Method of accurate countersinking and rivet shaving

Todd Rudberg; Scott Smith; Andy Smith

doi:10.4271/2001-01-2569

Method of accurate countersinking and rivet shaving

Todd Rudberg, Scott Smith, Andy Smith

Research output: Contribution to journal › Conference article › peer-review

1 Scopus citations

Abstract

Wing skin riveting and bolting requires the surface to be flush to +/-.025mm(.001") to produce an acceptable finish. Using the method described in this paper, automated wing riveting technology and panel assembly techniques can achieve better shave height and countersink accuracies than have previously been possible in production.

Original language	English
Journal	SAE Technical Papers
DOIs	https://doi.org/10.4271/2001-01-2569
State	Published - 2001
Externally published	Yes
Event	SAE Aerospace Automated Fastening Conference - 2001 Aerospace Congress - Seattle, WA, United States Duration: Sep 10 2001 → Sep 14 2001

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10.4271/2001-01-2569

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title = "Method of accurate countersinking and rivet shaving",

abstract = "Wing skin riveting and bolting requires the surface to be flush to +/-.025mm(.001{"}) to produce an acceptable finish. Using the method described in this paper, automated wing riveting technology and panel assembly techniques can achieve better shave height and countersink accuracies than have previously been possible in production.",

author = "Todd Rudberg and Scott Smith and Andy Smith",

year = "2001",

doi = "10.4271/2001-01-2569",

language = "English",

journal = "SAE Technical Papers",

issn = "0148-7191",

publisher = "SAE International",

note = "SAE Aerospace Automated Fastening Conference - 2001 Aerospace Congress ; Conference date: 10-09-2001 Through 14-09-2001",

}

TY - JOUR

T1 - Method of accurate countersinking and rivet shaving

AU - Rudberg, Todd

AU - Smith, Scott

AU - Smith, Andy

PY - 2001

Y1 - 2001

N2 - Wing skin riveting and bolting requires the surface to be flush to +/-.025mm(.001") to produce an acceptable finish. Using the method described in this paper, automated wing riveting technology and panel assembly techniques can achieve better shave height and countersink accuracies than have previously been possible in production.

AB - Wing skin riveting and bolting requires the surface to be flush to +/-.025mm(.001") to produce an acceptable finish. Using the method described in this paper, automated wing riveting technology and panel assembly techniques can achieve better shave height and countersink accuracies than have previously been possible in production.

UR - http://www.scopus.com/inward/record.url?scp=85072481834&partnerID=8YFLogxK

U2 - 10.4271/2001-01-2569

DO - 10.4271/2001-01-2569

M3 - Conference article

AN - SCOPUS:85072481834

SN - 0148-7191

JO - SAE Technical Papers

JF - SAE Technical Papers

T2 - SAE Aerospace Automated Fastening Conference - 2001 Aerospace Congress

Y2 - 10 September 2001 through 14 September 2001

ER -

Method of accurate countersinking and rivet shaving

Abstract

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