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Erschienen in: Strength of Materials 3/2014

01.05.2014

Probabilistic Model of Multiple-Site Fatigue Damage of Riveting in Airframes

verfasst von: S. R. Ignatovich

Erschienen in: Strength of Materials | Ausgabe 3/2014

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Abstract

The probabilistic model of multiple-site damage of riveting in airframes is based on the statistical description of kinetics of the three fatigue fracture factors: time to crack initiation near the rivet hole, dimensional nonuniformity of flaws, and coalescence of counterpropagating cracks from neighboring holes. The probabilistic measure of these factors is used to determine time-dependent performance characteristics of a rivet joint: no-failure operation function and lifetime distribution function. The limiting state of the structure comes if at least one of the ligaments between the holes is fractured.

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Literatur
1.
Zurück zum Zitat J. Schijve, “Multiple-site damage in aircraft fuselage structures,” Fatigue Fract. Eng. Mater. Struct., 18, No. 3, 329–344 (1995).CrossRef J. Schijve, “Multiple-site damage in aircraft fuselage structures,” Fatigue Fract. Eng. Mater. Struct., 18, No. 3, 329–344 (1995).CrossRef
2.
Zurück zum Zitat W. R. Hendricks, “The Aloha airlines accident – a new era for aging aircraft,” in: S. N. Atluri, S. G. Sampath, and P. Tong (Eds.), Structural Integrity of Aging Airplanes, Springer-Verlag, Berlin–Heidelberg (1991), pp. 153–166. W. R. Hendricks, “The Aloha airlines accident – a new era for aging aircraft,” in: S. N. Atluri, S. G. Sampath, and P. Tong (Eds.), Structural Integrity of Aging Airplanes, Springer-Verlag, Berlin–Heidelberg (1991), pp. 153–166.
3.
Zurück zum Zitat Method of Determining the Consistency with AP 25.571. Provision of Safety of the Construction as Regards the Strength during Long-Term Operation [in Russian], Mintrans, Moscow (1996). Method of Determining the Consistency with AP 25.571. Provision of Safety of the Construction as Regards the Strength during Long-Term Operation [in Russian], Mintrans, Moscow (1996).
4.
Zurück zum Zitat Recommendations for Regulatory Action to Prevent Widespread Fatigue Damage in the Commercial Airplane Fleet: a Report of the AAWG (Final Report), Airworthiness Assurance Working Group (1999). Recommendations for Regulatory Action to Prevent Widespread Fatigue Damage in the Commercial Airplane Fleet: a Report of the AAWG (Final Report), Airworthiness Assurance Working Group (1999).
5.
Zurück zum Zitat C. Boller, “Structural health management of ageing aircraft and other infrastructure,” in: Structural Health Monitoring, Institute of Smart Structures and Systems (ISSS), Bangalore, India (2002), pp. 1–59. C. Boller, “Structural health management of ageing aircraft and other infrastructure,” in: Structural Health Monitoring, Institute of Smart Structures and Systems (ISSS), Bangalore, India (2002), pp. 1–59.
6.
Zurück zum Zitat A. Rambalakos and G. Deodatis, “Non-periodic inspection of aging aircraft structures,” in: Proc. 9th Joint FAA/DoD/NASA Conf. on Aging Aircraft (March 6–9, 2006, Atlanta, USA, GA) (2006), pp. 1–18. A. Rambalakos and G. Deodatis, “Non-periodic inspection of aging aircraft structures,” in: Proc. 9th Joint FAA/DoD/NASA Conf. on Aging Aircraft (March 6–9, 2006, Atlanta, USA, GA) (2006), pp. 1–18.
7.
Zurück zum Zitat V. Pavelko and J. Timoshtchenko, “Model of the multi-site fatigue damage in the thin-walled structure,” in: Proc. 5th Int. Conf. “Reliability and Statistics in Transportation and Communication” (Oct. 13–14, 2005, Riga, Latvia), Part 2, Riga (2005), pp. 327 –334. V. Pavelko and J. Timoshtchenko, “Model of the multi-site fatigue damage in the thin-walled structure,” in: Proc. 5th Int. Conf. “Reliability and Statistics in Transportation and Communication” (Oct. 13–14, 2005, Riga, Latvia), Part 2, Riga (2005), pp. 327 –334.
8.
Zurück zum Zitat H. L. Wang and A. F. Grandt, “Monte Carlo analysis of widespread fatigue damage in lap joints,” in: A. F. Grandt, Jr., T. N. Farris, and B. H. Hillberry (Prep.), Analysis of Widespread Fatigue Damage in Aerospace Structures (Final Report for Air Force Office of Scientific Research), Purdue University (1999), p. 25. H. L. Wang and A. F. Grandt, “Monte Carlo analysis of widespread fatigue damage in lap joints,” in: A. F. Grandt, Jr., T. N. Farris, and B. H. Hillberry (Prep.), Analysis of Widespread Fatigue Damage in Aerospace Structures (Final Report for Air Force Office of Scientific Research), Purdue University (1999), p. 25.
9.
