Ryggsäckar används vid mängder av aktiviteter och har många fördelar jämfört med andra väskor, särskilt när det kommer till att bära tungt. Emellertid blir dåligt utformade ryggsäckar med bristande hänsyn till ergonomiska faktorer obekväma och kan i värsta fall orsaka skador. Studier har visat att belastningen på axlar är den främst begränsande faktorn vid ryggsäcksbärande. Klättermusen har försökt lösa detta problem med innovationen Butterfly Bridge som är tänkt att fördela lasten över axeln på ett mer skonsamt sätt. Projektet genomfördes i syfte att bredda kunskapen kring ryggsäckars påverkan på kroppen samt bidra med information om Butterfly Bridges effekt till uppdragsgivaren. Mer specifikt var målet med projektet att utveckla lämplig metod för att mäta effekten och utvärdera huruvida Butterfly Bridge fungerar som beskrivet och har en mätbar effekt på tryckfördelning mellan ryggsäck och axel. Den inledande litteraturstudien visade på ett antal tillgängliga metoder för att mäta och bedöma en ryggsäcks påverkan på kroppen. För att utvärdera Butterfly Bridges effekt valdes en kvantitativ metod med experimentella tester på testdocka. Trycket mellan axelrem och dockan mättes med taktila trycksensorer från Tekscan. Mätningar gjordes med och utan Butterfly Bridge för två ryggsäckar från Klättermusen, Grip 60L och Ymer 65L. Resultaten visade inte på någon skillnad mellan att använda Butterfly Bridge eller inte. Tryckbilder från mätningarna visade inga synliga skillnader i tryckfördelning och det kan utifrån mätningarna i denna studie inte bevisas att Butterfly Bridge har någon effekt på tryckfördelningen. Slutsatsen är att Tekscan F-Scan kan användas för att mäta skillnader i tryck mellan olika ryggsäckar men metoden är på intet sätt felfri. Fler tester krävs för att bestämma Butterfly Bridges effekt. / <p>2022-07-01</p>

Phased microphone arrays are valuable tools for aeroacoustic measurements that can measure the directivity of multiple acoustic sources. However, when deployed in closed test-section wind tunnels, the acoustics suffer due to intense pressure fluctuations contained in the wall-bound turbulent boundary layer. Furthermore, phased microphone arrays require many sensors distributed over a large aperture to ensure good spatial resolution over a wide frequency range. Microphone arrays of such large count are not always feasible due to constraints in space and cost. This thesis describes an alternative approach for measuring single broadband acoustic sources that uses an acoustic metasurface. The metasurface is comprised of a meandering channel of quarter-wave cavities and an array of equally spaced half-wave open through-cavities. A series of tests were conducted in Virginia Tech's Anechoic Wall-Jet Tunnel where combinations of a wall-bound turbulent jet-flow and a single broadband acoustic source were used to excite the metasurface and produce acoustic surface waves. Measurements of the acoustic surface waves were performed using two methods: a pair of traversing microphones scanning the pressure field along the length of the metasurface 0.25 mm beneath its bottom face, and an array of unequally spaced microphones embedded inside the metasurface. Spectral analysis on the measurements revealed that the inclusion of multiple through-cavities leads to constructive reinforcement of select acoustic surface waves as a function of the acoustic source location. In the case of the embedded microphones, acoustic beamforming was applied in order to extract spatial information. This reinforcement was observed during measurements made with both flow and acoustic excitation, up to Wall-Jet Tunnel nozzle exit speeds of 40 m/s beyond which it was no longer seen. A series of quiescent measurements made with a range of speaker locations constituted a calibration for the metasurface which was used to locate an unknown broadband acoustic source within an The Root-Mean-Square (RMS) error of 1.06 degrees. / Master of Science / Phased microphone arrays are valuable tools for aeroacoustic measurements that can measure the directivity of multiple acoustic sources within a sound field. When used in conjunction with signal processing techniques, such as delay-and-sum beamforming, a researcher or engineer can obtain an intuitive view of the sound field and distinguish between multiple sources over a wide frequency range. However, these microphone arrays often utilize dozens of microphones which raises the array's complexity and cost. Furthermore, when a phased microphone array is mounted flush to the wall of a wind tunnel test section, it is submerged under a turbulent boundary layer which imposes intense pressure fluctuations on the microphones making it difficult to identify acoustic sources. Boundary layers form at the interface between a fluid and solid interface. This thesis describes experimentation performed in the Virginia Tech Anechoic Wall-Jet Tunnel on a new type of pressure sensing microphone array that leverage acoustic metamaterial technology. The acoustic metamaterial shields the microphones from the flow, lessening the influence of the turbulent boundary layer on the measurement. The focus in this thesis is on the novel array's ability to locate a single broadband acoustic source using as few as six microphones. The metasurface was installed in the Wall-Jet Tunnel test plate such that an array of evenly spaced through-cavities are flush to the surface. The through-cavities communicate the pressure field on top of the test surface to a meandering channel of interconnected closed cavities below. Near the resonant depth frequencies of the closed cavities, acoustic surface waves form which are evanescent pressure waves that are bound to the surface or structure that support them. The interference between the acoustic surface waves generated at each through-cavity leads to reinforced acoustic surface waves which are sensitive to the direction of a broadband source. In all, an acoustic metamaterial was tested under a variety of conditions such as: Wall-Jet Tunnel flow speed, speaker location, and the number of through-cavities open. The performance of the novel array and future plans are discussed.

