangements for mounting power plants in aircraft
- B64D27/402—Arrangements for mounting power plants in aircraft comprising box like supporting frames, e.g. pylons or arrangements for embracing the power plant
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
- F01D25/04—Antivibration arrangements
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
- F01D25/28—Supporting or mounting arrangements, e.g. for turbine casing
-
- G—PHYSICS
- G06—COMPUTING OR CALCULATING; COUNTING
- G06F—ELECTRIC DIGITAL DATA PROCESSING
- G06F11/00—Error detection; Error correction; Monitoring
- G06F11/30—Monitoring
- G06F11/34—Recording or statistical evaluation of computer activity, e.g. of down time, of input/output operation ; Recording or statistical evaluation of user activity, e.g. usability assessment
- G06F11/3447—Performance evaluation by modeling
-
- G—PHYSICS
- G06—COMPUTING OR CALCULATING; COUNTING
- G06F—ELECTRIC DIGITAL DATA PROCESSING
- G06F11/00—Error detection; Error correction; Monitoring
- G06F11/30—Monitoring
- G06F11/34—Recording or statistical evaluation of computer activity, e.g. of down time, of input/output operation ; Recording or statistical evaluation of user activity, e.g. usability assessment
- G06F11/3466—Performance evaluation by tracing or monitoring
-
- 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
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/40—Arrangements for mounting power plants in aircraft
- B64D27/404—Suspension arrangements specially adapted for supporting vertical loads
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2220/00—Application
- F05D2220/30—Application in turbines
- F05D2220/32—Application in turbines in gas turbines
- F05D2220/323—Application in turbines in gas turbines for aircraft propulsion, e.g. jet engines
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2230/00—Manufacture
- F05D2230/60—Assembly methods
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2240/00—Components
- F05D2240/90—Mounting on supporting structures or systems
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2260/00—Function
- F05D2260/96—Preventing, counteracting or reducing vibration or noise
-
- G—PHYSICS
- G06—COMPUTING OR CALCULATING; COUNTING
- G06F—ELECTRIC DIGITAL DATA PROCESSING
- G06F11/00—Error detection; Error correction; Monitoring
- G06F11/30—Monitoring
- G06F11/34—Recording or statistical evaluation of computer activity, e.g. of down time, of input/output operation ; Recording or statistical evaluation of user activity, e.g. usability assessment
- G06F11/3409—Recording or statistical evaluation of computer activity, e.g. of down time, of input/output operation ; Recording or statistical evaluation of user activity, e.g. usability assessment for performance assessment
-
- G—PHYSICS
- G06—COMPUTING OR CALCULATING; COUNTING
- G06F—ELECTRIC DIGITAL DATA PROCESSING
- G06F11/00—Error detection; Error correction; Monitoring
- G06F11/30—Monitoring
- G06F11/34—Recording or statistical evaluation of computer activity, e.g. of down time, of input/output operation ; Recording or statistical evaluation of user activity, e.g. usability assessment
- G06F11/3409—Recording or statistical evaluation of computer activity, e.g. of down time, of input/output operation ; Recording or statistical evaluation of user activity, e.g. usability assessment for performance assessment
- G06F11/3419—Recording or statistical evaluation of computer activity, e.g. of down time, of input/output operation ; Recording or statistical evaluation of user activity, e.g. usability assessment for performance assessment by assessing time
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- 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
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/40—Weight reduction
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Theoretical Computer Science (AREA)
- General Physics & Mathematics (AREA)
- Quality & Reliability (AREA)
- Physics & Mathematics (AREA)
- Computer Hardware Design (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Life Sciences & Earth Sciences (AREA)
- Bioinformatics & Cheminformatics (AREA)
- Bioinformatics & Computational Biology (AREA)
