Field survey and laboratory tests on composite materials case of GRP (Glass Fiber Reinforced Polyester) tubes for water suply

In the Moldova land, were made two lines of water adduction, having 6000 m length and 40 m slope, or 1/150 slope. The water supply component tubes were disposed under the plant: The tubes are made of glass – reinforced thermosetting plastics (GRP). After about 180 days of operation, one of the lines showed severe deterioration of the quality pipe components. This paper deals with some laboratory tests in order to detect the failure cases of the pipelines components

International Developments in the Field of Unconventional Gas and Oil Extraction: Update 2017

The last few years have witnessed a wealth of studies, reports and assessments being published in many EU member states, by national and international organisations and in the research community on economic, environmental and human health related aspects of unconventional oil and gas exploration and production. Many R&D initiatives are also underway. This report attempts to provide a survey of several of such studies and initiatives, with a focus on the years 2015, 2016 and early 2017. Principally, reports and studies from public bodies and scientific institutes were covered. Additionally, several papers published in peer-reviewed journals were included. A review of the quality of the studies covered, the accuracy of their claims and their possible limitations was not carried out. This report is therefore only meant to provide a compilation of their summaries, without any endorsement of the findings reported in any of the studies and assessments covered in the report.JRC.C.3-Energy Security, Distribution and Market

A Decoupled CHT Procedure: Application and Validation on a Gas Turbine Vane with Different Cooling Configurations

AbstractGas turbine performance improvement is strictly linked to the attainment of higher maximum temperature, hence heat load man- agement becomes an essential activity.This paper presents a decoupled procedure aimed to predict cooling performances and metal temperatures of gas turbine blades and nozzles: needed inputs are evaluated by different tools (CFD, in-house fluid network solver, thermal FEM). The procedure is validated on two different test cases: an internally cooled vane (Hylton et al.[1]), and an internally and film cooled vane (Hylton et al.[2]). Metal temperature and adiabatic effectiveness distributions are compared against experimental data and results from a fully 3D coupled CHT CFD analysis

Development of a multi-payload 2U CubeSat: the Alba project

Alba CubeSat UniPD is a student team of University of Padova with the aim to participate to the ESA Fly Your Satellite! (FYS!) programme and to launch for the first time at University of Padova a CubeSat made by students. The proposed mission has three independent objectives: (1) to collect in-situ measurements of the sub-mm space debris environment in LEO, (2) to study the micro-vibration environment on the satellite throughout different mission phases, (3) to do precise orbit determination through laser ranging and evaluate procedures for fast satellite Pointing, Acquisition and Tracking (PAT) from ground. The proposed technological experiments aim to obtain data that will enrich the current knowledge of the space environment and will provide precious information useful for the further development of some research projects currently performed at University of Padova. In order to reach the objectives, in these years the activities of the teams aimed to develop a 2U CubeSat equipped with three payloads. The first payload is an impact sensor that will be placed on one of the outer faces of the satellite and will be able to count the number of debris impacting the spacecraft thus being able to measure the energy/momentum transferred to the satellite. The second one is a Commercial Off The Shelf (COTS) sensor that measures the micro-vibrations experienced by payloads in a CubeSat in different mission phases. The third one consists in a number of COTS Corner Cube Retroreflectors that will be placed onboard the satellite. Thanks to this, Satellite Laser Ranging (SLR) will be done to collect data on the satellite range and range rate using a facility currently under development at University. This paper presents the mission objectives and motivations. In addition, the mission phases and the preliminary design of the CubeSat reached during the activities of the project are shown. Particular attention is given to the payloads which are the most challenging aspect of this project