ES8702592A1 - Elastomeric high torque constant velocity joint - Google Patents

Elastomeric high torque constant velocity joint

Info

Publication number
ES8702592A1
ES8702592A1 ES544336A ES544336A ES8702592A1 ES 8702592 A1 ES8702592 A1 ES 8702592A1 ES 544336 A ES544336 A ES 544336A ES 544336 A ES544336 A ES 544336A ES 8702592 A1 ES8702592 A1 ES 8702592A1
Authority
ES
Spain
Prior art keywords
constant velocity
high torque
velocity joint
bearing
spherical
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.)
Expired
Application number
ES544336A
Other languages
Spanish (es)
Other versions
ES544336A0 (en
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.)
Raytheon Technologies Corp
Original Assignee
United Technologies Corp
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
Priority claimed from US06/622,801 external-priority patent/US4575358A/en
Application filed by United Technologies Corp filed Critical United Technologies Corp
Publication of ES8702592A1 publication Critical patent/ES8702592A1/en
Publication of ES544336A0 publication Critical patent/ES544336A0/en
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C27/00Rotorcraft; Rotors peculiar thereto
    • B64C27/32Rotors
    • B64C27/35Rotors having elastomeric joints
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C27/00Rotorcraft; Rotors peculiar thereto
    • B64C27/32Rotors
    • B64C27/37Rotors having articulated joints
    • B64C27/41Rotors having articulated joints with flapping hinge or universal joint, common to the blades
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16FSPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
    • F16F1/00Springs
    • F16F1/36Springs made of rubber or other material having high internal friction, e.g. thermoplastic elastomers
    • F16F1/38Springs 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
    • F16F1/393Springs 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

Abstract

A part spherical laminated elastomeric bearing has a non- circular latitudinal cross-section to accommodate high torque loads in elastomer bending rather than in shear. The spherical profile of the bearing accommodates tilt primarily in shear. Both inwardly and outwardly extending lobes, or spines, are disclosed. The spherical, lobed bearing is useful for a constant velocity joint especially in a helicopter gimbal rotor system.
ES544336A 1984-06-20 1985-06-19 Elastomeric high torque constant velocity joint Expired ES8702592A1 (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US62280984A 1984-06-20 1984-06-20
US62259184A 1984-06-20 1984-06-20
US06/622,801 US4575358A (en) 1984-06-20 1984-06-20 Accommodating axial load in an elastomeric high torque, constant velocity joint

Publications (2)

Publication Number Publication Date
ES8702592A1 true ES8702592A1 (en) 1987-01-01
ES544336A0 ES544336A0 (en) 1987-01-01

Family

ID=27417320

Family Applications (1)

Application Number Title Priority Date Filing Date
ES544336A Expired ES8702592A1 (en) 1984-06-20 1985-06-19 Elastomeric high torque constant velocity joint

Country Status (10)

Country Link
AU (1) AU577866B2 (en)
BE (1) BE902685A (en)
BR (1) BR8502917A (en)
DE (1) DE3521877C2 (en)
DK (1) DK276485A (en)
ES (1) ES8702592A1 (en)
FR (1) FR2566489B1 (en)
GB (1) GB2160619B (en)
IL (1) IL75565A (en)
IT (1) IT1185049B (en)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5083725A (en) * 1990-10-11 1992-01-28 United Technologies Corporation Elastomeric swashplate configuration for helicopters
US5482406A (en) * 1993-04-15 1996-01-09 Continental Emsco Company Variable spring rate compression element and riser tensioner system using the same
US5641248A (en) * 1993-04-15 1997-06-24 Continental Emsco Company Variable spring rate compression element and riser tensioner system using the same
US5628586A (en) * 1995-06-23 1997-05-13 Continental Emsco Company Elastomeric riser tensioner system
US6296444B1 (en) * 1999-10-01 2001-10-02 Bell Helicopter Textron Inc. Prop rotor hub
US7341283B2 (en) 2004-01-29 2008-03-11 Oil States Industries, Inc. High temperature flexible pipe joint
EP3038909B1 (en) * 2013-08-28 2019-05-08 Sikorsky Aircraft Corporation Rotor hub for rotary wing aircraft
US10214284B2 (en) 2013-09-30 2019-02-26 Sikorsky Aircraft Corporation Pitch bearing
FR3059296B1 (en) * 2016-11-29 2019-03-29 Airbus Helicopters ELASTOMERIC ASSEMBLY, LAMINATED BUFFER, ROTOR WITH SUCH A ROCKET, AND AIRCRAFT
CN113195929B (en) 2018-10-31 2023-09-19 Fm能源有限责任两合公司 Elastic hinge with torsion stop and use thereof in a shock absorber

Family Cites Families (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1488740A (en) * 1922-12-23 1924-04-01 Timothy C Dobbins Resilinet universal joint for power transmission
GB492517A (en) * 1936-01-23 1938-09-21 Max Goldschmidt Improvements in and relating to springs comprising rubber and metal parts
US2363469A (en) * 1942-09-01 1944-11-21 Metalastik Ltd Flexible coupling, flexible mounting, and the like
US2948129A (en) * 1958-06-23 1960-08-09 Schwitzer Corp Elliptical vibration damper
GB919351A (en) * 1958-06-23 1963-02-27 Schwitzer Corp An improved rotatable assembly
BE588408A (en) * 1959-03-13 1960-09-08 Glaenzer Spicer Sa Universal flexible coupling for transmissions
FR1255940A (en) * 1959-03-13 1961-03-17 Glaenzerspicer Flexible coupling for transmissions
US3524332A (en) * 1968-09-06 1970-08-18 Rex Chainbelt Inc Elastomer coupling
GB1351138A (en) * 1970-04-07 1974-04-24 Dunlop Holdings Ltd Springs
SE7500297L (en) * 1975-01-13 1976-07-14 Skf Nova Ab VIBRATION DAMPING COUPLING
DE2643166A1 (en) * 1975-11-03 1977-05-12 United Technologies Corp ELASTOMER BEARING FOR HELICOPTER ROTOR
GB1507381A (en) * 1976-07-16 1978-04-12 Oswell J Patient support apparatus
DE2706479C2 (en) * 1977-02-16 1984-05-30 Maschinenfabrik Stromag Gmbh, 4750 Unna Torsionally flexible coupling
CA1096188A (en) * 1977-07-07 1981-02-24 Jerome Greene Flexible coupling
US4208889A (en) * 1978-08-30 1980-06-24 Barry Wright Corporation Constant velocity, torsionally rigid, flexible coupling
US4323332A (en) * 1979-12-21 1982-04-06 United Technologies Corporation Hingeless helicopter rotor with elastic gimbal hub
US4427340A (en) * 1982-06-24 1984-01-24 Bell Helicopter Textron Inc. Soft inplane bearingless helicopter rotor

Also Published As

Publication number Publication date
DE3521877C2 (en) 1996-07-11
DK276485D0 (en) 1985-06-19
BR8502917A (en) 1986-03-04
GB8514510D0 (en) 1985-07-10
DK276485A (en) 1985-12-21
AU577866B2 (en) 1988-10-06
DE3521877A1 (en) 1986-01-02
IT1185049B (en) 1987-10-28
GB2160619A (en) 1985-12-24
FR2566489B1 (en) 1990-04-06
ES544336A0 (en) 1987-01-01
FR2566489A1 (en) 1985-12-27
IL75565A (en) 1989-12-15
GB2160619B (en) 1987-10-14
AU4379485A (en) 1986-01-02
BE902685A (en) 1985-10-16
IT8521200A0 (en) 1985-06-19

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