FR2975132B1 - Bielles de suspension du canal de flux froid d'un turboreacteur a rotules excentriques - Google Patents
Bielles de suspension du canal de flux froid d'un turboreacteur a rotules excentriquesInfo
- Publication number
- FR2975132B1 FR2975132B1 FR1153947A FR1153947A FR2975132B1 FR 2975132 B1 FR2975132 B1 FR 2975132B1 FR 1153947 A FR1153947 A FR 1153947A FR 1153947 A FR1153947 A FR 1153947A FR 2975132 B1 FR2975132 B1 FR 2975132B1
- Authority
- FR
- France
- Prior art keywords
- turbojuster
- excentric
- balls
- flow channel
- cold flow
- 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
Links
- 239000000725 suspension Substances 0.000 title 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/20—Mounting or supporting of plant; Accommodating heat expansion or creep
-
- 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
- B64D29/00—Power-plant nacelles, fairings, or cowlings
- B64D29/06—Attaching of nacelles, fairings or cowlings
-
- 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
- F01D25/16—Arrangement of bearings; Supporting or mounting bearings in casings
- F01D25/162—Bearing supports
-
- 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
-
- 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
- F16C11/00—Pivots; Pivotal connections
- F16C11/04—Pivotal connections
- F16C11/06—Ball-joints; Other joints having more than one degree of angular freedom, i.e. universal joints
- F16C11/0614—Ball-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
-
- 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
- F16C2360/00—Engines or pumps
- F16C2360/23—Gas turbine engines
-
- 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
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Pivots And Pivotal Connections (AREA)
Priority Applications (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1153947A FR2975132B1 (fr) | 2011-05-09 | 2011-05-09 | Bielles de suspension du canal de flux froid d'un turboreacteur a rotules excentriques |
GB1207780.6A GB2490781B (en) | 2011-05-09 | 2012-05-03 | A device for assembly of a suspension member on a casing of a turbo-engine |
US13/465,302 US8596603B2 (en) | 2011-05-09 | 2012-05-07 | Suspension rods for the bypass flow duct of a turbojet with eccentric ball joints |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1153947A FR2975132B1 (fr) | 2011-05-09 | 2011-05-09 | Bielles de suspension du canal de flux froid d'un turboreacteur a rotules excentriques |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2975132A1 FR2975132A1 (fr) | 2012-11-16 |
FR2975132B1 true FR2975132B1 (fr) | 2015-06-26 |
Family
ID=46330761
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1153947A Active FR2975132B1 (fr) | 2011-05-09 | 2011-05-09 | Bielles de suspension du canal de flux froid d'un turboreacteur a rotules excentriques |
Country Status (3)
Country | Link |
---|---|
US (1) | US8596603B2 (fr) |
FR (1) | FR2975132B1 (fr) |
GB (1) | GB2490781B (fr) |
Families Citing this family (23)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2978985B1 (fr) * | 2011-08-10 | 2016-11-04 | Snecma | Suspension du canal de flux froid d'un turboreacteur par des bielles avec douilles en elastomere |
US8770513B2 (en) * | 2011-11-30 | 2014-07-08 | Honeywell International Inc. | Resilient aircraft engine mounts and aircraft engine mounting systems including the same |
FR3003896B1 (fr) * | 2013-03-29 | 2015-03-20 | Snecma | Dispositif d'articulation a rotule pour la suspension d'une turbomachine a un pylone ou la suspension d'un equipement au corps de la turbomachine |
GB201314667D0 (en) | 2013-08-16 | 2013-10-02 | Rolls Royce Plc | A panel attachment system |
US10202869B2 (en) * | 2013-08-22 | 2019-02-12 | United Technologies Corporation | Connection for a fairing in a mid-turbine frame of a gas turbine engine |
US20150117804A1 (en) * | 2013-10-30 | 2015-04-30 | United Technologies Corporation | Gas turbine engine bushing |
US9556902B2 (en) * | 2013-11-07 | 2017-01-31 | Cnh Industrial America Llc | Agricultural tandem pivot assembly |
