DE3935925A1 - Passiver flatterdaempfer - Google Patents

Passiver flatterdaempfer

Info

Publication number
DE3935925A1
DE3935925A1 DE19893935925 DE3935925A DE3935925A1 DE 3935925 A1 DE3935925 A1 DE 3935925A1 DE 19893935925 DE19893935925 DE 19893935925 DE 3935925 A DE3935925 A DE 3935925A DE 3935925 A1 DE3935925 A1 DE 3935925A1
Authority
DE
Germany
Prior art keywords
wing
flutter
damper
mass
inertia
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.)
Granted
Application number
DE19893935925
Other languages
German (de)
English (en)
Other versions
DE3935925C2 (cs
Inventor
Gerhard Dipl Ing Dr Loebert
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 Defence and Space GmbH
Original Assignee
Messerschmitt Bolkow Blohm AG
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 Messerschmitt Bolkow Blohm AG filed Critical Messerschmitt Bolkow Blohm AG
Priority to DE19893935925 priority Critical patent/DE3935925A1/de
Publication of DE3935925A1 publication Critical patent/DE3935925A1/de
Application granted granted Critical
Publication of DE3935925C2 publication Critical patent/DE3935925C2/de
Granted legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
    • B64C13/02—Initiating means
    • B64C13/16—Initiating means actuated automatically, e.g. responsive to gust detectors
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/30—Balancing hinged surfaces, e.g. dynamically
    • 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
    • F16F7/00—Vibration-dampers; Shock-absorbers
    • F16F7/10—Vibration-dampers; Shock-absorbers using inertia effect
    • F16F7/1022—Vibration-dampers; Shock-absorbers using inertia effect the linear oscillation movement being converted into a rotational movement of the inertia member, e.g. using a pivoted mass
    • 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
    • F16F7/00—Vibration-dampers; Shock-absorbers
    • F16F7/10—Vibration-dampers; Shock-absorbers using inertia effect
    • F16F7/104—Vibration-dampers; Shock-absorbers using inertia effect the inertia member being resiliently mounted

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Automation & Control Theory (AREA)
  • Toys (AREA)
  • Vibration Prevention Devices (AREA)
DE19893935925 1989-10-27 1989-10-27 Passiver flatterdaempfer Granted DE3935925A1 (de)

Priority Applications (1)

Application Number Priority Date Filing Date Title
DE19893935925 DE3935925A1 (de) 1989-10-27 1989-10-27 Passiver flatterdaempfer

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19893935925 DE3935925A1 (de) 1989-10-27 1989-10-27 Passiver flatterdaempfer

Publications (2)

Publication Number Publication Date
DE3935925A1 true DE3935925A1 (de) 1991-05-16
DE3935925C2 DE3935925C2 (cs) 1993-02-11

Family

ID=6392421

Family Applications (1)

Application Number Title Priority Date Filing Date
DE19893935925 Granted DE3935925A1 (de) 1989-10-27 1989-10-27 Passiver flatterdaempfer

Country Status (1)

Country Link
DE (1) DE3935925A1 (cs)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6607161B1 (en) * 1999-09-14 2003-08-19 Eurocopter Convertible aircraft with tilting rotors
FR2902163A1 (fr) * 2006-06-13 2007-12-14 Peugeot Citroen Automobiles Sa Vehicule automobile comportant un batteur cooperant avec une poutre
FR2951794A1 (fr) * 2009-10-22 2011-04-29 Peugeot Citroen Automobiles Sa Systeme absorbeur des vibrations de la caisse d'un vehicule.

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US11814162B2 (en) * 2020-06-18 2023-11-14 Textron Innovations Inc. Rotatable winglets for a rotary wing aircraft

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2056730B2 (de) * 1969-11-27 1978-11-30 Societe Nationale Industrielle Aerospatiale S.A., Paris Vorrichtung zur Verbesserung der Längsstabilität eines Hubschraubers

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2056730B2 (de) * 1969-11-27 1978-11-30 Societe Nationale Industrielle Aerospatiale S.A., Paris Vorrichtung zur Verbesserung der Längsstabilität eines Hubschraubers

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6607161B1 (en) * 1999-09-14 2003-08-19 Eurocopter Convertible aircraft with tilting rotors
FR2902163A1 (fr) * 2006-06-13 2007-12-14 Peugeot Citroen Automobiles Sa Vehicule automobile comportant un batteur cooperant avec une poutre
FR2951794A1 (fr) * 2009-10-22 2011-04-29 Peugeot Citroen Automobiles Sa Systeme absorbeur des vibrations de la caisse d'un vehicule.

Also Published As

Publication number Publication date
DE3935925C2 (cs) 1993-02-11

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Legal Events

Date Code Title Description
OP8 Request for examination as to paragraph 44 patent law
D2 Grant after examination
8327 Change in the person/name/address of the patent owner

Owner name: DEUTSCHE AEROSPACE AG, 8000 MUENCHEN, DE

8364 No opposition during term of opposition
8320 Willingness to grant licenses declared (paragraph 23)
8327 Change in the person/name/address of the patent owner

Owner name: DAIMLER-BENZ AEROSPACE AKTIENGESELLSCHAFT, 80804 M

8339 Ceased/non-payment of the annual fee