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2-Amino-2-(hydroxymethyl)-1,3-propanediol (TRIS) and ethylene-diaminetetraacetic acid (EDTA) are key components of biological buffers and are frequently used as DNA stabilizers in irradiation studies. Such surface or liquid phase studies are done with the aim to understand the fundamental mechanisms of DNA radiation damage and to improve cancer radiotherapy. When ionizing radiation is used, abundant secondary electrons are formed during the irradiation process, which are able to attach to the molecular compounds present on the surface. In the present study we experimentally investigate low energy electron attachment to TRIS and methyliminodiacetic acid (MIDA), an analogue of EDTA, supported by quantum chemical calculations. The most prominent dissociation channel for TRIS is through hydroperoxyl radical formation, whereas the dissociation of MIDA results in the formation of formic and acetic acid. These compounds are well-known to cause DNA modifications, like strand breaks. The present results indicate that buffer compounds may not have an exclusive protecting effect on DNA as suggested previously.
To increase the competitiveness of jacket substructures compared to monopiles a changeover from an individual towards a serial jacket production based on automated manufactured tubular joints combined with standardized pipes has to be achieved. Therefore, this paper addresses fatigue tests of automatically welded tubular X-joints focusing on the location of the technical fatigue crack. The detected location of the technical crack is compared to numerical investigations predicting the most fatigue prone notch considering the structural stress approach as well as the notch stress approach. Besides, the welding process of the automated manufactured tubular X-joints is presented.
To increase the competitiveness of jacket substructures compared to monopiles a changeover from an individual towards a serial jacket production based on automated manufactured tubular joints com-bined with standardized pipes has to be achieved. Therefore, this paper addresses fatigue tests of automatical-ly welded tubular X-joints focusing on the location of the technical fatigue crack. For this X-joint, the detect-ed location of the technical crack is then compared to numerical investigations predicting the most fatigue prone notch considering the structural stress approach as well as the notch stress approach. Additionally, the fatigue prone hot spot according to both approaches is compared for a typical offshore jacket double-K-joint to emphasize the significance of the presented outcomes for the existing offshore structures. Besides, the welding process of the automated manufactured tubular X-joints is presented.
To increase the competitiveness of jacket substructures compared to monopiles a changeover from an individual towards a serial jacket production based on automated manufactured tubular joints combined with standardized pipes has to be achieved. Therefore, this paper ad-dresses the welding process of automated manufactured tubular X-joints. Additionally, fatigue tests of the automatically welded tubular joints are presented focusing on the location of the technical fatigue crack. The detected location of the technical crack is compared to numerical investigations predicting the most fatigue prone notch con-sidering the structural stress approach as well as the notch stress ap-proach.
To increase the competitiveness of jacket substructures compared to monopiles a changeover from an individual towards a serial jacket production based on automated manufactured tubular joints combined with standardized pipes has to be achieved. Therefore, this paper addresses fatigue tests of automatically welded tubular X-joints focusing on the location of the technical fatigue crack. The detected location of the technical crack is compared to numerical investigations predicting the most fatigue prone notch considering the structural stress approach as well as the notch stress approach. Besides, the welding process of the automated manufactured tubular X-joints is presented.
The development within the offshore wind sector towards more powerful turbines combined with increasing water depth for new wind parks is challenging both the designer as well as the manufacturer of bottom fixed support structures. Besides XL-monopiles, the market developed an innovative and economic jacket support structure which is based on automatically manufactured tubular joints combined with standardized pipes. Besides the improvements for a serial manufacturing process the automatically welded tubular joints show a great potential in terms of fatigue resistance e.g. due to a smooth weld geometry without sharp notches. However, these benefits are not considered yet within the fatigue design process of automatically manufactured jacket substructures according to current standards due to the lack of suitable S-N curves. Therefore, 32 axial fatigue tests on single and double-sided automatically welded tubular X-joints have been performed to determine a new hot spot stress related S-N curve. Based on these constant amplitude fatigue tests a new S-N curve equal to a FAT 126 curve was computed which implicitly includes the benefits of the automatically welding procedure.