No description available.

This dissertation presents design challenges and promising solutions for temperature and pressure sensors which are highly desirable for harsh-environment applications, such as turbine engines. To survive the harsh environment consisting of high temperatures above 1000°C, high pressures around 300 psi, and corrosive gases, the sensors are required to be robust both electrically and mechanically. In addition, wire connection of the sensors is a challenging packaging problem, which remains unresolved as of today. In this dissertation, robust ceramic sensors are demonstrated for both high temperature and pressure measurements. Also, the wireless sensors are achieved based on microwave resonators. Two types of temperature sensors are realized using integrated resonator/antennas and reflective patches, respectively. Both types of the sensors utilize alumina substrate which has a temperature-dependent dielectric constant. The temperature in the harsh environment is wirelessly detected by measuring the resonant frequency of the microwave resonator, which is dependent on the substrate permittivity. The integrated resonator/antenna structure minimizes the sensor dimension by adopting a seamless design between the resonator sensor and antenna. This integration technique can be also used to achieve an antenna array integrated with cavity filters. Alternatively, the aforementioned reflective patch sensor works simultaneously as a resonator sensor and a radiation element. Due to its planar structure, the reflective patch sensor is easy for design and fabrication. Both temperature sensors are measured above 1000°C. A pressure sensor is also demonstrated for high-temperature applications. Pressure is detected via the change in resonant frequency of an evanescent-mode resonator which corresponds to cavity deformation under gas pressure. A compact sensor size is achieved with a post loading the cavity resonator and a low-profile antenna connecting to the sensor. Polymer-Derived-Ceramic (PDC) is developed and used for the sensor fabrication. The pressure sensor is characterized under various pressures at high temperatures up to 800°C. In addition, to facilitate sensor characterizations, a robust antenna is developed in order to wirelessly interrogate the sensors. This specially-developed antenna is able to survive a record-setting temperature of 1300°C.

