Temperature control system for lubricant and fuel of a jet engine
The system provides temperature control of oil and fuel in the turbojet engine (1) equipped with an alternator (2). It includes a first oil circuit (4) for cooling the engine oil, and a second oil circuit (10) for cooling the lubrication oil for the alternator. The first oil circuit (4) includes an...
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Main Authors | , , , , , , , , , , , |
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Format | Patent |
Language | English French German |
Published |
10.07.1996
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Edition | 6 |
Subjects | |
Online Access | Get full text |
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Summary: | The system provides temperature control of oil and fuel in the turbojet engine (1) equipped with an alternator (2). It includes a first oil circuit (4) for cooling the engine oil, and a second oil circuit (10) for cooling the lubrication oil for the alternator. The first oil circuit (4) includes an air/oil heat exchanger (5) and a fuel/oil heat exchanger (7) as well as an oil/oil heat exchanger for the cooling the oil circulating in the second oil circuit (10). Controls (20-25) are provided for the flow of oil through the exchangers as a function of the flight conditions and the oil temperatures.
L'invention concerne un système de régulation des températures d'huile et du carburant dans un turboréacteur (1) équipé, d'un alternateur (2), et comportant un premier circuit d'huile (4) pour le refroidissement de l'huile du moteur, un deuxième circuit d'huile (10) pour le refroidissement de l'huile de lubrification des moyens d'entraînement (3) de l'alternateur. Le premier circuit d'huile (4) comporte d'amont en aval un échangeur de chaleur air/huile (5), un échangeur de chaleur huile/carburant (7) et un échangeur huile/huile (8) pour le refroidissement de l'huile circulant dans le deuxième circuit (10). |
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Bibliography: | Application Number: EP19960400015 |