FR3014970B1 (fr) | 2013-12-12 | 2016-01-22 | 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 |
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 |
GB201322048D0 (en) | 2013-12-13 | 2014-01-29 | Rolls Royce Deutschland | A joint between components |
FR3021373B1 (fr) * | 2014-05-21 | 2016-12-09 | Snecma | Dispositif d'articulation a rotule pour une turbomachine. |
US9656744B2 (en) * | 2014-05-21 | 2017-05-23 | Bell Helicopter Textron Inc. | Adjustable blade-to-hub lead-lag damper attachment |
US9784129B2 (en) * | 2014-08-01 | 2017-10-10 | Pratt & Whitney Canada Corp. | Rear mount assembly for gas turbine engine |
FR3027875A1 (fr) * | 2014-10-30 | 2016-05-06 | Airbus Operations Sas | Dispositif de fixation d'un moteur d'aeronef, et aeronef correspondant |
US10100779B2 (en) * | 2016-04-09 | 2018-10-16 | United Technologies Corporation | Enhanced durability drive link for high load misalignment |
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 |
GB2568756A (en) * | 2017-11-28 | 2019-05-29 | Airbus Operations Ltd | Fastener |
GB201810606D0 (en) * | 2018-06-28 | 2018-08-15 | Rolls Royce Plc | Gas turbine engine |
US10837320B2 (en) * | 2018-09-25 | 2020-11-17 | Honeywell International Inc. | Frangible strut for gas turbine engine |
US10823011B2 (en) * | 2019-02-07 | 2020-11-03 | Raytheon Technologies Corporation | Turbine engine tie rod systems |
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 |
FR3099800B1 (fr) * | 2019-08-09 | 2021-07-09 | Safran Aircraft Engines | Dispositif d'accrochage d'un boîtier d'alimentation en air d'un dispositif de refroidissement d'un carter de turbomachine |
FR3124228B1 (fr) * | 2021-06-18 | 2024-03-08 | Safran Ceram | Bride de liaison pour le raccordement d’un carter d’échappement et d’un cône d’éjection de gaz d’échappement d’un turboréacteur d’aéronef |
Family Cites Families (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2718756A (en) * | 1951-06-14 | 1955-09-27 | Gen Motors Corp | Mounting and supporting structure for aircraft gas turbine power plants having reduction gearing |
FR2630703B1 (fr) * | 1988-04-29 | 1990-08-24 | Aerospatiale | Tete de rotor de giravion a tirants interpales de rappel elastique avec amortissement incorpore |
AUPN313795A0 (en) * | 1995-05-23 | 1995-06-15 | Reilly, Bruce John | Adjustment of camber |
US6330995B1 (en) * | 2000-02-29 | 2001-12-18 | General Electric Company | Aircraft engine mount |
US6296203B1 (en) * | 2000-05-24 | 2001-10-02 | General Electric Company | Snubber thrust mount |
US7093996B2 (en) | 2003-04-30 | 2006-08-22 | General Electric Company | Methods and apparatus for mounting a gas turbine engine |
FR2867155B1 (fr) * | 2004-03-08 | 2007-06-29 | Snecma Moteurs | Suspension d'un moteur a la structure d'un avion |
FR2879695B1 (fr) * | 2004-12-16 | 2007-04-06 | Snecma Moteurs Sa | Dispositif de liaison, de longueur ajustable, entre deux pieces |
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 |
US8313293B2 (en) | 2009-05-15 | 2012-11-20 | Pratt & Whitney Canada Corp. | Turbofan mounting system |
GB2470586A (en) * | 2009-05-29 | 2010-12-01 | Rolls Royce Plc | Eccentric joint for actuator connection rod. |
-
2011
- 2011-05-09 FR FR1153947A patent/FR2975132B1/fr active Active
-
2012
- 2012-05-03 GB GB1207780.6A patent/GB2490781B/en active Active
- 2012-05-07 US US13/465,302 patent/US8596603B2/en active Active
Also Published As
Publication number | Publication date |
---|---|
US20120286126A1 (en) | 2012-11-15 |
GB201207780D0 (en) | 2012-06-13 |
FR2975132A1 (fr) | 2012-11-16 |
GB2490781B (en) | 2018-02-07 |
GB2490781A (en) | 2012-11-14 |
US8596603B2 (en) | 2013-12-03 |
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Legal Events
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PLFP | Fee payment |
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CD | Change of name or company name |
Owner name: SAFRAN AIRCRAFT ENGINES, FR Effective date: 20170719 |
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Year of fee payment: 9 |
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Year of fee payment: 10 |
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