FR2677723A1 - Dispositif de liaison elastique entre deux pieces, procede de fabrication de ce dispositif, et installation pour la mise en óoeuvre de ce procede. - Google Patents
Dispositif de liaison elastique entre deux pieces, procede de fabrication de ce dispositif, et installation pour la mise en óoeuvre de ce procede. Download PDFInfo
- Publication number
- FR2677723A1 FR2677723A1 FR9107336A FR9107336A FR2677723A1 FR 2677723 A1 FR2677723 A1 FR 2677723A1 FR 9107336 A FR9107336 A FR 9107336A FR 9107336 A FR9107336 A FR 9107336A FR 2677723 A1 FR2677723 A1 FR 2677723A1
- Authority
- FR
- France
- Prior art keywords
- tubular element
- hooping
- parts
- envelope
- sleeve
- 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.)
- Granted
Links
Classifications
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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
- F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
- F16F1/00—Springs
- F16F1/36—Springs made of rubber or other material having high internal friction, e.g. thermoplastic elastomers
- F16F1/38—Springs made of rubber or other material having high internal friction, e.g. thermoplastic elastomers with a sleeve of elastic material between a rigid outer sleeve and a rigid inner sleeve or pin, i.e. bushing-type
- F16F1/3807—Springs made of rubber or other material having high internal friction, e.g. thermoplastic elastomers with a sleeve of elastic material between a rigid outer sleeve and a rigid inner sleeve or pin, i.e. bushing-type characterised by adaptations for particular modes of stressing
- F16F1/3814—Springs made of rubber or other material having high internal friction, e.g. thermoplastic elastomers with a sleeve of elastic material between a rigid outer sleeve and a rigid inner sleeve or pin, i.e. bushing-type characterised by adaptations for particular modes of stressing characterised by adaptations to counter axial forces
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/51—Damping of blade movements
-
- 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
- F16C7/00—Connecting-rods or like links pivoted at both ends; Construction of connecting-rod heads
- F16C7/04—Connecting-rods or like links pivoted at both ends; Construction of connecting-rod heads with elastic intermediate part of fluid cushion
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60G—VEHICLE SUSPENSION ARRANGEMENTS
- B60G2202/00—Indexing codes relating to the type of spring, damper or actuator
- B60G2202/10—Type of spring
- B60G2202/14—Plastic spring, e.g. rubber
- B60G2202/142—Plastic spring, e.g. rubber subjected to shear, e.g. Neidhart type
- B60G2202/1422—Axial
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60G—VEHICLE SUSPENSION ARRANGEMENTS
- B60G2202/00—Indexing codes relating to the type of spring, damper or actuator
- B60G2202/10—Type of spring
- B60G2202/14—Plastic spring, e.g. rubber
- B60G2202/142—Plastic spring, e.g. rubber subjected to shear, e.g. Neidhart type
- B60G2202/1424—Torsional
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60G—VEHICLE SUSPENSION ARRANGEMENTS
- B60G2206/00—Indexing codes related to the manufacturing of suspensions: constructional features, the materials used, procedures or tools
- B60G2206/01—Constructional features of suspension elements, e.g. arms, dampers, springs
- B60G2206/10—Constructional features of arms
- B60G2206/11—Constructional features of arms the arm being a radius or track or torque or steering rod or stabiliser end link
- B60G2206/111—Constructional features of arms the arm being a radius or track or torque or steering rod or stabiliser end link of adjustable length
- B60G2206/1114—Self-adjustable during driving
-
- 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
- F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
- F16F2236/00—Mode of stressing of basic spring or damper elements or devices incorporating such elements
- F16F2236/06—Tension
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Health & Medical Sciences (AREA)
- Child & Adolescent Psychology (AREA)
- Springs (AREA)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR9107336A FR2677723A1 (fr) | 1991-06-14 | 1991-06-14 | Dispositif de liaison elastique entre deux pieces, procede de fabrication de ce dispositif, et installation pour la mise en óoeuvre de ce procede. |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR9107336A FR2677723A1 (fr) | 1991-06-14 | 1991-06-14 | Dispositif de liaison elastique entre deux pieces, procede de fabrication de ce dispositif, et installation pour la mise en óoeuvre de ce procede. |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2677723A1 true FR2677723A1 (fr) | 1992-12-18 |
FR2677723B1 FR2677723B1 (US06559137-20030506-C00071.png) | 1995-02-17 |
Family
ID=9413885
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR9107336A Granted FR2677723A1 (fr) | 1991-06-14 | 1991-06-14 | Dispositif de liaison elastique entre deux pieces, procede de fabrication de ce dispositif, et installation pour la mise en óoeuvre de ce procede. |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR2677723A1 (US06559137-20030506-C00071.png) |
Cited By (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0621936A1 (en) * | 1992-09-09 | 1994-11-02 | Massachusetts Institute Of Technology | Replicated-in-place internal viscous shear damper for machine structures and components |
