GB2267470B - Method and apparatus for in-flight shake testing of an aircraft fuselage - Google Patents

Method and apparatus for in-flight shake testing of an aircraft fuselage

Info

Publication number
GB2267470B
GB2267470B GB9311080A GB9311080A GB2267470B GB 2267470 B GB2267470 B GB 2267470B GB 9311080 A GB9311080 A GB 9311080A GB 9311080 A GB9311080 A GB 9311080A GB 2267470 B GB2267470 B GB 2267470B
Authority
GB
United Kingdom
Prior art keywords
aircraft fuselage
shake testing
flight
flight shake
testing
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 - Lifetime
Application number
GB9311080A
Other versions
GB2267470A (en
GB9311080D0 (en
Inventor
Alan Edward Staple
Daniel Murray Wells
Andrew Leslie Jordan
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.)
AgustaWestland Ltd
Original Assignee
Westland Helicopters Ltd
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 claimed from GB929211719A external-priority patent/GB9211719D0/en
Application filed by Westland Helicopters Ltd filed Critical Westland Helicopters Ltd
Priority to GB9311080A priority Critical patent/GB2267470B/en
Publication of GB9311080D0 publication Critical patent/GB9311080D0/en
Publication of GB2267470A publication Critical patent/GB2267470A/en
Application granted granted Critical
Publication of GB2267470B publication Critical patent/GB2267470B/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01M—TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
    • G01M7/00—Vibration-testing of structures; Shock-testing of structures

Landscapes

  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Testing Of Devices, Machine Parts, Or Other Structures Thereof (AREA)
GB9311080A 1992-06-03 1993-05-28 Method and apparatus for in-flight shake testing of an aircraft fuselage Expired - Lifetime GB2267470B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB9311080A GB2267470B (en) 1992-06-03 1993-05-28 Method and apparatus for in-flight shake testing of an aircraft fuselage

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB929211719A GB9211719D0 (en) 1992-06-03 1992-06-03 Method & apparatus for in-flight shake testing of an aircraft fuselage
GB9311080A GB2267470B (en) 1992-06-03 1993-05-28 Method and apparatus for in-flight shake testing of an aircraft fuselage

Publications (3)

Publication Number Publication Date
GB9311080D0 GB9311080D0 (en) 1993-07-14
GB2267470A GB2267470A (en) 1993-12-08
GB2267470B true GB2267470B (en) 1995-12-13

Family

ID=26300981

Family Applications (1)

Application Number Title Priority Date Filing Date
GB9311080A Expired - Lifetime GB2267470B (en) 1992-06-03 1993-05-28 Method and apparatus for in-flight shake testing of an aircraft fuselage

Country Status (1)

Country Link
GB (1) GB2267470B (en)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB0007619D0 (en) 2000-03-29 2000-05-17 British Aerospace Aircraft control system
WO2017060558A1 (en) * 2015-10-08 2017-04-13 Wärtsilä Finland Oy Method and arrangement for testing earthquake resistance of an engine
CN114184879B (en) * 2021-11-08 2024-01-23 陕西千山航空电子有限责任公司 Abnormal frequency point monitoring method for helicopter vibration data

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3074385A (en) * 1958-05-15 1963-01-22 Gen Dynamics Corp Dynamic testing apparatus
GB2160840A (en) * 1984-06-29 1986-01-02 Westland Plc Method and apparatus for reducing vibration of a helicopter fuselage
GB2197473A (en) * 1986-10-31 1988-05-18 Helitune Limited Method and apparatus for vibration testing equipment

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3074385A (en) * 1958-05-15 1963-01-22 Gen Dynamics Corp Dynamic testing apparatus
GB2160840A (en) * 1984-06-29 1986-01-02 Westland Plc Method and apparatus for reducing vibration of a helicopter fuselage
GB2197473A (en) * 1986-10-31 1988-05-18 Helitune Limited Method and apparatus for vibration testing equipment

Also Published As

Publication number Publication date
GB2267470A (en) 1993-12-08
GB9311080D0 (en) 1993-07-14

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Legal Events

Date Code Title Description
PE20 Patent expired after termination of 20 years

Expiry date: 20130527