5,028 research outputs found
Reciprocating engines
An intake valve arrangement for positively controlling the opening and closing of the poppet valve in a hot gas cylinder in a hydrazine powered engine is described. The poppet valve is operated by the piston and gas pressure only. The poppet valve uses a pneumatic spring which holds the poppet valve against the piston while the valve is opened and closed. To accomplish this, a poppet valve is slidably mounted in a pneumatic spring chamber which reaches a pressure approaching the gas supply pressure and, during the opening of the valve, the spring chamber retains enough pressure to hold the poppet valve onto the piston. In addition, the bottom of the poppet valve can have a suction cup type configuration to hold the poppet valve on the piston during the down stroke
Permeability Experiments: Design, development and methodology of a resin transfer moulding measuring device [Abstract]
A permeability prediction for non-crimp fabrics
A model is proposed to analyse the variation in the permeability of NonâCrimp Fabrics, originating from variations in the internal structure of the material. A geometrical description of the fabric based on the distortion induced by the stitch threads piercing through the fabric is employed. The distortions form channels which are mutually connected. It is assumed that these channels dominate the permeability of the fabric. A network of flow channels is subsequently defined, in which the variations, measured in the dimensions of the distortions, is explicitly accounted for. The variations in the internal structure of the fabric affect the averaged permeability significantly. Moreover, a network rather that a single unit cell is required to predict the averaged permeability and its variation properly. Finally, the spatial distribution of the randomly generated channel dimensions affects the permeability significantly
Non-crimp fabric permeability modelling
A qualitative study to the in-plane permeability modelling of Non-Crimp\ud
Fabrics has been carried out. A network flow model was developed to describe flow through\ud
inter bundle channels (meso level). To improve this model, it was extended with details that\ud
consider stitch yarn influenced regions. The model predicts a highly anisotropic permeability.\ud
The predicted permeability in the machine direction of the fabric corresponds with the\ud
experimental results. However, prediction of permeability perpendicular to the fabricâs\ud
machine direction does not correspond with the experimental results. Possibly, flow through\ud
fibre filaments (micro level) is significant and the network flow model has to be extended to\ud
include this type of flow
A consolidation process model for film stacking glass/PPS laminates
The applied pressure, processing temperature and holding time influence the\ud
consolidation of thermoplastic laminates. A model to optimise the processing\ud
parameters is proposed. The influence of heating rate, processing temperature and pressure is investigated. Short textile impregnation times, in the order of seconds, are predicted. The model is validated in an experimental programme
Braiding simulation for RTM preforms
Braiding is a manufacturing process that is increasingly being used to manufacture pre-forms for Resin Transfer Moulding. A fast simulation method is presented for the prediction of the fibre distribution on complex braided parts and complex kinetic situations (e.g. changes in velocity, orientation). The implementation is suited for triangular surface representations as generated by many CAD software packages in use. Experimental results are presented to validate the model predictions, showing an acceptable correlation with the data predicted by the simulation method. The guide ring dimensions and spacing appear to have a significant effect on the accuracy of the predicted fibre orientations
Hydrazine monopropellant reciprocating engine development
A hydrazine fueled piston engine for providing 11.2 kW was developed to satisfy the need for an efficient power supply in the range from 3.7 to 74.6 kW where existing nonair-breathing power supplies such as fuel cells or turbines are inappropriate. The engine was developed for an aircraft to fly to 21.3 km and above and cruise for extended periods. A remotely piloted aircraft and the associated flight control techniques for this application were designed. The engine is geared down internally (2:1) to accommodate a 1.8 m diameter propeller. An alternator is included to provide electrical power. The pusher-type engine is mounted onto the aft closure of the fuel tank, which also provides mounting for all other propulsion equipment. About 20 hrs of run time demonstrated good efficiency and adequate life. One flight test to 6.1 km was made using the engine with a small fixed-pitch four-bladed propeller. The test was successful in demonstrating operational characteristics and future potential
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