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  • 1
    Electronic Resource
    Electronic Resource
    Springer
    Medical & biological engineering & computing 1 (1963), S. 203-215 
    ISSN: 1741-0444
    Source: Springer Online Journal Archives 1860-2000
    Topics: Biology , Chemistry and Pharmacology , Medicine
    Description / Table of Contents: Résumé La détermination du débit cardiaque et du volume central du sang est d'une importance capitale non seulement pour les examens du coeur mais encore pour le diagnostic et le traitement de cardiopathies. A l'heure actuelle, la méthode de dilution d'indicateurs semble être la méthode cliniquement la plus appropriée pour déterminer ces paramètres. Cependant, l'analyse des courbes de dilution d'indicateurs prend beaucoup de temps, car même un opérateur rompu au travail met 20 à 40 minutes pour la réaliser. On a donc créé un instrument simple permettant de déterminer le débit cardiaque et le volume du sang en omins d'une minute. L'ordinateur décrit dans la présente communication se sert d'une courbe produite par voie électronique et qui apparaît sur un CRT; cette courbe sera superposée optiquement à la courbe actuelle de dilution de l'indicateur. 3 contrôles réglés à la main permettent de faire coincider les deux courbes, et donnent de la sorte les paramètres désirés. L'ordinateur peut être utilisé pour analyser les courbes dans les domaines suivants: amplitude de courbe (2A) —2,5–10 cm; période (T) 2,5–10 secondes; constant de temps (CT)—(0,25−1)xT secondes; injection (I) 5–12,5 mg; calibrage (M) 5–1,2 cm/mg-litre; débit cardiaque 0–48 litres/minutes; temps de circulation moyen—25 secondes.
    Abstract: Zusammenfassung Die Bestimmung der Herzauswurfleistung und des umlaufenden Blutvolumens ist von großer Bedeutung nicht nur für Herzuntersuchungen, sondern auch für Diagnose und Behandlung von Herzkrankheiten. Zur Zeit ist die Indikator-Verdünnungstechnik die klinisch am besten geeingete Methode zur Bestimmung der entsprechenden Parameter. Allerdings ist die Auswertung der Indikator-Verdünnungskurven ein zeitraubendes Unterfangen, da auch ein geschickter Laborant hierzu 20 bis 40 Minuten benötigt. Es ist nun ein einfaches Instrument geschaffen worden, mit welchem sich Herzauswurfleistung und Blutvolumen in weniger als 1 Minute bestimmen lassen. Der in der vorliegenden Arbeit beschriebene Rechenautomat arbeitet mit einer elektronisch erzeugten Kurve, die auf einem CRT erscheint und optisch der tatsächlichen Indikator-Verdünnungskurve überlagert wird. 3 handbetätigte Steuerorgane, mit welchen die Kurven in übereinstimmung gebracht werden, ergeben die gewünschten Parameter. Der Rechenautomat läßt sich dazu benutzen, die Kurven in folgenden Bereichenauszuwerten: Kurven amplitude (2A)—2,5–10 cm. Periode (T)—2,5–10 Sekunden. Zeitkonstante (CT)—(0,25–1)×T Sekunden. Injektion (I)—5–12,5 mg. Kalibrierung (M)—5–1,2 cm/mg-Liter. herzauswurfleistung—0–48 Liter. Mittlere Umlaufzeit—25 Sekunden.
    Notes: Abstract The determination of cardiac output and central blood volume is of considerable importance, not only in cardiac research but i the diagnosis and treatment of heart disease. At present, the most clinically adaptable method of determining these parameters is the indicator-dilution technique. However, analysis of indicator-dilution curves is laborious, requiring 20–40 min. of a skilled operator's time. A simple instrument has been devised which permits the determination of cardiac output and central blood volume in less than one min. The computer described in this paper makes use of an electronically-generated curve which is displayed on a CRT and optically superimposed on the actual indicator-dilution curve. Three manual controls, used to match the curves, yield the desired parameters. The computer may be used to analyse curves within the following ranges: Curve amplitude (2A)—2.5–10 cm; Period (T)—2.5–10 sec; Time constant (CT)—(0.25–1)×T sec; Injection (I)—5–12.5 mgm; Calibration (M)—5–1.2 cm/mgm-liter; Cardiac output—0–48 liters/min Mean transit time—25 sec full scale.
    Type of Medium: Electronic Resource
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  • 2
    Publication Date: 2019-06-27
    Description: Methods used to determine a procedure for correcting static engine data for the effects of forward motion are described. Data were analyzed from airplane flyover and static-engine tests with a JT8D-109 low-bypass-ratio turbofan engine installed on a DC-9-30, with a CF6-6D high-bypass-ratio turbofan engine installed on a DC-10-10, and with a JT9D-59A high-bypass-ratio turbofan engine installed on a DC-10-40. The observed differences between the static and the flyover data bases are discussed in terms of noise generation, convective amplification, atmospheric propagation, and engine installation. The results indicate that each noise source must be adjusted separately for forward-motion and installation effects and then projected to flight conditions as a function of source-path angle, directivity angle, and acoustic range relative to the microphones on the ground.
    Keywords: AIRCRAFT PROPULSION AND POWER
    Type: NASA-CR-134954 , MDC-J7708
    Format: application/pdf
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  • 3
    Publication Date: 2019-07-13
    Description: Flyover and static noise data from several engines are presented that show inlet fan noise measured in flight can be lower than that projected from static tests for some engines. The differences between flight and static measurements appear greatest when the fan fundamental tone due to rotor-stator interaction or to the rotor-alone field is below cutoff. Data from engine and fan tests involving inlet treatment on the walls only are presented that show the attenuation from this treatment is substantially larger than expected from previous theories or flow duct experience. Data showing noise shielding effects due to the location of the engine on the airplane are also presented. These observations suggest that multiringed inlets may not be necessary to achieve the desired noise reduction in many applications.
    Keywords: PROPULSION SYSTEMS
    Type: AIAA PAPER 74-946 , Aircraft Design, Flight Test and Operations Meeting; Aug 12, 1974 - Aug 14, 1974; Los Angeles, CA
    Format: text
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  • 4
    Publication Date: 2019-07-13
    Description: Flyover and static noise data from several engines are presented that show inlet fan noise measured in flight can be lower than that projected from static tests for some engines. The differences between flight and static measurements appear greatest when the fan fundamental tone due to rotor-stator interaction or to the rotor alone field is below cutoff. Data from engine and fan tests involving inlet treatment on the walls only are presented that show the attenuation from this treatment is substantially larger than expected from previous theories or flow duct experience. Data showing noise shielding effects due to the location of the engine on the airplane are also presented. These observations suggest that multiringed inlets may not be necessary to achieve the desired noise reduction in many applications.
    Keywords: PROPULSION SYSTEMS
    Type: NASA-TM-X-71591 , E-8045 , Aircraft Design Flight test and Operations Meeting; Aug 12, 1974 - Aug 14, 1974; Los Angeles
    Format: application/pdf
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