FR3014972B1 - 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 - Google Patents
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-rotationInfo
- Publication number
- FR3014972B1 FR3014972B1 FR1362478A FR1362478A FR3014972B1 FR 3014972 B1 FR3014972 B1 FR 3014972B1 FR 1362478 A FR1362478 A FR 1362478A FR 1362478 A FR1362478 A FR 1362478A FR 3014972 B1 FR3014972 B1 FR 3014972B1
- Authority
- FR
- France
- Prior art keywords
- immobilized
- translation
- cap
- assembly
- locking device
- 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
Classifications
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- B64D27/40—
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- 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
- F16B—DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
- F16B39/00—Locking of screws, bolts or nuts
- F16B39/22—Locking of screws, bolts or nuts in which the locking takes place during screwing down or tightening
- F16B39/24—Locking of screws, bolts or nuts in which the locking takes place during screwing down or tightening by means of washers, spring washers, or resilient plates that lock against the object
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- 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
- F16B—DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
- F16B39/00—Locking of screws, bolts or nuts
- F16B39/02—Locking of screws, bolts or nuts in which the locking takes place after screwing down
- F16B39/10—Locking of screws, bolts or nuts in which the locking takes place after screwing down by a plate, spring, wire or ring immovable with regard to the bolt or object and mainly perpendicular to the axis of the bolt
- F16B39/108—Locking of screws, bolts or nuts in which the locking takes place after screwing down by a plate, spring, wire or ring immovable with regard to the bolt or object and mainly perpendicular to the axis of the bolt with a locking washer under the nut or bolt head having at least one tongue or lug folded against the nut or bolt head, or against the object itself
-
- 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
-
- 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
- F16B—DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
- F16B39/00—Locking of screws, bolts or nuts
- F16B39/02—Locking of screws, bolts or nuts in which the locking takes place after screwing down
- F16B39/04—Locking of screws, bolts or nuts in which the locking takes place after screwing down with a member penetrating the screw-threaded surface of at least one part, e.g. a pin, a wedge, cotter-pin, screw
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- 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
- 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
-
- 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
-
- 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T403/00—Joints and connections
- Y10T403/32—Articulated members
- Y10T403/32606—Pivoted
- Y10T403/32861—T-pivot, e.g., wrist pin, etc.
- Y10T403/32893—T-pivot, e.g., wrist pin, etc. including distinct pin retainer
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1362478A FR3014972B1 (fr) | 2013-12-12 | 2013-12-12 | 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 |
US14/553,432 US9593708B2 (en) | 2013-12-12 | 2014-11-25 | Assembly comprising an articulation spindle supported by a clevis and immobilized in translation by a blocking device integrating a double anti-rotation system |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1362478A FR3014972B1 (fr) | 2013-12-12 | 2013-12-12 | 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 |
Publications (2)
Publication Number | Publication Date |
---|---|
FR3014972A1 FR3014972A1 (fr) | 2015-06-19 |
