[go: up one dir, main page]

Barnard et al., 2001 - Google Patents

Development of a magnetic cam for the computer aided tap test system

Barnard et al., 2001

Document ID
11033332417802324127
Author
Barnard D
Peters J
Hsu D
Publication year
Publication venue
AIP Conference Proceedings

External Links

Snippet

A novel magnetic cam mechanism was developed for a computer aided tap test system. It makes use of the repulsion between opposing permanent magnets and provides a simple way for position-encoding the tap test data and producing “C-scan” like images of the local …
Continue reading at pubs.aip.org (other versions)

Classifications

    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01N—INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
    • G01N2203/00—Investigating strength properties of solid materials by application of mechanical stress
    • G01N2203/02—Details not specific for a particular testing method
    • G01N2203/026—Specifications of the specimen
    • G01N2203/0262—Shape of the specimen
    • G01N2203/0278—Thin specimens
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01N—INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
    • G01N2203/00—Investigating strength properties of solid materials by application of mechanical stress
    • G01N2203/0058—Kind of property studied
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01N—INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
    • G01N3/00—Investigating strength properties of solid materials by application of mechanical stress
    • 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49815—Disassembling
    • Y10T29/49822—Disassembling by applying force

Similar Documents

Publication Publication Date Title
EP2345881B1 (en) Crawling automated scanner for non-destructive inspection of aerospace structural elements
Baker et al. Advances in the bonded composite repair of metallic aircraft structure
Vasudevan et al. Fatigue damage analysis: Issues and challenges
Raut et al. A review of various techniques used for shaft failure analysis
Barnard et al. Development of a magnetic cam for the computer aided tap test system
CN108593473A (en) A kind of constant-temperature constant-humidity environment abrasion test case
Peters et al. A prototype tap test imaging system: Initial field test results
EP4350340A1 (en) Device for testing drive shafts and other bodies
Marušić et al. METHODS TO DETECT AND PREVENT FATIGUE IN AGEING AIRCRAFT STRUCTURES.
US20240110847A1 (en) Method for testing drive shafts and other bodies
Wells et al. Mechanisms of fatigue in the creep range
De Pauw Experimental research on the influence of palliatives in fretting fatigue
Gnanamoorthy et al. Fretting fatigue in AISI 1015 steel
Bangaru Early stage fatigue damage mechanisms in composite material used for wind turbine rotor blades
Hsu et al. Nondestructive evaluation of repairs on aircraft composite structures
Leis Fatigue life prediction of complex structures
Perry Jr Calculation of energy release rates for delaminations in composite materials using phase shifting moiré interferometry
Hahn et al. Fretting Corrosion in Airframe Riveted and Pinned Connections
Schwalbe et al. Damage tolerance: fracture mechanics in design
Chu et al. Detection of delamination in graphite/epoxy composite by electric potential method
Hsu et al. Development of fieldable systems for inspecting aircraft composite structures
Minnaar Experimental and numerical analyses of damage in laminate composites under low velocity impact loading
Shikhmanter et al. Fractography of CFRP composites damaged by impact and subsequently loaded statically to failure
Crawford et al. Damage tolerance analysis for rotorcraft, what the issues are
Haque et al. Fatigue damage in laminated composites