- Evolutionary Biology (AREA)
- Vibration Prevention Devices (AREA)
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US201361905526P | 2013-11-18 | 2013-11-18 | |
| US61/905,526 | 2013-11-18 | ||
| PCT/US2014/066140 WO2015074043A2 (en) | 2013-11-18 | 2014-11-18 | Turboprop engine attachment systems and methods |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| BR112016010876A2 true BR112016010876A2 (enExample) | 2017-08-08 |
| BR112016010876B1 BR112016010876B1 (pt) | 2022-02-01 |
Family
ID=52103162
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| BR112016010876-0A BR112016010876B1 (pt) | 2013-11-18 | 2014-11-18 | Sistema de fixação de motor e método de fixação de um motor turboélice |
Country Status (5)
| Country | Link |
|---|---|
| US (1) | US10144526B2 (enExample) |
| EP (1) | EP3071481B1 (enExample) |
| CN (1) | CN106414241B (enExample) |
| BR (1) | BR112016010876B1 (enExample) |
| WO (1) | WO2015074043A2 (enExample) |
Families Citing this family (23)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP3455128A1 (en) * | 2016-05-13 | 2019-03-20 | LORD Corporation | Isolator devices, systems and methods for aircraft |
| FR3053661B1 (fr) | 2016-07-11 | 2018-07-13 | Safran Aircraft Engines | Dispositif de propulsion pour un aeronef, tel par exemple qu'un turbopropulseur |
| FR3058704B1 (fr) * | 2016-11-14 | 2018-11-16 | Safran Aircraft Engines | Berceau bipartite a coulissement pour turbopropulseur |
| US11485507B2 (en) * | 2016-12-20 | 2022-11-01 | Bombardier Inc. | Thrust link with tuned absorber |
| FR3061149B1 (fr) * | 2016-12-27 | 2023-11-03 | Airbus Operations Sas | Structure primaire d'un mat pour groupe propulseur d'aeronef comportant une partie pyramidale a montants convergents |
| EP3539865A1 (en) | 2018-03-12 | 2019-09-18 | Ge Avio S.r.l. | Fan blade support assembly |
| WO2020210800A1 (en) * | 2019-04-11 | 2020-10-15 | Aero Innovations LLC | Aircraft engine adapter system |
| US11635024B2 (en) | 2019-08-16 | 2023-04-25 | Pratt & Whitney Canada Corp. | Pusher turboprop powerplant installation |
| FR3106126B1 (fr) * | 2020-01-10 | 2022-01-07 | Safran Aircraft Engines | Assemblage entre un pylône d’aéronef et une turbomachine |
| US11674414B2 (en) * | 2021-03-19 | 2023-06-13 | Pratt & Whitney Canada Corp. | Gas turbine engine and mount assembly therefor |
| GB202117777D0 (en) * | 2021-12-09 | 2022-01-26 | Rolls Royce Plc | Support structure for attaching a gas turbine engine to an aircraft pylon |
| US12103692B2 (en) * | 2021-12-20 | 2024-10-01 | Textron Innovations Inc. | Engine truss for aircraft |
| US12415610B2 (en) * | 2022-05-13 | 2025-09-16 | The Boeing Company | Strut assembly and method for coupling an engine to a wing of an aircraft |
| FR3137367A1 (fr) * | 2022-07-04 | 2024-01-05 | Airbus Operations (S.A.S.) | Structure en treillis renforcée et aéronef comprenant au moins une telle structure |
| FR3147252A1 (fr) * | 2023-03-29 | 2024-10-04 | Airbus Operations | Ensemble propulsif d’aéronef comportant une nacelle avec un châssis en t |
| FR3148063A1 (fr) | 2023-04-21 | 2024-10-25 | Airbus Operations | Ensemble pour la fixation de poutres comportant une plaque support et deux ferrures de part et d’autre de la plaque support |
| US12270313B2 (en) * | 2023-09-01 | 2025-04-08 | Pratt & Whitney Canada Corp. | Engine carcass stiffener for high maneuver loads |
| CN122186407A (zh) * | 2023-09-25 | 2026-06-12 | 通用电气公司 | 可变直径推力连杆设备 |
| US12509999B2 (en) | 2023-09-25 | 2025-12-30 | General Electric Company | Viscous damper apparatus and associated methods to control a response to a resonant vibration frequency |
| US12529323B2 (en) | 2023-09-25 | 2026-01-20 | General Electric Company | Variable diameter thrust link apparatus |
| CN117699021A (zh) * | 2023-12-28 | 2024-03-15 | 中国航空工业集团公司西安飞机设计研究所 | 一种桁架式发动机安装结构 |
| US12509237B2 (en) * | 2024-01-29 | 2025-12-30 | Airbus Operations Sas | Forward engine mount for a half or full wraparound pylon |
| FR3166886A1 (fr) * | 2024-09-30 | 2026-04-03 | Airbus Operations | Ensemble de propulsion d’aéronef comprenant une structure porteuse intercalée entre une motorisation et une structure primaire d’un mât |
