FR2082274A5 - Ultracentrifuge rotor - hub spider and wall assembly of high rigidity to weight ratio - Google Patents

Ultracentrifuge rotor - hub spider and wall assembly of high rigidity to weight ratio

Info

Publication number
FR2082274A5
FR2082274A5 FR7008394A FR7008394A FR2082274A5 FR 2082274 A5 FR2082274 A5 FR 2082274A5 FR 7008394 A FR7008394 A FR 7008394A FR 7008394 A FR7008394 A FR 7008394A FR 2082274 A5 FR2082274 A5 FR 2082274A5
Authority
FR
France
Prior art keywords
spider
weight ratio
hub
high rigidity
wall assembly
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
FR7008394A
Other languages
English (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.)
Airbus Group SAS
Original Assignee
Airbus Group 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 Group SAS filed Critical Airbus Group SAS
Priority to FR7008394A priority Critical patent/FR2082274A5/fr
Application granted granted Critical
Publication of FR2082274A5 publication Critical patent/FR2082274A5/fr
Expired legal-status Critical Current

Links

Classifications

    • 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
    • F16F15/00Suppression of vibrations in systems; Means or arrangements for avoiding or reducing out-of-balance forces, e.g. due to motion
    • F16F15/30Flywheels
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B04CENTRIFUGAL APPARATUS OR MACHINES FOR CARRYING-OUT PHYSICAL OR CHEMICAL PROCESSES
    • B04BCENTRIFUGES
    • B04B7/00Elements of centrifuges
    • B04B7/08Rotary bowls
    • B04B7/085Rotary bowls fibre- or metal-reinforced

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Acoustics & Sound (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Iron Core Of Rotating Electric Machines (AREA)
FR7008394A 1970-03-09 1970-03-09 Ultracentrifuge rotor - hub spider and wall assembly of high rigidity to weight ratio Expired FR2082274A5 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR7008394A FR2082274A5 (en) 1970-03-09 1970-03-09 Ultracentrifuge rotor - hub spider and wall assembly of high rigidity to weight ratio

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR7008394A FR2082274A5 (en) 1970-03-09 1970-03-09 Ultracentrifuge rotor - hub spider and wall assembly of high rigidity to weight ratio

Publications (1)

Publication Number Publication Date
FR2082274A5 true FR2082274A5 (en) 1971-12-10

Family

ID=9051965

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7008394A Expired FR2082274A5 (en) 1970-03-09 1970-03-09 Ultracentrifuge rotor - hub spider and wall assembly of high rigidity to weight ratio

Country Status (1)

Country Link
FR (1) FR2082274A5 (fr)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3020497A1 (de) * 1979-05-29 1980-12-04 Aerospatiale Subzirkularer rotor
EP0063074A1 (fr) * 1981-04-14 1982-10-20 AEROSPATIALE Société Nationale Industrielle Rotor à haute vitesse de rotation notamment pour volant d'inertie
US5545118A (en) * 1989-08-02 1996-08-13 Romanauskas; William A. Tension band centrifuge rotor
US5562584A (en) * 1989-08-02 1996-10-08 E. I. Du Pont De Nemours And Company Tension band centrifuge rotor

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3020497A1 (de) * 1979-05-29 1980-12-04 Aerospatiale Subzirkularer rotor
EP0063074A1 (fr) * 1981-04-14 1982-10-20 AEROSPATIALE Société Nationale Industrielle Rotor à haute vitesse de rotation notamment pour volant d'inertie
US5545118A (en) * 1989-08-02 1996-08-13 Romanauskas; William A. Tension band centrifuge rotor
US5562584A (en) * 1989-08-02 1996-10-08 E. I. Du Pont De Nemours And Company Tension band centrifuge rotor

Similar Documents

Publication Publication Date Title
GB1534393A (en) Flywheels
GB1325853A (en) Supersonic centrifugal compressor
GB1235448A (en) Resilient mounting arrangement
FR2082274A5 (en) Ultracentrifuge rotor - hub spider and wall assembly of high rigidity to weight ratio
GB907144A (en) Improvements relating to high speed ball or roller bearings
DE3266293D1 (en) High speed rotor especially for flywheel
GB1417132A (en) Turbine wheel
GB914240A (en) Improvements in or relating to torsional vibration dampers
GB1473259A (en) Torque converter
US2441239A (en) Blower apparatus
GB975892A (en) Turbine rotors
GB1215623A (en) A method of making a torque converter and converters obtained by this method
US2325530A (en) Fluid driven gyroscope
GB1027843A (en) An axial-flow turbine
GB1351567A (en) Damping device
FR2470879A1 (fr) Ventilateur monobloc a encastrer
GB1055113A (en) Foettinger torque converter
GB1401810A (en) Vibration damper with a hermetically closed damping chamber
GB1081649A (en) Turbine wheel
GB839622A (en) Improvements in centrifuges
GB955560A (en) Improvements in rotor hubs for fans
GB915070A (en) Rotor blade spacer
GB850004A (en) Hub structure for an aeronautical propeller
SU375413A1 (ru) Радиальный газодинамический подшипник
MOORE et al. Performance of a single-stage axial-flow transonic compressor stage with a blade tip solidity of 1. 7(Performance tests of single stage, axial flow, transonic compressor over stable operating range at rotative speeds from fifty to one hundred percent of design speed)

Legal Events

Date Code Title Description
ST Notification of lapse