FR1404239A - Rotating mass balancing device - Google Patents

Rotating mass balancing device

Info

Publication number
FR1404239A
FR1404239A FR985073A FR985073A FR1404239A FR 1404239 A FR1404239 A FR 1404239A FR 985073 A FR985073 A FR 985073A FR 985073 A FR985073 A FR 985073A FR 1404239 A FR1404239 A FR 1404239A
Authority
FR
France
Prior art keywords
balancing device
rotating mass
mass balancing
rotating
mass
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
FR985073A
Other languages
French (fr)
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.)
Waldrich H A GmbH
HA Waldrich GmbH
Original Assignee
Waldrich H A GmbH
HA Waldrich GmbH
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 Waldrich H A GmbH, HA Waldrich GmbH filed Critical Waldrich H A GmbH
Priority to FR985073A priority Critical patent/FR1404239A/en
Application granted granted Critical
Publication of FR1404239A publication Critical patent/FR1404239A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B24—GRINDING; POLISHING
    • B24B—MACHINES, DEVICES, OR PROCESSES FOR GRINDING OR POLISHING; DRESSING OR CONDITIONING OF ABRADING SURFACES; FEEDING OF GRINDING, POLISHING, OR LAPPING AGENTS
    • B24B41/00—Component parts such as frames, beds, carriages, headstocks
    • B24B41/04—Headstocks; Working-spindles; Features relating thereto
    • B24B41/042—Balancing mechanisms
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01M—TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
    • G01M1/00—Testing static or dynamic balance of machines or structures
    • G01M1/30—Compensating imbalance
    • G01M1/36—Compensating imbalance by adjusting position of masses built-in the body to be tested

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
FR985073A 1963-08-13 1964-08-13 Rotating mass balancing device Expired FR1404239A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR985073A FR1404239A (en) 1963-08-13 1964-08-13 Rotating mass balancing device

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DEW0035082 1963-08-13
FR985073A FR1404239A (en) 1963-08-13 1964-08-13 Rotating mass balancing device

Publications (1)

Publication Number Publication Date
FR1404239A true FR1404239A (en) 1965-06-25

Family

ID=26002613

Family Applications (1)

Application Number Title Priority Date Filing Date
FR985073A Expired FR1404239A (en) 1963-08-13 1964-08-13 Rotating mass balancing device

Country Status (1)

Country Link
FR (1) FR1404239A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2559901A1 (en) * 1984-02-22 1985-08-23 Snecma DEVICE AND TOOLING FOR CORRECTING TURBOMACHINE ROTOR BOTTOM AND METHOD FOR IMPLEMENTING THE SAME

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2559901A1 (en) * 1984-02-22 1985-08-23 Snecma DEVICE AND TOOLING FOR CORRECTING TURBOMACHINE ROTOR BOTTOM AND METHOD FOR IMPLEMENTING THE SAME
EP0153887A1 (en) * 1984-02-22 1985-09-04 Societe Nationale D'etude Et De Construction De Moteurs D'aviation, "S.N.E.C.M.A." Balancing device and equipment for a turbine rotor and method of operating
US4667532A (en) * 1984-02-22 1987-05-26 Societe Nationale D'etude Et De Construction De Moteurs D'aviation-"S.N.E.C.M.A." Method and apparatus for correcting the imbalance of a turbojet engine rotor

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