Die Entwicklung in der Offshore-Windenergie hin zu größeren, leistungsstärkeren An-lagentypen sowie die zeitgleich zunehmenden Wassertiefen der projektierten Wind-parks stellt u. a. Designer und Fertiger der Gründungsstrukturen von Windenergiean-lagen vor wachsende Herausforderungen. Neben dem Gründungskonzept der XL-Monopiles rückt wegen der Kombination aus dem vergleichsweise geringen Materialverbrauch bei gleichzeitig hoher Steifigkeit, auch die Jacketgründung in den Fokus. Der Fertigungsaufwand der Jackets ist verglichen mit Monopiles groß; kann jedoch durch die Nutzung von Standardrohren mit automatisiert gefertigten Jacketknoten reduziert werden.
Vor diesem Hintergrund beschreibt der vorliegende Forschungsbericht den Fertigungs-prozess zum automatisierten Schweißen von X-förmigen Hohlprofilknoten für Jacket-Gründungsstrukturen von Offshore-Windenergieanlagen. Ein weiteres wesentliches Ziel dieses Vorhabens war die konsequente Digitalisierung der schweißtechnischen Fertigungskette während der automatisierten Schweißung der X-Knoten. Die so ge-speicherten Prozessparameter können zum einen als Grundlage einer Qualitätskon-trolle dienen, zum anderen ermöglichen sie eine vollständige Nachverfolgbarkeit der automatisiert gefertigten Rohrknoten.
Der zweite maßgebend in diesem Bericht behandelte Aspekt umfasst die Quantifizie-rung der Einflüsse aus Fertigungsautomatisierung und Innenschweißen auf die Ermü-dungsfestigkeit der Hohlprofilknoten auf Basis serieller Ermüdungsversuche. Dazu wurden im Projekt zwei Serien mit jeweils 16 Schwingversuchen an ein- und doppel-seitig automatisiert geschweißten X-Knoten durchgeführt und entsprechende Struktur-spannungswöhlerlinien für die automatisiert gefertigten X-Knoten bestimmt.
Die Ergebnisse dieser Ermüdungsversuche werden abschließend in numerischen Untersuchungen auf Basis der Strukturspannungs- und des Kerbspannungskonzeptes gegenübergestellt, um die Prognosefähigkeit beider Konzepte für die ermüdungs-kritischen Bereiche des X-Knotens bewerten zu können.
Durch die im Forschungsvorhaben durchgeführten schweißtechnischen, experimen-tellen und numerischen Analysen konnte das Potential automatisiert gefertigter Rohr-knoten hinsichtlich Reproduzierbarkeit und Ermüdungsverhalten quantifiziert werden. Zusätzlich konnte der Einfluss der inneren Schweißnaht auf die Ermüdungsfestigkeit bewertet werden.
To increase the competitiveness of jacket substructures compared to monopiles a changeover from an individual towards a serial jacket production based on automated manufactured tubular joints combined with standardized pipes has to be achieved. Therefore, this paper ad-dresses the welding process of automated manufactured tubular X-joints. Additionally, fatigue tests of the automatically welded tubular joints are presented focusing on the location of the technical fatigue crack. The detected location of the technical crack is compared to numerical investigations predicting the most fatigue prone notch considering the structural stress approach as well as the notch stress approach.
To increase the competitiveness of jacket substructures compared to monopiles a changeover from an individual towards a serial jacket production based on automated manufactured tubular joints combined with standardized pipes has to be achieved. Therefore, this paper addresses fatigue tests of automatically welded tubular X-joints focusing on the location of the technical fatigue crack. The detected location of the technical crack is compared to numerical investigations predicting the most fatigue prone notch considering the structural stress approach as well as the notch stress approach. Besides, the welding process of the automated manufactured tubular X-joints is presented.
To increase the competitiveness of jacket substructures compared to monopiles a changeover from an individual towards a serial jacket production based on automated manufactured tubular joints com-bined with standardized pipes has to be achieved. Therefore, this paper addresses fatigue tests of automatical-ly welded tubular X-joints focusing on the location of the technical fatigue crack. For this X-joint, the detect-ed location of the technical crack is then compared to numerical investigations predicting the most fatigue prone notch considering the structural stress approach as well as the notch stress approach. Additionally, the fatigue prone hot spot according to both approaches is compared for a typical offshore jacket double-K-joint to emphasize the significance of the presented outcomes for the existing offshore structures. Besides, the welding process of the automated manufactured tubular X-joints is presented.