<p>In the assembly process of airframe structures there are many drilled holes and on some parts the holes are mainly drilled manually with pneumatic handheld drilling machines. During conventional drilling in metal, burrs appear. To remove these burrs the parts of the structure must be separated and deburred before they can be put together for fastening. This is a time consuming measure and therefore expensive. To facilitate this process and lower production costs some parts of the process needs to be automated.</p><p>A part of this thesis was a project in co-operation with Saab, Novator, Specma Automation and the University of Linköping. The purpose of this project was to investigate the ability of an industrial robot to drill holes in aeroplane structures using orbital drilling.</p><p>How the project tests were carried out and the results of these tests are presented in the first part of this thesis. The tests showed that slip-stick appeared when a force was applied on the working object by the robot. Because of the movement of the pressure foot the drilled hole will be in the wrong position and if the movement appears during drilling the quality of the hole is being poor.</p><p>Several different tests were performed using different amounts of forces and different pressure feet trying to prevent slip-stick from appearing. Finally tests were performed with good results concerning the quality of the holes.</p><p>In the second part of this thesis the proceeding tests that were carried out are presented. The purpose of these tests was to find out how the robot acts when a static pressure is applied on a work object by the robot and try to find out what the cause of the slip-stick was. Several tests were done where the robot applied a force on several different points on the fixture and the slip-stick was measured.</p><p>The tests that were carried out during this thesis showed that an industrial robot can be used to drill holes in aeroplane structures. To make sure that the quality of the drilled holes is sufficient for the high demands of the aeroplane industry the working area of the robot is limited to a small area in front of the robot. The slip-stick that appears when the robot is extended into a position on the far side of the robot is too large for the robot to drill the hole in an accurate position.</p> / <p>Vid flygplansmontering borras det många olika hål och på vissa delar borras större delen av dessa hål manuellt med pneumatiska handborrmaskiner. Vid konventionell borrning i metall bildas oönskade grader. Strukturen plockas därför isär så att graderna kan tas bort innan strukturens delar kan passas samman igen för att sammanfogas. Detta är en tidskrävande åtgärd och därmed dyr och i ett steg att förenkla denna process och få en billigare produktion vill man automatisera vissa steg i denna process.</p><p>En del av detta examensarbete var ett projekt i samarbete med Saab, Novator, Specma Automation och Linköpings Universitet vars syfte var att klargöra en robots förmåga att borra hål i flygplansmaterial med orbitalborrningsteknik.</p><p>I första delen av detta examensarbete redovisas genomförande och resultat av projektets tester. Testerna visade att tryckfoten gled på testmaterialets yta när roboten lade en tryckkraft på testplåten, så kallad slip-stick uppkom. Denna glidning gör att det borrade hålet inte hamnar på rätt position och sker glidningen under borroperationen så försämras hålets kvalité. Flera olika tester gjordes med varierad tryckkraft och med olika tryckfötter för att försöka förhindra att slip-stick uppkom. Tester genomfördes där hål borrades med bra kvalité.</p><p>I den andra delen av denna rapport redovisas fortsättningen på examensarbetet som var en vidareundersökning av de tidigare genomförda testerna. Syftet med denna del var att undersöka hur en industrirobot beter sig när den används för att lägga på en tryckkraft mot ett material samt att försöka ta reda på vad som är orsaken till slip-sticken. Fler tester gjordes där roboten tryckte på olika punkter på en fixtur och de uppkomna slip-sticken mättes upp.</p><p>Testerna under detta examensarbete har visat att det går att använda en industrirobot till att borra hål i flyglansmaterial. För att kvaliteten på de borrade hålen ska klara de höga krav som ställs inom flygplansindustrin är robotens arbetsområde begränsat till ett litet fönster mitt framför roboten. De glidningar som uppkommer när robotarmen är utsträckt långt åt sidan om roboten är alldeles för stora för de positioneringskrav som är på hålens placering på flygplansstrukturen.</p>