FR3014972B1 true FR3014972B1 (fr) | 2016-04-22 |
Family
ID=50289922
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1362478A Active FR3014972B1 (fr) | 2013-12-12 | 2013-12-12 | 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 |
Country Status (2)
Country | Link |
---|---|
US (1) | US9593708B2 (fr) |
FR (1) | FR3014972B1 (fr) |
Families Citing this family (28)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
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 |
FR3016608B1 (fr) * | 2014-01-21 | 2016-02-26 | Airbus Operations Sas | Attache moteur pour aeronef. |
FR3021373B1 (fr) * | 2014-05-21 | 2016-12-09 | Snecma | Dispositif d'articulation a rotule pour une turbomachine. |
FR3021298B1 (fr) * | 2014-05-26 | 2016-07-01 | Airbus Operations Sas | Attache moteur pour un aeronef |
US10100779B2 (en) * | 2016-04-09 | 2018-10-16 | United Technologies Corporation | Enhanced durability drive link for high load misalignment |
FR3050719B1 (fr) * | 2016-04-28 | 2018-04-13 | Airbus Operations | Helice pour turbomachine d'aeronef comprenant des moyens de secours de calage en incidence de pale |
US10570950B2 (en) * | 2016-05-23 | 2020-02-25 | United Technologies Corporation | Spherical joint assembly with a spherical bearing between integral collars |
US10598211B2 (en) * | 2016-05-23 | 2020-03-24 | United Technologies Corporation | Spherical bearing sleeve configured with one or more discrete collars |
FR3059645B1 (fr) * | 2016-12-02 | 2018-12-07 | Safran Aircraft Engines | Dispositif de suspension pour turbomachine |
US20190293116A1 (en) * | 2016-12-03 | 2019-09-26 | Ge Aviation Systems, Llc | Spherical bearing system |
CN107939799A (zh) * | 2017-05-22 | 2018-04-20 | 深圳亚太航空技术有限公司 | 可快速拆卸的连接装置 |
CN107521706A (zh) * | 2017-07-28 | 2017-12-29 | 中国航空工业集团公司西安飞机设计研究所 | 发动机辅助安装接头 |
US10634092B2 (en) * | 2017-09-08 | 2020-04-28 | United Technologies Corporation | Linkage assembly preventing axial rotation of the link rod |
FR3074146B1 (fr) * | 2017-11-24 | 2019-10-18 | Airbus Operations | Axe de pivotement ameliore pour une attache-moteur d'aeronef |
FR3077560B1 (fr) * | 2018-02-06 | 2020-01-10 | Airbus Operations | Assemblage pour une attache-moteur d'aeronef comprenant un axe d'articulation supporte par une chape et immobile en translation |
FR3079892B1 (fr) * | 2018-04-10 | 2020-03-27 | Airbus Operations | Dispositif de liaison pivotante entre au moins deux pieces, aeronef comprenant un capot equipe dudit dispositif de liaison pivotante |
FR3081442B1 (fr) * | 2018-05-22 | 2020-05-08 | Airbus Operations | Dispositif de liaison pivotante entre au moins deux pieces, aeronef comprenant un capot equipe dudit dispositif de liaison pivotante |
FR3081836B1 (fr) * | 2018-06-01 | 2020-11-06 | Airbus Operations Sas | Ensemble propulsif d'aeronef et procede de verification de l'integrite d'une attache moteur de l'ensemble propulsif |
FR3088902B1 (fr) * | 2018-11-27 | 2020-11-06 | Safran Aircraft Engines | Assemblage pour ensemble moteur d’aéronef, comprenant une fonction anti-rotation améliorée |
FR3091519A1 (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 de type fourchette d’un pion de cisaillement, procédé de montage de ladite attache-moteur et aéronef comprenant ladite attache-moteur |
FR3091911A1 (fr) * | 2019-01-21 | 2020-07-24 | Airbus Operations (S.A.S.) | Dispositif de liaison pivotante entre au moins deux pièces, aéronef comprenant un capot équipé dudit dispositif de liaison pivotante |
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 |
US11479104B2 (en) | 2019-07-24 | 2022-10-25 | Honeywell International Inc. | System and method for gas turbine engine mount with seal |
