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Sørensen, Jesper Kirk - One of the best experts on this subject based on the ideXlab platform.

  • Reduction of Oscillations in Hydraulically Actuated Knuckle Boom Cranes
    Universitet i Agder University of Agder, 2016
    Co-Authors: Sørensen, Jesper Kirk
    Abstract:

    Doktorgradsavhandling ved Universitetet i Agder, Institutt for ingeniørvitenskap, 2016A knuckle boom crane is characterized by being a versatile machine that during operation experiences large load variations caused by the changes in position and payload. Common uses are as a mobile loader crane mounted on trucks and in offshore applications. Since their introduction the use of counterbalance valves (CBV) have been the de facto standard on load-carrying hydraulically actuated applications like the knuckle boom crane. It offers a simple and practical solution to one of the issues of mobile cranes: Controlling the load safely when lowering. By law (e.g. European Standard) the hydraulic circuit of load-carrying applications is required to contain a load holding protection device. The classical way of actuating such a crane is to use a circuit containing a pressure compensator valve and a directional control valve (DCV) in series with a CBV. This circuit is referred to as the base circuit. It is well known that this combination of valve components tends to introduce instability in the base circuit. This is Mainly a problem when the controlled actuator is subjected to a negative load, because this will require the CBV to throttle the return flow. The instability presents itself as pressure oscillations in the hydraulic circuit which cause the mechanical structure to oscillate. The consequence of the oscillations is a decreased accuracy of the boom motion which create a safety risk, reduces productivity and introduces an undesirable extra fatigue load. The objective of this project was to investigate the oscillations created in the hydraulic circuit of knuckle boom cranes and reduce their severity. The effort has Mainly been split in two: First, was looked into existing solutions with the focus on the ones not requiring control systems to function. This was done with reliability and robustness in mind. The investigation identified the pressure control valve (PCV) as the best commercially available solution. The use of a PCV to control the inlet flow in crane applications was rather uncharted territory. The valve, a DCV with a pressure control Spool manufactured by Danfoss, has been investigated both theoretically and experimentally. A linear stability analysis has been performed with the Routh-Hurwitz stability criterion. This analysis of the valve used together with a hydraulically actuated experimental setup indicates that the combination is stable in all situations. The use of the pressure control Spool in the DCV is a simple and robust solution to the stability problem of the base circuit. Not related to the PCV’s ability to reduce the oscillations the use of it in knuckle boom cranes, however, comes with certain drawbacks. The drawbacks include a load dependent dead band and a load dependent inlet flow. In order to achieve similar behavior as the normal pressure compensated DCV a closed loop control system is required. These issues are addressed in this project, where control schemes are proposed to handle them. In the second part the perspective of the search was broadened to include solutions using control systems. This has lead to the development of a novel, patent pending, concept that significantly reduces the oscillations of the base circuit. It introduces a secondary circuit where a low-pass filtered value of the load pressure is generated and fed back to the compensator of the flow supply valve. The work has demonstrated a significant improvement of stability obtained for a system with the novel concept implemented both theoretically and experimentally. The stability has been investigated both using a linear and a nonlinear model of a hydraulically actuated experimental setup. The presented novel concept circuit has the same steady state characteristics as the base circuit but without the corresponding oscillatory nature. Because the Main Spool of the DCV is not used for stabilising the system, the novel concept can be combined with any feedback control strategy. In this project, the novel concept is presented with linear actuators only. However,its use covers circuits with rotational actuators and CBV’s as well. The base circuit is used as a reference for comparison. Therefore, the stability of the base circuit is also investigated with a linear model

  • Reduction of Oscillations in Hydraulically Actuated Knuckle Boom Cranes
    Universitet i Agder University of Agder, 2016
    Co-Authors: Sørensen, Jesper Kirk
    Abstract:

    A knuckle boom crane is characterized by being a versatile machine that during operation experiences large load variations caused by the changes in position and payload. Common uses are as a mobile loader crane mounted on trucks and in offshore applications. Since their introduction the use of counterbalance valves (CBV) have been the de facto standard on load-carrying hydraulically actuated applications like the knuckle boom crane. It offers a simple and practical solution to one of the issues of mobile cranes: Controlling the load safely when lowering. By law (e.g. European Standard) the hydraulic circuit of load-carrying applications is required to contain a load holding protection device. The classical way of actuating such a crane is to use a circuit containing a pressure compensator valve and a directional control valve (DCV) in series with a CBV. This circuit is referred to as the base circuit. It is well known that this combination of valve components tends to introduce instability in the base circuit. This is Mainly a problem when the controlled actuator is subjected to a negative load, because this will require the CBV to throttle the return flow. The instability presents itself as pressure oscillations in the hydraulic circuit which cause the mechanical structure to oscillate. The consequence of the oscillations is a decreased accuracy of the boom motion which create a safety risk, reduces productivity and introduces an undesirable extra fatigue load. The objective of this project was to investigate the oscillations created in the hydraulic circuit of knuckle boom cranes and reduce their severity. The effort has Mainly been split in two: First, was looked into existing solutions with the focus on the ones not requiring control systems to function. This was done with reliability and robustness in mind. The investigation identified the pressure control valve (PCV) as the best commercially available solution. The use of a PCV to control the inlet flow in crane applications was rather uncharted territory. The valve, a DCV with a pressure control Spool manufactured by Danfoss, has been investigated both theoretically and experimentally. A linear stability analysis has been performed with the Routh-Hurwitz stability criterion. This analysis of the valve used together with a hydraulically actuated experimental setup indicates that the combination is stable in all situations. The use of the pressure control Spool in the DCV is a simple and robust solution to the stability problem of the base circuit. Not related to the PCV’s ability to reduce the oscillations the use of it in knuckle boom cranes, however, comes with certain drawbacks. The drawbacks include a load dependent dead band and a load dependent inlet flow. In order to achieve similar behavior as the normal pressure compensated DCV a closed loop control system is required. These issues are addressed in this project, where control schemes are proposed to handle them. In the second part the perspective of the search was broadened to include solutions using control systems. This has lead to the development of a novel, patent pending, concept that significantly reduces the oscillations of the base circuit. It introduces a secondary circuit where a low-pass filtered value of the load pressure is generated and fed back to the compensator of the flow supply valve. The work has demonstrated a significant improvement of stability obtained for a system with the novel concept implemented both theoretically and experimentally. The stability has been investigated both using a linear and a nonlinear model of a hydraulically actuated experimental setup. The presented novel concept circuit has the same steady state characteristics as the base circuit but without the corresponding oscillatory nature. Because the Main Spool of the DCV is not used for stabilising the system, the novel concept can be combined with any feedback control strategy. In this project, the novel concept is presented with linear actuators only. However,its use covers circuits with rotational actuators and CBV’s as well. The base circuit is used as a reference for comparison. Therefore, the stability of the base circuit is also investigated with a linear model

