FR3059296B1 - Ensemble elastomerique, butee lamifiee, rotor muni d'une telle butee, et aeronef - Google Patents

Ensemble elastomerique, butee lamifiee, rotor muni d'une telle butee, et aeronef Download PDF

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Publication number
FR3059296B1
FR3059296B1 FR1601688A FR1601688A FR3059296B1 FR 3059296 B1 FR3059296 B1 FR 3059296B1 FR 1601688 A FR1601688 A FR 1601688A FR 1601688 A FR1601688 A FR 1601688A FR 3059296 B1 FR3059296 B1 FR 3059296B1
Authority
FR
France
Prior art keywords
main
rocket
aircraft
rotor
axis
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
Application number
FR1601688A
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English (en)
Other versions
FR3059296A1 (fr
Inventor
Mathias Fournier
Jean Romain Bihel
Guillaume Fiocchi
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Airbus Helicopters SAS
Original Assignee
Airbus Helicopters SAS
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Airbus Helicopters SAS filed Critical Airbus Helicopters SAS
Priority to FR1601688A priority Critical patent/FR3059296B1/fr
Priority to CA2984667A priority patent/CA2984667C/fr
Publication of FR3059296A1 publication Critical patent/FR3059296A1/fr
Application granted granted Critical
Publication of FR3059296B1 publication Critical patent/FR3059296B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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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
    • 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
    • F16F1/393—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 with spherical or conical sleeves
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/32—Rotors
    • B64C27/35—Rotors having elastomeric joints
    • 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
    • F16F1/40—Springs made of rubber or other material having high internal friction, e.g. thermoplastic elastomers consisting of a stack of similar elements separated by non-elastic intermediate layers
    • F16F1/41—Springs made of rubber or other material having high internal friction, e.g. thermoplastic elastomers consisting of a stack of similar elements separated by non-elastic intermediate layers the spring consisting of generally conically arranged elements

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Laminated Bodies (AREA)

Abstract

La présente invention concerne un ensemble lamifié (20) comprenant un empilement de couches principales (25) et de couches secondaires (30), chaque couche principale (25) comportant un matériau souple et chaque couche secondaire comportant un matériau rigide, ledit empilement s'étendant en envergure selon l'axe d'extension (AX) d'une première couche principale (26) jusqu'à une dernière couche principale (27). Au moins une desdites couches principales (25) a une forme de coiffe de sphère, ladite coiffe de sphère représentant une partie d'une paroi sphérique tronquée par un tube à section non circulaire, ladite section s'étendant selon un premier axe sur une longueur et un selon un deuxième axe perpendiculaire au premier axe sur une largeur, ladite longueur étant supérieure à ladite largeur.
FR1601688A 2016-11-29 2016-11-29 Ensemble elastomerique, butee lamifiee, rotor muni d'une telle butee, et aeronef Active FR3059296B1 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
FR1601688A FR3059296B1 (fr) 2016-11-29 2016-11-29 Ensemble elastomerique, butee lamifiee, rotor muni d'une telle butee, et aeronef
CA2984667A CA2984667C (fr) 2016-11-29 2017-11-02 Ensemble elastomerique, butee lamifiee, rotor muni d'une telle butee, etaeronef

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1601688A FR3059296B1 (fr) 2016-11-29 2016-11-29 Ensemble elastomerique, butee lamifiee, rotor muni d'une telle butee, et aeronef
FR1601688 2016-11-29

Publications (2)

Publication Number Publication Date
FR3059296A1 FR3059296A1 (fr) 2018-06-01
FR3059296B1 true FR3059296B1 (fr) 2019-03-29

Family

ID=57796394

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1601688A Active FR3059296B1 (fr) 2016-11-29 2016-11-29 Ensemble elastomerique, butee lamifiee, rotor muni d'une telle butee, et aeronef

Country Status (2)

Country Link
CA (1) CA2984667C (fr)
FR (1) FR3059296B1 (fr)

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2948129A (en) * 1958-06-23 1960-08-09 Schwitzer Corp Elliptical vibration damper
GB2160619B (en) * 1984-06-20 1987-10-14 United Technologies Corp Elastomeric high torque constant velocity joint
US4895354A (en) * 1985-05-13 1990-01-23 United Technologies Corporation Equalizing stress distribution in each laminate of an asymmetrically loaded elastomeric bearing

Also Published As

Publication number Publication date
CA2984667C (fr) 2019-12-31
FR3059296A1 (fr) 2018-06-01
CA2984667A1 (fr) 2018-01-09

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