FR3104219B1 (fr) * | 2019-12-10 | 2021-12-10 | Airbus Operations Sas | Assemblage comprenant un axe de liaison immobile en translation et en rotation, attache-moteur ou aéronef comprenant un tel assemblage |
US11066860B1 (en) * | 2020-01-06 | 2021-07-20 | Rohr, Inc. | Hinged assembly with fail-safe hinge pin |
TWI722932B (zh) * | 2020-06-24 | 2021-03-21 | 簡文豐 | 適用於鎖孔之安全鉸鎖裝置 |
GB2602160A (en) * | 2020-12-21 | 2022-06-22 | Airbus Operations Ltd | A pin joint assembly |
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GB186552A (en) * | 1922-02-23 | 1922-10-05 | Arthur Prince | Improvements in nut-locks |
FR1506796A (fr) * | 1968-12-16 | 1967-12-22 | Standard Pressed Steel Co | Dispositif de fixation de sécurité |
US3638980A (en) * | 1970-01-02 | 1972-02-01 | Standard Pressed Steel Co | Self-retained bolt assembly |
US3831888A (en) | 1972-07-27 | 1974-08-27 | Mc Donnell Douglas Corp | Aircraft engine suspension system |
JPS6014312A (ja) | 1983-07-04 | 1985-01-24 | Omron Tateisi Electronics Co | 自動電圧調整装置 |
JPS6289341U (fr) | 1985-11-27 | 1987-06-08 | ||
US4655657A (en) * | 1985-12-23 | 1987-04-07 | John A. Duran | Self-retaining positive locking bolt |
FR2635751B1 (fr) * | 1988-09-01 | 1991-01-04 | Snecma | Dispositif de fixation d'une biellette de suspension d'un turboreacteur |
US5176339A (en) | 1991-09-30 | 1993-01-05 | Lord Corporation | Resilient pivot type aircraft mounting |
DE4221250C2 (de) * | 1992-07-01 | 1995-10-05 | Daimler Benz Aerospace Airbus | Vorrichtung zur Sicherung |
FR2728538A1 (fr) | 1994-12-23 | 1996-06-28 | Eurocopter France | Dispositif de suspension anti-vibratoire de rotor d'helicoptere |
FR2799432A1 (fr) | 1999-10-07 | 2001-04-13 | Snecma | Suspension a securite integree pour groupes motopropulseurs d'aeronefs |
US6330995B1 (en) * | 2000-02-29 | 2001-12-18 | General Electric Company | Aircraft engine mount |
US6669393B2 (en) | 2001-10-10 | 2003-12-30 | General Electric Co. | Connector assembly for gas turbine engines |
US6843449B1 (en) | 2004-02-09 | 2005-01-18 | General Electric Company | Fail-safe aircraft engine mounting system |
FR2867155B1 (fr) | 2004-03-08 | 2007-06-29 | Snecma Moteurs | Suspension d'un moteur a la structure d'un avion |
US20060138295A1 (en) * | 2004-12-27 | 2006-06-29 | Frank Blateri | Apparatus and method for mounting a fixture |
FR2887851B1 (fr) * | 2005-06-29 | 2007-08-17 | Airbus France Sas | Mat d'accrochage de moteur pour aeronef |
FR2887852B1 (fr) * | 2005-06-29 | 2007-08-17 | Airbus France Sas | Mat d'accrochage de moteur pour aeronef |
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 |
FR2903382B1 (fr) | 2006-07-10 | 2008-10-10 | Airbus France Sas | Dispositif d'accrochage d'un moteur d'aeronef comportant deux bielles de reprise de poussee a emboitement transversal |
FR2958267B1 (fr) * | 2010-04-02 | 2012-03-23 | Airbus Operations Sas | Systeme d'axe pour ensemble de liaison d'un mat-reacteur sous une voilure d'aeronef |
US8348191B2 (en) | 2010-07-14 | 2013-01-08 | Spirit Aerosystems, Inc. | Fail-safe aircraft engine mounting apparatus |
FR2975132B1 (fr) * | 2011-05-09 | 2015-06-26 | Snecma | Bielles de suspension du canal de flux froid d'un turboreacteur a rotules excentriques |
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 |
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 |
FR3014973B1 (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 |
FR3014971B1 (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 |
-
2013
- 2013-12-12 FR FR1362478A patent/FR3014972B1/fr active Active
-
2014
- 2014-11-25 US US14/553,432 patent/US9593708B2/en active Active
Also Published As
Publication number | Publication date |
---|---|
US9593708B2 (en) | 2017-03-14 |
FR3014972A1 (fr) | 2015-06-19 |
US20150167726A1 (en) | 2015-06-18 |
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