WO2002016900A3 - Flutter exciter - Google Patents

Flutter exciter Download PDF

Info

Publication number
WO2002016900A3
WO2002016900A3 PCT/IB2001/001497 IB0101497W WO0216900A3 WO 2002016900 A3 WO2002016900 A3 WO 2002016900A3 IB 0101497 W IB0101497 W IB 0101497W WO 0216900 A3 WO0216900 A3 WO 0216900A3
Authority
WO
WIPO (PCT)
Prior art keywords
impellers
flutter
flutter exciter
rotating
force
Prior art date
Application number
PCT/IB2001/001497
Other languages
French (fr)
Other versions
WO2002016900A2 (en
Inventor
Zyl Louwrens Hermias Van
Original Assignee
Csir
Zyl Louwrens Hermias Van
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 Csir, Zyl Louwrens Hermias Van filed Critical Csir
Priority to AU2001277652A priority Critical patent/AU2001277652A1/en
Publication of WO2002016900A2 publication Critical patent/WO2002016900A2/en
Publication of WO2002016900A3 publication Critical patent/WO2002016900A3/en

Links

Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01MTESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
    • G01M7/00Vibration-testing of structures; Shock-testing of structures

Landscapes

  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Wind Motors (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

A flutter exciter includes first and second impellers rotatably connected together by coupling means and rotatable about a common axis in opposite directions, each impeller having at least one vane so that fluid flowing over the vanes causes the impellers to rotate and each to generate a rotating force, the resultant of the rotating forces being an oscillating substantially rectilinear excitation force.
PCT/IB2001/001497 2000-08-21 2001-08-20 Flutter exciter WO2002016900A2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
AU2001277652A AU2001277652A1 (en) 2000-08-21 2001-08-20 Flutter exciter

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
ZA2000/4283 2000-08-21
ZA200004283 2000-08-21

Publications (2)

Publication Number Publication Date
WO2002016900A2 WO2002016900A2 (en) 2002-02-28
WO2002016900A3 true WO2002016900A3 (en) 2002-05-02

Family

ID=25588873

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/IB2001/001497 WO2002016900A2 (en) 2000-08-21 2001-08-20 Flutter exciter

Country Status (2)

Country Link
AU (1) AU2001277652A1 (en)
WO (1) WO2002016900A2 (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103604350B (en) * 2013-11-28 2016-06-22 中国神华能源股份有限公司 The measurement auxiliary device of exciter rotor sway degree and measurement apparatus
CN106441780B (en) * 2016-09-06 2020-11-06 中国航空工业集团公司沈阳飞机设计研究所 Pulse excitation method for flutter flight test of scaling model

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3552192A (en) * 1968-02-16 1971-01-05 Lockheed Aircraft Corp Rotary excitation device
EP0299436A2 (en) * 1987-07-16 1989-01-18 Dynamic Engineering Inc. Flutter Exciter
RU2144657C1 (en) * 1996-02-08 2000-01-20 Летно-исследовательский институт им.М.М.Громова Aerodynamic exciter of vibration of aircraft wing

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3552192A (en) * 1968-02-16 1971-01-05 Lockheed Aircraft Corp Rotary excitation device
EP0299436A2 (en) * 1987-07-16 1989-01-18 Dynamic Engineering Inc. Flutter Exciter
RU2144657C1 (en) * 1996-02-08 2000-01-20 Летно-исследовательский институт им.М.М.Громова Aerodynamic exciter of vibration of aircraft wing

Also Published As

Publication number Publication date
AU2001277652A1 (en) 2002-03-04
WO2002016900A2 (en) 2002-02-28

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