WO1995002131A1 (en) * | 1993-07-08 | 1995-01-19 | United Technologies Corporation | Split tubular elastomer damper |
WO1999006734A1 (en) * | 1997-08-04 | 1999-02-11 | Lord Corporation | Fluid and elastomer damper |
FR2818717A1 (fr) | 2000-12-26 | 2002-06-28 | Eurocopter France | Dispositif de liaison elastique amortie et son procede de fabrication |
EP1514960A3 (de) * | 2003-09-10 | 2005-12-07 | Groz-Beckert KG | Vibrationsarmes Fachbildesystem |
EP1655159A1 (en) * | 2004-11-03 | 2006-05-10 | C.R.F. Società Consortile per Azioni | Suspension system with longitudinal interconnection for a vehicle |
US7607892B2 (en) | 2005-09-21 | 2009-10-27 | Eurocopter | Rotorcraft rotor with blades hinged in flap and in lag |
FR2952150A1 (fr) * | 2009-11-02 | 2011-05-06 | Airbus Operations Sas | Bielle structurale comportant un mode filtrant des vibrations |
EP2508764A1 (en) * | 2011-04-04 | 2012-10-10 | Bell Helicopter Textron Inc. | Self pumping and priming ahesive joint system |
US20130099051A1 (en) * | 2010-06-14 | 2013-04-25 | Snecma | Turboshaft engine attached to a pylon of the fuselage of an aircraft by a failsafe suspension system |
US20220194636A1 (en) * | 2020-12-17 | 2022-06-23 | Maxar Space Llc | Passively damped end fittings and brackets |
IT202100001028A1 (it) * | 2021-01-21 | 2022-07-21 | Mecaer Aviation Group S P A | Asta smorzante per veicoli |
US11472380B2 (en) * | 2019-10-02 | 2022-10-18 | Zf Active Safety Gmbh | Force input member for a brake actuating device |
Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE714563C (de) * | 1938-03-20 | 1941-12-02 | Continental Gummi Werke Ag | Abfederung, insbesondere fuer Kraftfahrzeuge |
US3171622A (en) * | 1962-01-02 | 1965-03-02 | Ford Motor Co | Resilient mount |
-
1991
- 1991-06-14 FR FR9107336A patent/FR2677723A1/fr active Granted
Patent Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE714563C (de) * | 1938-03-20 | 1941-12-02 | Continental Gummi Werke Ag | Abfederung, insbesondere fuer Kraftfahrzeuge |
US3171622A (en) * | 1962-01-02 | 1965-03-02 | Ford Motor Co | Resilient mount |
Cited By (22)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0621936A1 (en) * | 1992-09-09 | 1994-11-02 | Massachusetts Institute Of Technology | Replicated-in-place internal viscous shear damper for machine structures and components |
EP0621936A4 (en) * | 1992-09-09 | 1996-01-10 | Massachusetts Inst Technology | Replicated-in-place internal viscous shear damper for machine structures and components. |
WO1995002131A1 (en) * | 1993-07-08 | 1995-01-19 | United Technologies Corporation | Split tubular elastomer damper |
WO1999006734A1 (en) * | 1997-08-04 | 1999-02-11 | Lord Corporation | Fluid and elastomer damper |
US6092795A (en) * | 1997-08-04 | 2000-07-25 | Lord Corporation | Fluid and elastomer damper |
FR2818717A1 (fr) | 2000-12-26 | 2002-06-28 | Eurocopter France | Dispositif de liaison elastique amortie et son procede de fabrication |
EP1514960A3 (de) * | 2003-09-10 | 2005-12-07 | Groz-Beckert KG | Vibrationsarmes Fachbildesystem |
US7032624B2 (en) | 2003-09-10 | 2006-04-25 | Groz-Beckert Kg | Low-vibration shedding system |
EP1655159A1 (en) * | 2004-11-03 | 2006-05-10 | C.R.F. Società Consortile per Azioni | Suspension system with longitudinal interconnection for a vehicle |
US7607892B2 (en) | 2005-09-21 | 2009-10-27 | Eurocopter | Rotorcraft rotor with blades hinged in flap and in lag |
FR2952150A1 (fr) * | 2009-11-02 | 2011-05-06 | Airbus Operations Sas | Bielle structurale comportant un mode filtrant des vibrations |
US8973885B2 (en) | 2009-11-02 | 2015-03-10 | Airbus Operations Sas | Structural rod incorporating a vibration filtration mode |
US20130099051A1 (en) * | 2010-06-14 | 2013-04-25 | Snecma | Turboshaft engine attached to a pylon of the fuselage of an aircraft by a failsafe suspension system |
US9067688B2 (en) * | 2010-06-14 | 2015-06-30 | Snecma | Turboshaft engine attached to a pylon of the fuselage of an aircraft by a failsafe suspension system |
EP2508764A1 (en) * | 2011-04-04 | 2012-10-10 | Bell Helicopter Textron Inc. | Self pumping and priming ahesive joint system |
CN102729580A (zh) * | 2011-04-04 | 2012-10-17 | 贝尔直升机泰克斯特龙公司 | 自泵和自装填的粘合剂接合系统 |
CN102729580B (zh) * | 2011-04-04 | 2015-09-09 | 贝尔直升机泰克斯特龙公司 | 自泵和自装填的粘合剂接合系统 |
US9382933B2 (en) | 2011-04-04 | 2016-07-05 | Textron Innovations Inc. | Self pumping and priming adhesive joint system |
US11472380B2 (en) * | 2019-10-02 | 2022-10-18 | Zf Active Safety Gmbh | Force input member for a brake actuating device |
US20220194636A1 (en) * | 2020-12-17 | 2022-06-23 | Maxar Space Llc | Passively damped end fittings and brackets |
IT202100001028A1 (it) * | 2021-01-21 | 2022-07-21 | Mecaer Aviation Group S P A | Asta smorzante per veicoli |
WO2022157709A1 (en) * | 2021-01-21 | 2022-07-28 | Mecaer Aviation Group S.P.A. | Damping rod for vehicles |
Also Published As
Publication number | Publication date |
---|---|
FR2677723B1 (US06559137-20030506-C00071.png) | 1995-02-17 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
CD | Change of name or company name | ||
TP | Transmission of property | ||
ST | Notification of lapse |
Effective date: 20110228 |