NO791554L - Fremgangsmaate og system for aa frembringe treghets-, konstruksjons-, og aerodynamiske data - Google Patents

Fremgangsmaate og system for aa frembringe treghets-, konstruksjons-, og aerodynamiske data

Info

Publication number: NO791554L
Authority: NO; Norway
Prior art keywords: construction; aerodynamic; structural; aircraft; data
Prior art date: 1978-05-10

Application number

NO791554A

Other languages

English (en)

Norwegian (no)

Inventor

Thomas Stewart Rhoades

Richard Errol Willes

Willie James Honea

Robert Anthony Golobic

Original Assignee

Res Analysis & Dev

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.)

1978-05-10

Filing date

1979-05-09

Publication date

1979-11-13

1979-05-09 Application filed by Res Analysis & Dev filed Critical Res Analysis & Dev

1979-11-13 Publication of NO791554L publication Critical patent/NO791554L/no

Links

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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
- G01M5/00—Investigating the elasticity of structures, e.g. deflection of bridges or air-craft wings
- G01M5/0041—Investigating the elasticity of structures, e.g. deflection of bridges or air-craft wings by determining deflection or stress
- G—PHYSICS
- G01—MEASURING; TESTING
- G01B—MEASURING LENGTH, THICKNESS OR SIMILAR LINEAR DIMENSIONS; MEASURING ANGLES; MEASURING AREAS; MEASURING IRREGULARITIES OF SURFACES OR CONTOURS
- G01B11/00—Measuring arrangements characterised by the use of optical techniques
- G01B11/16—Measuring arrangements characterised by the use of optical techniques for measuring the deformation in a solid, e.g. optical strain gauge
- G—PHYSICS
- G01—MEASURING; TESTING
- G01M—TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
- G01M5/00—Investigating the elasticity of structures, e.g. deflection of bridges or air-craft wings
- G01M5/0016—Investigating the elasticity of structures, e.g. deflection of bridges or air-craft wings of aircraft wings or blades
- G—PHYSICS
- G01—MEASURING; TESTING
- G01M—TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
- G01M5/00—Investigating the elasticity of structures, e.g. deflection of bridges or air-craft wings
- G01M5/0033—Investigating the elasticity of structures, e.g. deflection of bridges or air-craft wings by determining damage, crack or wear
- G—PHYSICS
- G01—MEASURING; TESTING
- G01M—TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
- G01M5/00—Investigating the elasticity of structures, e.g. deflection of bridges or air-craft wings
- G01M5/0066—Investigating the elasticity of structures, e.g. deflection of bridges or air-craft wings by exciting or detecting vibration or acceleration

Landscapes

Physics & Mathematics (AREA)
General Physics & Mathematics (AREA)
Engineering & Computer Science (AREA)
Aviation & Aerospace Engineering (AREA)
Length Measuring Devices By Optical Means (AREA)
Testing Of Engines (AREA)
Circuits Of Receivers In General (AREA)
Force Measurement Appropriate To Specific Purposes (AREA)
Navigation (AREA)

NO791554A 1978-05-10 1979-05-09 Fremgangsmaate og system for aa frembringe treghets-, konstruksjons-, og aerodynamiske data NO791554L (no)

Applications Claiming Priority (1)

Application Number	Priority Date	Filing Date	Title
US90454978A	1978-05-10	1978-05-10

Publications (1)

Publication Number	Publication Date
NO791554L true NO791554L (no)	1979-11-13

Family

ID=25419343

Family Applications (1)

Application Number	Title	Priority Date	Filing Date
NO791554A NO791554L (no)	1978-05-10	1979-05-09	Fremgangsmaate og system for aa frembringe treghets-, konstruksjons-, og aerodynamiske data

Country Status (14)

Country	Link
JP (1)	JPS54151299A (fr)
AU (1)	AU4688079A (fr)
BE (1)	BE876171A (fr)
BR (1)	BR7902765A (fr)
DE (1)	DE2918886A1 (fr)
FR (1)	FR2425627A1 (fr)
GB (1)	GB2021261B (fr)
IL (1)	IL57235A (fr)
IN (1)	IN151971B (fr)
IT (1)	IT1112859B (fr)
NL (1)	NL7903628A (fr)
NO (1)	NO791554L (fr)
NZ (1)	NZ190374A (fr)
SE (1)	SE7904034L (fr)