Zurück zum Zitat C. Proppe, “Probabilistic analysis of multi-site damage in aircraft fuselages,” Comp. Mech., 30, No. 4, 323–329 (2003). C. Proppe, “Probabilistic analysis of multi-site damage in aircraft fuselages,” Comp. Mech., 30, No. 4, 323–329 (2003).
10.
Zurück zum Zitat A. N. Garcia and P. E. Irving, “Lap joint MSD assessment using a probabilistic model,” in: Proc. 11th Int. Conf. on Fracture “Aeronautics & Aerospace” (March 20–25, 2005, Turin, Italy) (2005), pp. 74–79. A. N. Garcia and P. E. Irving, “Lap joint MSD assessment using a probabilistic model,” in: Proc. 11th Int. Conf. on Fracture “Aeronautics & Aerospace” (March 20–25, 2005, Turin, Italy) (2005), pp. 74–79.
11.
Zurück zum Zitat G. Cavallini and R. Lazzeri, “A probabilistic approach to fatigue risk assessment in aerospace components,” Eng. Fract. Mech., 74, Issue 18, 2964–2970 (2007).CrossRef G. Cavallini and R. Lazzeri, “A probabilistic approach to fatigue risk assessment in aerospace components,” Eng. Fract. Mech., 74, Issue 18, 2964–2970 (2007).CrossRef
12.
Zurück zum Zitat U. G. Goranson, Damage Tolerance. Facts and Fiction, Keynote Presentation in Int. Conf. on Damage Tolerance of Aircraft Structure (Sept. 25, 2007, Delft, The Netherlands). U. G. Goranson, Damage Tolerance. Facts and Fiction, Keynote Presentation in Int. Conf. on Damage Tolerance of Aircraft Structure (Sept. 25, 2007, Delft, The Netherlands).
13.
Zurück zum Zitat J. H. Kim, G. Zi, S.-N. Van, et al., “Fatigue life prediction of multiple-site damage based on probabilistic equivalent initial flaw model,” Struct. Eng. Mech., 38, No. 4, 443–457 (2011). J. H. Kim, G. Zi, S.-N. Van, et al., “Fatigue life prediction of multiple-site damage based on probabilistic equivalent initial flaw model,” Struct. Eng. Mech., 38, No. 4, 443–457 (2011).
14.
Zurück zum Zitat Handbook for Damage Tolerant Design, Section 3.2: Equivalent Initial Quality (2010), pp. 3.2.1–3.2.11. Handbook for Damage Tolerant Design, Section 3.2: Equivalent Initial Quality (2010), pp. 3.2.1–3.2.11.
15.
Zurück zum Zitat Durability Methods Development, Technical Report AFFDL-TR-79-3118, Vol. V: J. N. Yang, S. D. Manning, and W. R. Garver (Eds.), Durability Analysis Methodology Development, Structural and Design Department, GDC, Fort Worth, Texas, US (1979). Durability Methods Development, Technical Report AFFDL-TR-79-3118, Vol. V: J. N. Yang, S. D. Manning, and W. R. Garver (Eds.), Durability Analysis Methodology Development, Structural and Design Department, GDC, Fort Worth, Texas, US (1979).
16.
Zurück zum Zitat J. N. Yang, “Statistical estimation of economic life for aircraft structures,” J. Aircraft, 17, No. 7, 528–535 (1980).CrossRef J. N. Yang, “Statistical estimation of economic life for aircraft structures,” J. Aircraft, 17, No. 7, 528–535 (1980).CrossRef
17.
Zurück zum Zitat Y. C. Tong, Literature Review on Aircraft Structural Risk and Reliability Analysis, Technical Report DSTO-TR-1110, Aeronautical and Maritime Research Laboratory (2001). Y. C. Tong, Literature Review on Aircraft Structural Risk and Reliability Analysis, Technical Report DSTO-TR-1110, Aeronautical and Maritime Research Laboratory (2001).
18.
Zurück zum Zitat Joint Service Specification Guide for Aircraft Structures (JSSG-2006), Department of Defense of USA (1998). Joint Service Specification Guide for Aircraft Structures (JSSG-2006), Department of Defense of USA (1998).
19.
Zurück zum Zitat Handbook for Damage Tolerant Design, Section 1.3: Summary of Damage Tolerance Design Guidelines (2010), pp. 1.3.1–1.3.35. Handbook for Damage Tolerant Design, Section 1.3: Summary of Damage Tolerance Design Guidelines (2010), pp. 1.3.1–1.3.35.
20.
Zurück zum Zitat P. White, Review of Methods and Approaches for the Structural Risk Assessment of Aircraft, Technical Report DSTO-TR-1916, Defense Science and Technology Organisation (2006). P. White, Review of Methods and Approaches for the Structural Risk Assessment of Aircraft, Technical Report DSTO-TR-1916, Defense Science and Technology Organisation (2006).
21.
Zurück zum Zitat S. R. Ignatovich, A. G. Kucher, A. S. Yakushenko, and A. V. Bashta, “Modeling of coalescence of dispersed surface cracks. Part 1. Probabilistic model for crack coalescence,” Strength Mater., 36, No. 2, 125–133 (2004).CrossRef S. R. Ignatovich, A. G. Kucher, A. S. Yakushenko, and A. V. Bashta, “Modeling of coalescence of dispersed surface cracks. Part 1. Probabilistic model for crack coalescence,” Strength Mater., 36, No. 2, 125–133 (2004).CrossRef
Metadaten
Titel
Probabilistic Model of Multiple-Site Fatigue Damage of Riveting in Airframes
verfasst von
S. R. Ignatovich
Publikationsdatum
01.05.2014
Verlag
Springer US
Erschienen in
Strength of Materials / Ausgabe 3/2014
Print ISSN: 0039-2316
Elektronische ISSN: 1573-9325
DOI
https://doi.org/10.1007/s11223-014-9555-5

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