Researchers performed 35 full-scale lateral load tests on piles driven within the reinforcement zone of a mechanically stabilized earth wall (MSE wall). Data defining the induced tensile force on the reinforcements during lateral pile loading was used to develop multi-linear regression equations to predict the induced tensile force. Equations were developed by previous researchers that did not consider the diameter of the pile, the fixed head condition, relative compaction, or cyclic loading. The purpose of this research was to include this tensile force data and develop prediction equations that considered these variables. Additionally, a full-scale lateral load test was performed for a 24-inch diameter pipe pile loaded against a 20-inch width square pile. The test piles were instrumented using load cells, string potentiometers, LVDTs, strain gauges and hybrid pressure sensors. The lateral load tests were used to evaluate the ability of finite difference (LPILE) and finite element (PLAXIS3D) models to compute results comparable to the measured results. The results of this analysis showed that the diameter of the pile is a statistically significant variable for the prediction of induced tensile force, and the induced tensile force is lower for piles with larger diameter. Fixed head conditions have no effect on the prediction of induced tensile force. Cyclic loading had minimal impact on the prediction of induced tensile force, but relative compaction did have an important statistical significance. Therefore, prediction equations for induced tensile force in welded wire were developed for relative compaction less than 95 percent and relative compaction greater or equal than 95 percent. A general prediction equation (Eq. 3-4) was developed for ribbed-strip reinforcements that included the effect of pile diameter and larger head loads. With 1058 data points, this equation has an R2 value of 0.72. A general prediction equation (Eq. 3-9) was also developed for welded-wire reinforcements that included data from cyclic and static loading, fixed and free head conditions, and relative compaction for 12-inch wide piles with a higher range of pile head loads. This equation based on 2070 data points has an R2 value of 0.72. The prediction equations developed based on all the available data are superior to equations developed based on the original set of field tests. The finite element models produced results with good agreement with pipe pile measurements while the finite difference model showed better agreement with the square pile measurements. However, for the denser backfills involved, back-calculated soil properties were much higher than would be predicted based on API correlations. The API equations are not well-calibrated for dense granular backfills.

This report describes a simple mechanical system developed for producing dynamic pressures of up to 50 kPa from zero-to-peak and over the frequency range 0-58 Hz. The system is constructed for dynamic calibration of pressure sensors and consists of an open tube, 30 cm in height, mounted vertically on the support plate. The support plate is connected to the vibration exciter which is driven by a piston, a connecting rod, disc and axle, and an electric motor. The pressure  sensor to be calibrated is mounted vertically at the bottom of the open tube so that the diaphragm of the sensor is in contact with the working liquid in the tube. When the system is started, the motion of the piston provides a sinusoidal movement to the open tube and calibration is achieved. The different parts of the system are designed using NX Siemens. MatLab is used to determine the results and graphs from the equations derived. The analysis shows that the displacement, velocity, and acceleration of the system are highly affected by the distance between the disc centre and the disc pin, and the rotational speed of the system. The length of the connecting rod does not affect the displacement and barely affects the velocity and acceleration of the system. The total force, torque, and power of the system is utilized to select the electric motor and the frequency inverter. / Denna rapport beskriver ett enkelt mekaniskt system som utvecklas för att producera dynamiska tryck upp till 50 kPa från noll-till-topp och över frekvensområdet 0-58 Hz. Systemet är konstruerat för dynamisk kalibrering av trycksensor och består av öppet rör 30 cm höjd monteras vertikalt på stödplattan. Stödplattan är ansluten till vibrationsexcite dvs, den yttre cylindern som drivs av en kolv, en vevstake, skiva och axel och en elmotor. Trycksensorn som skall kalibreras är monterad vertikalt vid botten av det öppna röret så att membranet hos sensorn är i kontakt med arbetsvätskan i röret. När systemet startas, ger rörelsen hos kolven som ger vibrationer till det öppna röret och kalibrering uppnås. De olika delarna av systemet är utformade med hjälp av NX Siemens. MatLab används för att bestämma resultaten och diagram härledda från ekvationerna. Analysen visar att den förskjutning, hastighet och acceleration av systemet är i hög grad påverkade av avståndet mellan skivans centrum och skivtappen, och rotationshastigheten hos systemet. Längdn av vevstaken påverkar inte försjutningen och påverkar knappt hastigheten och accelerationen hos systemet. Den totala kraften, vridmomentet och kraften i systemet användes för attvälja de andra komponenterna i systemet dvs, den elektriska motorn och frekvensomvandlaren.