In the assembly process of airframe structures there are many drilled holes and on some parts the holes are mainly drilled manually with pneumatic handheld drilling machines. During conventional drilling in metal, burrs appear. To remove these burrs the parts of the structure must be separated and deburred before they can be put together for fastening. This is a time consuming measure and therefore expensive. To facilitate this process and lower production costs some parts of the process needs to be automated. A part of this thesis was a project in co-operation with Saab, Novator, Specma Automation and the University of Linköping. The purpose of this project was to investigate the ability of an industrial robot to drill holes in aeroplane structures using orbital drilling. How the project tests were carried out and the results of these tests are presented in the first part of this thesis. The tests showed that slip-stick appeared when a force was applied on the working object by the robot. Because of the movement of the pressure foot the drilled hole will be in the wrong position and if the movement appears during drilling the quality of the hole is being poor. Several different tests were performed using different amounts of forces and different pressure feet trying to prevent slip-stick from appearing. Finally tests were performed with good results concerning the quality of the holes. In the second part of this thesis the proceeding tests that were carried out are presented. The purpose of these tests was to find out how the robot acts when a static pressure is applied on a work object by the robot and try to find out what the cause of the slip-stick was. Several tests were done where the robot applied a force on several different points on the fixture and the slip-stick was measured. The tests that were carried out during this thesis showed that an industrial robot can be used to drill holes in aeroplane structures. To make sure that the quality of the drilled holes is sufficient for the high demands of the aeroplane industry the working area of the robot is limited to a small area in front of the robot. The slip-stick that appears when the robot is extended into a position on the far side of the robot is too large for the robot to drill the hole in an accurate position. / Vid flygplansmontering borras det många olika hål och på vissa delar borras större delen av dessa hål manuellt med pneumatiska handborrmaskiner. Vid konventionell borrning i metall bildas oönskade grader. Strukturen plockas därför isär så att graderna kan tas bort innan strukturens delar kan passas samman igen för att sammanfogas. Detta är en tidskrävande åtgärd och därmed dyr och i ett steg att förenkla denna process och få en billigare produktion vill man automatisera vissa steg i denna process. En del av detta examensarbete var ett projekt i samarbete med Saab, Novator, Specma Automation och Linköpings Universitet vars syfte var att klargöra en robots förmåga att borra hål i flygplansmaterial med orbitalborrningsteknik. I första delen av detta examensarbete redovisas genomförande och resultat av projektets tester. Testerna visade att tryckfoten gled på testmaterialets yta när roboten lade en tryckkraft på testplåten, så kallad slip-stick uppkom. Denna glidning gör att det borrade hålet inte hamnar på rätt position och sker glidningen under borroperationen så försämras hålets kvalité. Flera olika tester gjordes med varierad tryckkraft och med olika tryckfötter för att försöka förhindra att slip-stick uppkom. Tester genomfördes där hål borrades med bra kvalité. I den andra delen av denna rapport redovisas fortsättningen på examensarbetet som var en vidareundersökning av de tidigare genomförda testerna. Syftet med denna del var att undersöka hur en industrirobot beter sig när den används för att lägga på en tryckkraft mot ett material samt att försöka ta reda på vad som är orsaken till slip-sticken. Fler tester gjordes där roboten tryckte på olika punkter på en fixtur och de uppkomna slip-sticken mättes upp. Testerna under detta examensarbete har visat att det går att använda en industrirobot till att borra hål i flyglansmaterial. För att kvaliteten på de borrade hålen ska klara de höga krav som ställs inom flygplansindustrin är robotens arbetsområde begränsat till ett litet fönster mitt framför roboten. De glidningar som uppkommer när robotarmen är utsträckt långt åt sidan om roboten är alldeles för stora för de positioneringskrav som är på hålens placering på flygplansstrukturen.

For a long time voltage spikes has been seen in measurement data from accelerator magnets during current ramps. These has been believed to be caused by movements, but has never before been studied in depth. The purpose of this thesis is therefore to prove, or disprove, that these events are caused by movements and to analyse what kind of displacements that actually occur. Measurement data from coil voltage, magnetic pick-up coils and current during transients has been acquired and analysed for the Nb3Sn-dipole magnets FRESCA2 and 11T models—named MBHSP107 and MBHSP109. The measurement data is compared to movement simulations that was done with the ROXIE-program, which is used to calculate mutual inductance change for a number of different movement types. The study strongly suggests that the transients are caused by movements, and also indicates that the maximal length of a single slip-stick motion can be up to around 10 micrometers, mostly in the direction of the magnet’s internal forces. The study has proven that transients in measurement data occur due to coil movements, and that these can be quantified—a discovery that can possibly affect future construction and design of accelerator magnets.