Family Cites Families (22)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2539960A (en) | 1946-05-22 | 1951-01-30 | Bristol Aeroplane Co Ltd | Mounting structure for gas-turbine power plants for aircraft |
| US3208217A (en) | 1964-08-28 | 1965-09-28 | Gen Electric | Turbine engine and gearbox mounting arrangement |
| US3502287A (en) * | 1968-10-01 | 1970-03-24 | David B Lindsay | Aircraft engine mounting system |
| US5918833A (en) * | 1997-01-16 | 1999-07-06 | Applied Power Inc. | Hydraulic torque restraint system |
| DE19713365C1 (de) | 1997-04-01 | 1998-10-22 | Deutsch Zentr Luft & Raumfahrt | Triebwerksaufhängung, insbesondere für Propellerflugzeuge, mit einem Stabwerk zur Befestigung eines Triebwerks |
| US6126110A (en) | 1997-12-22 | 2000-10-03 | Mcdonnell Douglas Corporation | Horizontally opposed trunnion forward engine mount system supported beneath a wing pylon |
| FR2851226B1 (fr) * | 2003-02-19 | 2005-05-20 | Snecma Moteurs | Structure porteuse pour un turbopropulseur et ensemble comportant une telle structure porteuse |
| FR2862612B1 (fr) | 2003-11-25 | 2006-02-17 | Airbus France | Dispositif d'accrochage d'un moteur sous une voilure d'aeronef |
| FR2862610B1 (fr) | 2003-11-25 | 2007-03-23 | Airbus France | Dispositif d'accrochage reliant un moteur et une voilure d'aeronef |
| FR2862611B1 (fr) | 2003-11-25 | 2007-03-09 | Airbus France | Dispositif d'accrochage d'un moteur sous une voilure d'aeronef |
| FR2862945B1 (fr) | 2003-12-01 | 2006-04-28 | Airbus France | Dispositif d'accrochage d'un turbopropulseur sous une voilure d'aeronef. |
| FR2862944B1 (fr) | 2003-12-01 | 2006-02-24 | Airbus France | Dispositif d'accrochage d'un turbopropulseur sous une voilure d'aeronef |
| FR2883256B1 (fr) | 2005-03-18 | 2008-10-24 | Airbus France Sas | Attache moteur d'un systeme de montage interpose entre un mat d'accrochage et un moteur d'aeronef |
| FR2885877B1 (fr) | 2005-05-23 | 2008-12-12 | Airbus France Sas | Mat d'accrochage de turboreacteur pour aeronef |
| FR2891526B1 (fr) | 2005-10-03 | 2007-11-02 | Airbus France Sas | Mat d'accrochage de turboreacteur pour aeronef |
| US8439299B2 (en) | 2005-12-21 | 2013-05-14 | General Electric Company | Active cancellation and vibration isolation with feedback and feedforward control for an aircraft engine mount |
| FR2916736B1 (fr) * | 2007-06-04 | 2009-09-04 | Airbus France Sa | Dispositif d'accrochage d'un turbopropulseur d'aeronef comprenant des moyens de fixation hydrauliques. |
| US20090278021A1 (en) | 2008-05-06 | 2009-11-12 | Eads Construcciones Aeronauticas, S.A. | Device for removing and installing aircraft components |
| FR2939103B1 (fr) | 2008-12-01 | 2011-01-21 | Airbus France | Systeme hydraulique de transmission d'efforts entre un turbopropulseur d'aeronef et un dispositif d'accrochage |
| EP2382130B1 (en) | 2009-01-26 | 2017-09-27 | LORD Corporation | Aircraft engine mounting system and method of mounting aircraft engines |
| FR2955311B1 (fr) | 2010-01-15 | 2012-03-23 | Airbus Operations Sas | Dispositif d'accrochage d'un turbopropulseur, de preference sous une voilure d'aeronef |
| EP3184433B1 (en) * | 2010-06-14 | 2018-07-25 | LORD Corporation | A helicopter engine mounting system and methods |
-
2014
- 2014-11-18 CN CN201480063026.9A patent/CN106414241B/zh active Active
- 2014-11-18 EP EP14812834.1A patent/EP3071481B1/en active Active
- 2014-11-18 WO PCT/US2014/066140 patent/WO2015074043A2/en not_active Ceased
- 2014-11-18 BR BR112016010876-0A patent/BR112016010876B1/pt active IP Right Grant
- 2014-11-18 US US15/034,443 patent/US10144526B2/en active Active
Also Published As
| Publication number | Publication date |
|---|---|
| CN106414241B (zh) | 2019-03-01 |
| WO2015074043A3 (en) | 2015-07-16 |
| EP3071481B1 (en) | 2020-01-08 |
| WO2015074043A2 (en) | 2015-05-21 |
| US10144526B2 (en) | 2018-12-04 |
| CN106414241A (zh) | 2017-02-15 |
| US20160280381A1 (en) | 2016-09-29 |
| BR112016010876B1 (pt) | 2022-02-01 |
| EP3071481A2 (en) | 2016-09-28 |
Similar Documents
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| B06U | Preliminary requirement: requests with searches performed by other patent offices: procedure suspended [chapter 6.21 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 18/11/2014, OBSERVADAS AS CONDICOES LEGAIS. |