GB942386A - Vibration resistant aircraft structures - Google Patents

Vibration resistant aircraft structures

Info

Publication number
GB942386A
GB942386A GB2230/60A GB223060A GB942386A GB 942386 A GB942386 A GB 942386A GB 2230/60 A GB2230/60 A GB 2230/60A GB 223060 A GB223060 A GB 223060A GB 942386 A GB942386 A GB 942386A
Authority
GB
United Kingdom
Prior art keywords
friction
aircraft
struts
rods
vibratable member
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
GB2230/60A
Other languages
English (en)
Inventor
David Williams
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.)
SECR AVIATION
Minister of Aviation
Original Assignee
SECR AVIATION
Minister of Aviation
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 to NL260320D priority Critical patent/NL260320A/xx
Application filed by SECR AVIATION, Minister of Aviation filed Critical SECR AVIATION
Priority to GB2230/60A priority patent/GB942386A/en
Priority to CH71161A priority patent/CH396522A/de
Priority to FR850356A priority patent/FR1284109A/fr
Publication of GB942386A publication Critical patent/GB942386A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
    • B64C1/066—Interior liners
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/40—Sound or heat insulation, e.g. using insulation blankets
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12—Blades
    • F01D5/26—Antivibration means not restricted to blade form or construction or to blade-to-blade connections or to the use of particular materials
    • 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
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/40—Weight reduction
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Vibration Prevention Devices (AREA)
  • Vibration Dampers (AREA)
GB2230/60A 1960-01-21 1960-01-21 Vibration resistant aircraft structures Expired GB942386A (en)

Priority Applications (4)

Application Number Priority Date Filing Date Title
NL260320D NL260320A (cg-RX-API-DMAC7.html) 1960-01-21
GB2230/60A GB942386A (en) 1960-01-21 1960-01-21 Vibration resistant aircraft structures
CH71161A CH396522A (de) 1960-01-21 1961-01-20 Anordnung zur Dämpfung von Flugzeugrumpfschwingungen
FR850356A FR1284109A (fr) 1960-01-21 1961-01-20 Structure résistant aux vibrations

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB2230/60A GB942386A (en) 1960-01-21 1960-01-21 Vibration resistant aircraft structures

Publications (1)

Publication Number Publication Date
GB942386A true GB942386A (en) 1963-11-20

Family

ID=9735887

Family Applications (1)

Application Number Title Priority Date Filing Date
GB2230/60A Expired GB942386A (en) 1960-01-21 1960-01-21 Vibration resistant aircraft structures

Country Status (3)

Country Link
FR (1) FR1284109A (cg-RX-API-DMAC7.html)
GB (1) GB942386A (cg-RX-API-DMAC7.html)
NL (1) NL260320A (cg-RX-API-DMAC7.html)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6669447B2 (en) 2001-01-11 2003-12-30 Rolls-Royce Plc Turbomachine blade
CN111252235A (zh) * 2020-01-20 2020-06-09 西北工业大学 基于流固耦合效应的被动式副翼嗡鸣增稳器
CN117404424A (zh) * 2023-10-20 2024-01-16 江苏科技大学 一种用于水上平台的减振机构及其使用方法

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB996729A (en) * 1963-12-16 1965-06-30 Rolls Royce Improvements relating to turbines and compressors
DE2225925C2 (de) * 1972-05-27 1985-02-28 Teldix Gmbh, 6900 Heidelberg Schwungrad, insbesondere zur Stabilisierung von Raumfahrzeugen

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6669447B2 (en) 2001-01-11 2003-12-30 Rolls-Royce Plc Turbomachine blade
CN111252235A (zh) * 2020-01-20 2020-06-09 西北工业大学 基于流固耦合效应的被动式副翼嗡鸣增稳器
CN117404424A (zh) * 2023-10-20 2024-01-16 江苏科技大学 一种用于水上平台的减振机构及其使用方法

Also Published As

Publication number Publication date
NL260320A (cg-RX-API-DMAC7.html)
FR1284109A (fr) 1962-02-09

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