Carbon nanotubes are molecular-scale tubes of graphitic carbon that possess many unique properties. They have high tensile strength and elastic modulus, are thermally and electrically conductive, and can be structurally modified using well established carbon chemistries. There is global interest in taking advantage of their unique combination of properties and using these interesting materials as components in nanoscale devices and composite materials. The goal of this research was the correlation of the mechanical properties of coiled carbon nanotubes with their chemical structure. Individual nanocoils, grown by chemical vapor deposition, were attached to scanning probe tip using the arc discharge method. Using a scanning probe microscope the nanocoils are repeatedly brought into and out of contact with a chemically-modified substrate. Precise control over the length (or area) of contact with the substrate is achievable through simultaneous monitoring the cantilever deflection resonance, and correlating these with scanner movement. The mechanical response of nanocoils depended upon the extent of their compression. Nonlinear response of the nanocoil was observed consistent with compression, buckling, and slip-stick motion of the nanocoil. The chemical structure of the nanocoil and its orientation on the tip was determined using scanning and transmission electron microscopy. The mechanical stiffness of eighteen different nanocoils was determined in three ways. In the first, the spring constant of each nanocoil was computed from the slope of the linear response region of the force-distance curve. The assumptions upon which this calculation is based are: 1) under compression, the cantilever-nanocoil system can be modeled as two-springs in series, and 2) the nanocoil behaves as an ideal spring as the load from the cantilever is applied. Nanocoil spring constants determined in this fashion ranged from 6.5x10-3 to 5.16 TPa for the CCNTs understudy. In the second, the spring constant of the nanocoil was computed from measuring the critical force required to buckle the nanocoil. The critical force method measured the force at the point where the nanocoil-cantilever system diverges from a linear region in the force curve. Nanocoil spring constants determined in this fashion ranged from 1.3x10-5 to 10.4 TPa for the CCNTs understudy. In the third, the spring constant of each nanocoil was computed from the thermal resonance of the cantilever-nanocoil system. Prior to contact of the nanocoil with the substrate, the effective spring constant of the system is essentially that of the cantilever. At the point of contact and prior to buckling or slip-stick motion, the effective spring constant of the system is modeled as two springs in parallel. Nanocoil spring constants determined in this fashion ranged from 2.7x10-3 to 0.03 TPa for the CCNTs understudy. Using the thermal resonance of the cantilever system a trend was observed relating nanocoil structure to the calculated modulus. Hollow, tube-like nanostructures had a higher measured modulus than solid or fibrous structures by several orders of magnitude. One can conclude that the structure of carbon nanocoils can be determined from using their mechanical properties. This correlation should significantly contribute to the knowledge of the scientific and engineering community. It will enable the integration of carbon nanocoils in microelectromechanical (MEMS) or nanoelectromechanical systems (NEMS) as resonators, vibration dampers, or any other application in which springs are used within complex devices.

This thesis deals with computational modeling of curve squeal noise phenomena which occurs during cornering tight curves by trams. Lateral creep between rail and wheel and slip-stick phenomena leads to self-excited vibrations of the wheel which, therefore, emits unpleasant high-pitched noise. Two FEM models in frequency domain are carried out. First model is based on prestressed modal analysis. Due to unsymmetric stiffness matrix, unstable eigenvalues can occur. It is assumed that self-excited vibrations occurs on frequencies corresponding to that eigenvalues. Second model uses harmonic response analysis. It examines vibrations of the wheel excited by lateral creep force acting in contact region. This force is obtained externally by simple time-domain model. Results from harmonic response are used consequently for noise radiation computation.

The aim of this diploma thesis is to develop a linear positioning stage for Ultra High Vacuum (UHV) environment. Simple prototypes of the linear positioning stage were designed and incorporated as part of a multiaxis sample manipulator for a UHV Scanning Tunneling Microscopy / Atomic Force Microscopy (STM/AFM). Different types of position encoders and linear guideways are discussed. Implementation of the homodyne interferometer as an optimization tool for a slip-stick based linear stage is described. Scalar diffraction theory is used to model the diffraction grating optical position encoder behavior.