Ultradünne Gläser (engl. Ultra Thin Glass – UTG) sind ab einer Glasdicke von 25 μm industriell herstellbar und verfügen über eine mechanische Flexibilität. Außerdem hat Glas in Abhängigkeit der Glassorte das Potenzial, eine gute chemische und thermisch Beständigkeit sowie gute elektrische Eigenschaften zu besitzen, wodurch es als Sub-stratmaterial für die Aufbau- und Verbindungstechnik der Elektronik geeignet ist. Der-zeit wächst die Anzahl am Markt verfügbarer ultradünner Gläser und durch bereits entwickelte Rolle zu Rolle (R2R) Anlagen ist eine industrielle Verarbeitung von UTG realisierbar. Um Glas, im Speziellen ultradünnes Glas, in der Aufbau- und Verbindungstechnik der Elektronik als Substratmaterial zu nutzen, wird die Anwendung interdisziplinärer Me-thoden notwendig. Durch die vorliegende Arbeit wird ein Überblick verschiedener Verfahren vorgestellt und ausgewählte Verfahren getestet, welche für die Herstellung von UTG-basierter, hochtemperaturfähiger (HT-fähiger) Schaltungsträger und/oder Sensorik notwendig sind. Abgedeckt wird das gesamte Spektrum beginnend bei der Konfektionierung und Bearbeitung über die Funktionalisierung bzw. die Funktions-schichtabscheidung, die Erzeugung HT-fähiger elektrischer Verbindungen bis hin zur Herstellung und den Test von Demonstratoren in Form von Druck- und Kraftsenso-ren. / Ultra Thin Glasses (UTG) can be produced industrially from a thickness of 25 μm and are mechanically flexible. Furthermore, glass has the potential to have a good chemi-cal and thermic persistence (depending on the type of glass) as well as good electrical characteristics, which makes it interesting as a material to use for the packag-ing of integrated circuits of electronics. Currently, the amount of ultra-thin glasses on the market is rising and roll to roll systems (R2R) allow an industrial processing of UTG. For the use of glass, especially ultra-thin glass for the packaging of integrated circuits of electronics, the use of interdisciplinary methods is needed. This thesis will give an overview over different procedures of which some selected ones, that are essential for the production of UGT-based, high-temperature (HT) resistant circuit carrier and/or sensor technology, will be tested. In doing so, the whole range will be covered: from packaging and processing to the functionalisation or functional layer disposition and the creation of HT-capable electrical connection as well as the production and testing of demonstration systems in the form of pressure sensors and force sensors.

No description available.

No description available.

Pressure measurements are required in various industrial applications, including extremely harsh environments such as turbine engines, power plants and material-processing systems. Conventional sensors are often difficult to apply due to the high temperatures, highly corrosive agents or electromagnetic interference (EMI) noise that may be present in those environments. Fiber optic pressure sensors have been developed for years and proved themselves successfully in such harsh environments. Especially, diaphragm based fiber optic pressure sensors have been shown to possess advantages of high sensitivity, wide bandwidth, high operation temperature, immunity to EMI, lightweight and long life. Static and dynamic pressure measurements at various locations of a gas turbine engine are highly desirable to improve its operation and reliability. However, the operating environment, in which temperatures may exceed 600 °C and pressures may reach 100 psi (690 kPa) with about 1 psi (6.9kPa) variation, is a great challenge to currently available sensors. To meet these requirements, a novel type of fiber optic engine pressure sensor has been developed. This pressure sensor functions as a diaphragm based extrinsic Fabry-Pérot interferometric sensor. One of the unique features of this sensor is the all silica structure, allowing a much higher operating temperature to be achieved with an extremely low temperature dependence. In addition, the flexible nature of the sensor design such as wide sensitivity selection, and passive or adaptive temperature compensation, makes the sensor suitable for a variety of applications An automatically controlled CO₂ laser-based sensor fabrication system was developed and implemented. Several novel bonding methods were proposed and investigated to improve the sensor mechanical ruggedness and reduce its temperature dependence. An engine sensor testing system was designed and instrumented. The system generates known static and dynamic pressures in a temperature-controlled environment, which was used to calibrate the sensor. Several sensor signal demodulation schemes were used for different testing purposes including a white-light interferometry system, a tunable laser based component test system (CTS), and a self-calibrated interferometric-intensity based (SCIIB) system. All of these sensor systems are immune to light source power fluctuations, which offer high reliability and stability. The fiber optic pressure sensor was tested in a F-109 turbofan engine. The testing results prove the sensor performance and the packaging ruggedization. Preliminary laboratory and field test results have shown great potential to meet not only the needs for reliable and precise pressure measurement of turbine engines but also for any other pressure measurements especially requiring high bandwidth and high temperature capability. / Ph. D.