FR3004418B1 - SYSTEM AND METHOD FOR DYNAMIC AZIMUTAL BALANCING OF AIRCRAFT PROPELLER ROTOR - Google Patents

SYSTEM AND METHOD FOR DYNAMIC AZIMUTAL BALANCING OF AIRCRAFT PROPELLER ROTOR

Info

Publication number
FR3004418B1
FR3004418B1 FR1353440A FR1353440A FR3004418B1 FR 3004418 B1 FR3004418 B1 FR 3004418B1 FR 1353440 A FR1353440 A FR 1353440A FR 1353440 A FR1353440 A FR 1353440A FR 3004418 B1 FR3004418 B1 FR 3004418B1
Authority
FR
France
Prior art keywords
azimutal
balancing
dynamic
aircraft propeller
propeller rotor
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
FR1353440A
Other languages
French (fr)
Other versions
FR3004418A1 (en
Inventor
Sebastien Tajan
Adrien Fabre
Christophe Jacquemard
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.)
Safran Aircraft Engines SAS
Original Assignee
SNECMA 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 SNECMA SAS filed Critical SNECMA SAS
Priority to FR1353440A priority Critical patent/FR3004418B1/en
Publication of FR3004418A1 publication Critical patent/FR3004418A1/en
Application granted granted Critical
Publication of FR3004418B1 publication Critical patent/FR3004418B1/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

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
    • F16F15/00—Suppression of vibrations in systems; Means or arrangements for avoiding or reducing out-of-balance forces, e.g. due to motion
    • F16F15/32—Correcting- or balancing-weights or equivalent means for balancing rotating bodies, e.g. vehicle wheels
    • F16F15/322—Correcting- or balancing-weights or equivalent means for balancing rotating bodies, e.g. vehicle wheels the rotating body being a shaft
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C11/00—Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
    • B64C11/008—Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft characterised by vibration absorbing or balancing means
    • 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
    • F16F2230/00—Purpose; Design features
    • F16F2230/18—Control arrangements

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Acoustics & Sound (AREA)
  • Mechanical Engineering (AREA)
  • Testing Of Balance (AREA)
FR1353440A 2013-04-16 2013-04-16 SYSTEM AND METHOD FOR DYNAMIC AZIMUTAL BALANCING OF AIRCRAFT PROPELLER ROTOR Active FR3004418B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR1353440A FR3004418B1 (en) 2013-04-16 2013-04-16 SYSTEM AND METHOD FOR DYNAMIC AZIMUTAL BALANCING OF AIRCRAFT PROPELLER ROTOR

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1353440A FR3004418B1 (en) 2013-04-16 2013-04-16 SYSTEM AND METHOD FOR DYNAMIC AZIMUTAL BALANCING OF AIRCRAFT PROPELLER ROTOR

Publications (2)

Publication Number Publication Date
FR3004418A1 FR3004418A1 (en) 2014-10-17
FR3004418B1 true FR3004418B1 (en) 2016-10-28

Family

ID=48656155

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1353440A Active FR3004418B1 (en) 2013-04-16 2013-04-16 SYSTEM AND METHOD FOR DYNAMIC AZIMUTAL BALANCING OF AIRCRAFT PROPELLER ROTOR

Country Status (1)

Country Link
FR (1) FR3004418B1 (en)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104354135B (en) * 2014-10-29 2016-01-27 哈尔滨工业大学 Aero-engine turns stator and assembles/measure five degree of freedom adjustment localization method and device
FR3097268B1 (en) 2019-06-11 2022-07-08 Safran Aircraft Engines Dynamic balancing device for rotor
CN114112193B (en) * 2021-09-22 2023-10-17 核工业理化工程研究院 Dynamic balance weight prediction method for flexible rotor

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3830109A (en) * 1972-07-10 1974-08-20 G Litvinovich Device for dynamic balancing of rotors
US4117742A (en) * 1977-07-29 1978-10-03 Stein Philip C Permanent automatic rotor balancer for shafts operating above critical speed
US8403643B2 (en) * 2008-03-20 2013-03-26 Sikorsky Aircraft Corporation Dual frequency hub mounted vibration suppressor system
US8961140B2 (en) * 2009-10-14 2015-02-24 Lord Corporation Aircraft propeller balancing system
FR2977030B1 (en) * 2011-06-22 2013-07-12 Airbus Operations Sas BALANCING METHOD FOR PROPULSIVE SYSTEM WITH NON-CARINE COAXIAL CONTRAROTATIVE PROPELLERS

Also Published As

Publication number Publication date
FR3004418A1 (en) 2014-10-17

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