Xiangdong Kong - One of the best experts on this subject based on the ideXlab platform.

  • Design and Verification of Two-Stage Brake Pressure Servo Valve for Aircraft Brake System
    'MDPI AG', 2021
    Co-Authors: Lilei Zhang, Zhipeng Huang, Yunhe Wang, Xiangdong Kong
    Abstract:

    Wheel braking devices is some of the most widely used landing deceleration devices in modern aircraft. Jet pipe pressure servo valves are widely used in large aircraft wheel brake control systems because of their high anti-pollution ability, high sensitivity and fast dynamic response. However, most brake systems suffer vibration phenomena during the braking process. The pressure servo valve is an important part of the hydraulic brake system, and also an important factor affecting the vibration of the system. In order to solve the vibration problem in the brake system this paper present a two-stage brake pressure servo valve design. We place feedback channels at both ends of the Main Spool to stabilize the output pressure. In addition, modeling, simulation and experimental verifications are carried out. Firstly, the principle and structure of the pressure servo valve are described. An accurate mathematical model of the two-stage brake pressure servo valve and the testing system is established. Then a simulation analysis is carried out. Finally, a two-stage brake pressure servo valve testing experimental platform system is built for experimental verification. The experimental results show that the mathematical model of the two-stage brake pressure servo valve and the test system established in this paper have high accuracy, and the designed servo valve structure can restrain vibrations. The above research results provide a useful theoretical reference for performance optimization, stability analysis and valve body structure improvement of brake pressure servo valves

J M Son - One of the best experts on this subject based on the ideXlab platform.

Ermert Markus - One of the best experts on this subject based on the ideXlab platform.

  • Electromechanical actuator concept for the controlled and direct actuation of a hydraulic Main stage
    Technische Universität Dresden, 2016
    Co-Authors: Ermert Markus
    Abstract:

    Hydraulic Main stages for off highway machines have usually electromagnetic driven pilot valves. You rarely find stepper motor driven pilot systems that are directly positioning the Main Spool in the sectional control valve. The presented concept shows the development of an actuator in a unique setup to fulfill the requirements of most off- highway applications. Precise positioning, strength, speed and fail safe requirements were the Main goals of the concept. The concept has a two phase BLDC transversal flux motor with a single gear stage transmission. The software and control unit are specially designed for this electric motor setup. On a test bench some results of the first samples reveal the technical potential of this concept. The development of the actuator was done in-house of Thomas Magnete GmbH (mechanical, electronical, and software development)

Lilei Zhang - One of the best experts on this subject based on the ideXlab platform.

  • Design and Verification of Two-Stage Brake Pressure Servo Valve for Aircraft Brake System
    'MDPI AG', 2021
    Co-Authors: Lilei Zhang, Zhipeng Huang, Yunhe Wang, Xiangdong Kong
    Abstract:

    Wheel braking devices is some of the most widely used landing deceleration devices in modern aircraft. Jet pipe pressure servo valves are widely used in large aircraft wheel brake control systems because of their high anti-pollution ability, high sensitivity and fast dynamic response. However, most brake systems suffer vibration phenomena during the braking process. The pressure servo valve is an important part of the hydraulic brake system, and also an important factor affecting the vibration of the system. In order to solve the vibration problem in the brake system this paper present a two-stage brake pressure servo valve design. We place feedback channels at both ends of the Main Spool to stabilize the output pressure. In addition, modeling, simulation and experimental verifications are carried out. Firstly, the principle and structure of the pressure servo valve are described. An accurate mathematical model of the two-stage brake pressure servo valve and the testing system is established. Then a simulation analysis is carried out. Finally, a two-stage brake pressure servo valve testing experimental platform system is built for experimental verification. The experimental results show that the mathematical model of the two-stage brake pressure servo valve and the test system established in this paper have high accuracy, and the designed servo valve structure can restrain vibrations. The above research results provide a useful theoretical reference for performance optimization, stability analysis and valve body structure improvement of brake pressure servo valves