Aeritalia

About: Aeritalia is a based out in . It is known for research contribution in the topics: Noise & EMI. The organization has 167 authors who have published 124 publications receiving 1407 citations.

Turbojet engine nozzle for attenuating core and turbine noise

Abstract: Core noise, a low frequency noise component believed to be partly caused by the combustion processes within the engine, and turbine noise, a higher frequency noise component caused by the interaction of high velocity gases with the engine's turbine, are attenuated by noise absorbing structures that are disposed within the engine's nozzle and that in part define the physical geometry of the nozzle duct. The nozzle is formed of an outer sleeve and an inner generally bulb-shaped plug which are coaxially arranged to define an annular nozzle duct that channels the flow of gases rearwardly from the outlet of the engine's turbine. The plug has a hollow interior that is partitioned into a plurality of cavities that communicate with the nozzle duct via perforations provided in an outer wall of the plug. The size, shape and positioning of the interior cavities and outer plug wall perforations are selected so as to absorb noise energy existing in the exhaust gases, both at the relatively low frequencies characteristic of core noise and at the relatively higher frequencies characteristic of turbine noise.

Gas turbine exhaust nozzle for controlled temperature flow across adjoining airfoils

Abstract: An exhaust nozzle for exhausting the effluent of a turbofan gas turbine engine across a portion of the upper surface of an aircraft wing wherein the exhaust nozzle is arranged to establish a temperature profile within the exhausted gases that prevents overheating the wing surface. The nozzle includes a contoured outer housing that longitudinally transists from a circular entrance opening, arranged for interconnection with the rear face of a gas turbine engine, to a semi-elliptical outlet opening located on the upper surface of the aircraft wing. A generally tubular mixer section, of the daisy type, is mounted within the outer housing and coaxially surrounds an engine tail plug. Exhaust gases flowing from the engine fan stage flow through an annular flow duct formed between the inner surface of the forward portion of the outer housing and the outer surface of the mixer section and the high temperature gases flowing from the engine turbine stages flow through an annular duct formed between the tail plug and the inner surface of the mixer section. As the turbine exhaust gases and the fan air flow past the mixer section exit plane, the two fluid streams mix with one another to increase engine thrust and decrease engine noise level. To establish a temperature profile in which the exhaust gases flowing along the aircraft wing do not overheat the wing structure, the outer housing is contoured to have a generally elliptical cross-sectional geometry at the exit plane of the mixer section and the mixer section lobes are of unequal radial dimension such that the mixer section has an asymmetric cross-sectional shape.

Human error detection processes

Abstract: The way in which humans detect their own errors has been a relatively neglected issue. The following study presents data on the relationship between types of errors and behavioural patterns of error detection, with the aim to define the psychological mechanism that allows the detection of errors. The results suggest that different kinds of psychological mechanisms are involved in the detection of different types of error. Effect of practice as a function of the distribution of attentional resources among levels of control of human behaviour is also discussed.

Radar detection of targets located in a coherent K distributed clutter background

Abstract: The paper describes a model for a coherent K distributed clutter by considering a coherent multidimensional Gaussian probability density function where its standard deviation is not known a priori but is itself a random variable with a Gamma distribution. Subsequently, the problems of detecting an a priori known target and a Swerling zero target model embedded in a coherent K distributed clutter are considered. The corresponding detectors based on the likelihood ratio test are evaluated. A mixed numerical and simulation procedure is set up to evaluate the receiver operating characteristics of the processor. The detection probability versus the signal-to-clutter power ratio, having as parameters the probability of false alarm and the clutter skewness, is evaluated for a number of processed pulses.

Combination primary and fan air thrust reversal control systems for long duct fan jet engines

Abstract: Combination primary and fan air thrust reversal control systems for long duct fan jet engines are disclosed. In one form, the system spoils and expands primary air and, then, allows the spoiled, expanded air to exit from the fan air duct exhaust nozzle while directing fan air in a thrust reversal direction out cascade vanes circumferentially located in the aft portion of the engine nacelle. In other forms, the system directs unequal pressure fan air and primary air through separate thrust reversal ducting and out cascade vanes circumferentially located in the engine nacelle. In equal pressure fan air and primary air systems, the air may be mixed in ducting prior to being emitted from common cascade vanes, or may be maintained separate prior to emission. In still other forms, the primary air is pre-exhausted through separate nozzles located in the primary duct wall, and a portion is then exhausted through the nacelle cascade vanes. In all systems, circumferential cascade vanes are radially located in the rear portion of the engine nacelle and are exposed by rearwardly translating the aft portion of the nacelle, which forms the fan air duct exhaust nozzle. As the fan air duct exhaust nozzle is translated rearwardly, fan air duct blocker doors and, depending on the system, primary air duct blocker doors are positioned to divert the jets for thrust reversing. As an alternative to a primary air duct blocker door, the primary air duct exhaust nozzle is translated rearwardly to contact the exhaust cone or plug and, thereby, valve off the primary air duct. In this case, the fan and primary exhaust nozzles are translated rearwardly as unit.