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    Experimental and Analytical Study of Aerospace Spiral Bevel Gear Tooth Fillet Stresses

    Source: Journal of Mechanical Design:;1999:;volume( 121 ):;issue: 004::page 565
    Author:
    R. F. Handschuh
    ,
    G. D. Bibel
    DOI: 10.1115/1.2829500
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: An aerospace-quality spiral bevel gearset was analytically and experimentally rolled through mesh to investigate tooth bending stress. A nonlinear finite element model utilized multiple teeth from the pinion and gear to simulate three-dimensional multitooth contact. The results were compared to those obtained experimentally with strain gages. A total of five strain gages, mounted in the root/fillet region of three teeth, were used. Effects of changing speed and load were measured. Tests were conducted from static (slow roll) to 14,400 rpm at power levels up to 537 kW (720 hp).
    keyword(s): Stress , Aerospace industry , Gear teeth , Strain gages , Gears , Finite element model AND Bending (Stress) ,
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      Experimental and Analytical Study of Aerospace Spiral Bevel Gear Tooth Fillet Stresses

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/122560
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    • Journal of Mechanical Design

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    contributor authorR. F. Handschuh
    contributor authorG. D. Bibel
    date accessioned2017-05-09T00:00:25Z
    date available2017-05-09T00:00:25Z
    date copyrightDecember, 1999
    date issued1999
    identifier issn1050-0472
    identifier otherJMDEDB-27665#565_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/122560
    description abstractAn aerospace-quality spiral bevel gearset was analytically and experimentally rolled through mesh to investigate tooth bending stress. A nonlinear finite element model utilized multiple teeth from the pinion and gear to simulate three-dimensional multitooth contact. The results were compared to those obtained experimentally with strain gages. A total of five strain gages, mounted in the root/fillet region of three teeth, were used. Effects of changing speed and load were measured. Tests were conducted from static (slow roll) to 14,400 rpm at power levels up to 537 kW (720 hp).
    publisherThe American Society of Mechanical Engineers (ASME)
    titleExperimental and Analytical Study of Aerospace Spiral Bevel Gear Tooth Fillet Stresses
    typeJournal Paper
    journal volume121
    journal issue4
    journal titleJournal of Mechanical Design
    identifier doi10.1115/1.2829500
    journal fristpage565
    journal lastpage572
    identifier eissn1528-9001
    keywordsStress
    keywordsAerospace industry
    keywordsGear teeth
    keywordsStrain gages
    keywordsGears
    keywordsFinite element model AND Bending (Stress)
    treeJournal of Mechanical Design:;1999:;volume( 121 ):;issue: 004
    contenttypeFulltext
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