2020
DOI: 10.17814/mechanik.2020.11.18
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Manufacturing technology and strength properties of new composite joints

Abstract: The paper presents the concept, technology of manufacturing and assembly of a new metal-composite-metal joint. The presented joint can be used in many constructions, especially in lightweight supporting structures. The research of the strength properties of the analysed composite joints of load-bearing structures is also presented.

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(2 citation statements)
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“…The delamination ratio g is defined as the ratio of the maximum diameter L max of the circle drilled to produce the exit delamination to the diameter L o of the drilled hole, and the size of g directly reflects the tearing and delamination condition of the exit surface layer. The delamination ratio g is defined as equation (2).…”
Section: Analysis Of the Entrance And Exit Quality Of The Holementioning
confidence: 99%
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“…The delamination ratio g is defined as the ratio of the maximum diameter L max of the circle drilled to produce the exit delamination to the diameter L o of the drilled hole, and the size of g directly reflects the tearing and delamination condition of the exit surface layer. The delamination ratio g is defined as equation (2).…”
Section: Analysis Of the Entrance And Exit Quality Of The Holementioning
confidence: 99%
“…In the aerospace field, in order to meet the demand for lightweight, lightweight and high-strength Fiber Reinforced Plastic (FRP) is used in a large number of aircraft, and there is a growing trend. 1,2 The overall performance of the aircraft has been improved by the reduction of the weight of the fuselage through the use of fiberglass in important parts of the fuselage, hatches, electronic equipment, wings, and tail of the aircraft. 3,4 FRP is often required to undergo some mechanical machining, especially hole machining when assembled with other aerospace parts.…”
Section: Introductionmentioning
confidence: 99%