Three-dimensional tube geometry control for rotary draw tube bending part 2: Statistical tube tolerance analysis and adaptive bend correction

Huazhou Lou, Kim A. Stelson

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Abstract

The control of each individual bend and overall process is presented in part 1 of the paper. In part 2 of the paper, statistical methods are used to analyze and improve 3-D tube bending accuracy. The relationship between bending process error and tube geometry error is obtained with Monte Carlo simulation. For the same tube tolerance requirement, the required process tolerance varies in a large range based on tube geometry. Among the three bending errors: bend angle, bend plane and distance between bends, bend angle error has the largest influence on tube error. For a tube with multiple bends, the overall tube geometry error can be minimized by intentionally modify the nominal values of the bends to be made based on the errors in the existing bends. The required modification of the bending commands is calculated with an adaptive bend correction algorithm.

Original languageEnglish (US)
Title of host publicationManufacturing Engineering
PublisherAmerican Society of Mechanical Engineers (ASME)
Pages621-627
Number of pages7
ISBN (Electronic)9780791819166
DOIs
StatePublished - 2000
EventASME 2000 International Mechanical Engineering Congress and Exposition, IMECE 2000 - Orlando, United States
Duration: Nov 5 2000Nov 10 2000

Publication series

NameASME International Mechanical Engineering Congress and Exposition, Proceedings (IMECE)
Volume2000-X

Conference

ConferenceASME 2000 International Mechanical Engineering Congress and Exposition, IMECE 2000
Country/TerritoryUnited States
CityOrlando
Period11/5/0011/10/00

Bibliographical note

Funding Information:
The authors appreciate the funding and technical assistance of GE Aircraft Engines, Elano and Eagle Precision Inc. (now Eagle Eaton-Leonard). The authors gratefully acknowledge the following individuals for their'help on this research: Mike Umney and Steve Mitchell of GE Aircraft Engines, Steve Creech of Elano, Tim Blurton-Jones, Qian Gao and Jim Sabine of Eagle Eaton-Leonard.

Publisher Copyright:
Copyright © 2000 by ASME.

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