Families Citing this family (18)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
DE3070977D1 (en) *	1980-05-22	1985-09-19	Acec	Method and apparatus for detecting misalignment of mechanical shafts
EP0046647A3 (fr) *	1980-08-21	1982-03-17	Idc Group Limited	Dispositif de mesure digital
US4409842A (en) *	1981-05-18	1983-10-18	Scott Science & Technology, Inc.	Structural information detector
FR2584489B1 (fr) *	1985-07-08	1990-06-08	Bertin & Cie	Dispositif pour controler la geometrie d'une structure mecanique.
DE3620888A1 (de) *	1986-06-21	1988-01-14	Messerschmitt Boelkow Blohm	Betriebslastenueberwachungseinrichtung fuer luftfahrzeuge
DE9015495U1 (de) *	1990-11-12	1992-01-02	Technischer Überwachungs-Verein Bayern e.V., 8000 München	Meßwertaufnehmer zum Erfassen physikalischer Kenngrößen eines Personen- und/oder Lastenaufzugs
US6289289B1 (en)	1998-12-10	2001-09-11	Honeywell International Inc.	Aircraft structural fatigue monitor
GB0204932D0 (en) *	2002-03-02	2002-04-17	Campbell Robert	Analysis system for plant real-time integrity assessment
US20060004499A1 (en) *	2004-06-30	2006-01-05	Angela Trego	Structural health management architecture using sensor technology
USD523145S1 (en) *	2004-10-13	2006-06-13	Astra Tech Ab	Impression coping for dental implant prosthetic
US8180750B2 (en)	2007-03-14	2012-05-15	The Boeing Company	Support model integration system and method
FR2916041B1 (fr) *	2007-05-11	2009-06-26	Airbus France Sas	Procede et dispositif de suivi de deformation d'une piece metallique, notamment pour le redressage d'une piece metallique
US8106753B2 (en)	2008-08-27	2012-01-31	The Boeing Company	Determining and providing vehicle conditions and capabilities
US8392045B2 (en)	2008-09-05	2013-03-05	The Boeing Company	System and methods for aircraft preflight inspection
FR2942536A1 (fr) *	2009-02-25	2010-08-27	Commissariat Energie Atomique	Procede d'estimation de la vitesse de deplacement d'un aeronef
CN114735231B (zh) *	2021-12-30	2024-06-18	中国人民解放军93184部队	一种飞行数据采集装置
CN120558140B (zh) *	2025-08-04	2025-11-04	山西省交通建设工程质量检测中心（有限公司）	基于无人机与深度学习的桥梁裂缝智能检测系统
CN120927306B (zh) *	2025-10-10	2026-01-30	中国航发湖南动力机械研究所	涡轴发动机的运行状态监视方法及系统、设备、介质

1979
- 1979-05-04 NZ NZ190374A patent/NZ190374A/xx unknown
- 1979-05-05 IN IN301/DEL/79A patent/IN151971B/en unknown
- 1979-05-08 IL IL57235A patent/IL57235A/xx unknown
- 1979-05-08 BR BR7902765A patent/BR7902765A/pt unknown
- 1979-05-08 SE SE7904034A patent/SE7904034L/xx not_active Application Discontinuation
- 1979-05-09 GB GB7916036A patent/GB2021261B/en not_active Expired
- 1979-05-09 NO NO791554A patent/NO791554L/no unknown
- 1979-05-09 NL NL7903628A patent/NL7903628A/xx not_active Application Discontinuation
- 1979-05-09 IT IT22501/79A patent/IT1112859B/it active
- 1979-05-09 AU AU46880/79A patent/AU4688079A/en not_active Abandoned
- 1979-05-10 FR FR7911928A patent/FR2425627A1/fr active Granted
- 1979-05-10 BE BE0/195094A patent/BE876171A/fr unknown
- 1979-05-10 JP JP5758679A patent/JPS54151299A/ja active Pending
- 1979-05-10 DE DE19792918886 patent/DE2918886A1/de not_active Withdrawn

Also Published As

Publication number	Publication date
NZ190374A (en)	1982-08-17
FR2425627A1 (fr)	1979-12-07
BE876171A (fr)	1979-11-12
GB2021261A (en)	1979-11-28
IT1112859B (it)	1986-01-20
IN151971B (fr)	1983-09-17
JPS54151299A (en)	1979-11-28
IT7922501A0 (it)	1979-05-09
BR7902765A (pt)	1979-11-27
DE2918886A1 (de)	1979-12-20
IL57235A (en)	1983-07-31
NL7903628A (nl)	1979-11-13
GB2021261B (en)	1983-01-12
SE7904034L (sv)	1979-11-11
FR2425627B3 (fr)	1982-03-26
AU4688079A (en)	1979-11-15

Publication	Publication Date	Title
NO791554L (no)	1979-11-13	Fremgangsmaate og system for aa frembringe treghets-, konstruksjons-, og aerodynamiske data
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Ranaudo et al.	1989	Determination of longitudinal aerodynamic derivatives using flight data from an icing research aircraft
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